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clc I=100 //current drawn in amperes ra=0.07 //armature resistance in ohms Vt=230 //terminal voltage of motor in volts mprintf("Eg*=VT*-Iara*=%fV\n",Vt-(I*ra)) n=1200 //speed of rotation in rev/min mprintf("w*=%dπrad/sec\n",(n/60)*2) mprintf("KaΦ=Eg*/w*=%fV-s/rad\n",(Vt-(I*ra))/((n/60)*2*%pi))//ans may vary due to roundoff error Ia=100 //armature current in ampere mprintf("τd=KaΦIa=%fN-m\n",(Ia*(Vt-(I*ra))/((n/60)*2*%pi)))//ans may vary due to roundoff error Td=300 //torque in N-m Ia=Td/((Vt-(I*ra))/((n/60)*2*%pi))//ans may vary due to roundoff error mprintf("Ia=τd/KaΦ=%fA\n",Ia) ra=0.07 //resistance in ohms VT=230 //voltage in volts w=(VT-Ia*ra)/((Vt-(I*ra))/((n/60)*2*%pi)) mprintf("w=(VT-Iara)/KaΦ=%frad/sec\n",w)//ans may vary due to roundoff error
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a b d u s 압 두 스 a b r a h a m 아 브 라 함 a c k e r m a n n 아 커 만 a d a l b e r t 아 달 베 르 트 a d d i n g t o n 애 딩 턴 a i k e n 에 이 킨 a l a s k a 알 래 스 카 a l b a n i a 알 바 니 아 a l b a n y 올 버 니 a l e c 앨 릭 a l f a 알 파 a l m q v i s t 알 름 크 비 스 트 a m b e r 앰 버 a n c h o r a g e 앵 커 리 지 a n c o n a 안 코 나 a n d e r s 안 데 르 스 a n d e r s e n 안 데 르 센 a n d r e 안 드 레 a n d r e s 안 드 레 스 a n g e l a 앙 겔 라 a n g e l a 앤 젤 라 a n g e l l 에 인 절 a n g e l o 안 젤 로 a n k r a h 안 크 라 a n n e m a r i e 아 네 마 리 a n s e l 언 셀 a n t e l a m i 안 텔 라 미 a n t o n o v 안 토 노 프 a p p e l 아 펠 a p p i a 아 피 아 a r a g o n 아 라 곤 a r l i n g t o n 알 링 턴 a r n e 아 르 네 a r n i m 아 르 님 a s s e r 아 세 르 a s t l e y 애 스 틀 리 a s u n c i o n 아 순 시 온 a u d e n 오 든 a v a 에 바 a v v a k u m 아 바 쿰 b a b e 베 이 브 b a d a j o z 바 다 호 스 b a d e n 바 덴 b a h r a i n 바 레 인 b a i e r 바 이 어 b a n a c h 바 나 흐 b a n t i n g 밴 팅 b a r d e m 바 뎀 b a r n a b y 바 르 나 비 b a r s t o w 바 르 스 토 우 b a r t o l o m m e o 바 르 톨 롬 메 오 b a s r a 바 스 라 b a s s e t t 바 셋 b a t c h e l o r 배 첼 러 b a u t i s t a 바 티 스 타 b a y r e u t h 바 이 로 이 트 b e a d l e 비 들 b e b e l 베 벨 b e c h e r 베 허 b e l a s c o 벨 라 스 코 b e l l 벨 b e n i t o 베 니 토 b e n n e t t 베 넷 b e r g s o n 베 르 그 송 b e r m a n 버 만 b e r n a r d o 베 르 나 르 도 b e r n e 베 른 b e r n o u l l i 베 르 누 이 b e s a n c o n 브 장 송 b e s s a r a b i a 베 사 라 비 아 b i b e r 비 버 b i l l i n g s 빌 링 스 b i n y o n 비 니 언 b i r k h o f f 버 코 프 b i s h o p 비 숍 b l a c k 블 랙 b l a c k s t o n e 블 랙 스 톤 b l o c k 블 록 b o 보 b o e t h i u s 보 이 티 우 스 b o n s e l s 본 젤 스 b o p p 보 프 b o r d e a u x 보 르 도 b o r g e 보 르 그 b o r j a 보 르 하 b o r o d i n 보 로 딘 b o t h a 보 타 b o t s f o r d 보 츠 포 드 b o v e t 보 베 b o w i e 보 위 b o w m a n 보 먼 b r a h m s 브 람 스 b r a z z a v i l l e 브 라 자 빌 b r e n d a n 브 렌 던 b r o o k i n g s 브 루 킹 스 b r u c e 브 루 스 b r u c h 브 루 흐 b r y a n 브 라 이 언 b u b e r 부 버 b u k h a r i n 부 하 린 b u n d y 번 디 b u r d i n 버 딘 b u r g 부 르 그 b u r n e t t 버 넷 b u s o n i 부 소 니 b u t l e r 버 틀 러 b u t t e r f i e l d 버 터 필 드 c a i r d 케 어 드 c a l d e c o t t 콜 더 컷 c a l f a 찰 파 c a m p a n e l l a 캄 파 넬 라 c a n b e r r a 캔 버 라 c a n t o r 칸 토 어 c a p r i v i 카 프 리 비 c a r a c a s 카 라 카 스 c a r d a n o 카 르 다 노 c a r d i f f 카 디 프 c a r d i n a l 카 디 날 c a r p e n t i e r 카 르 펜 티 에 르 c a r r e r a 카 레 라 c a r s o n 카 슨 c a s a d e s u s 카 자 드 쥐 c a s s i d y 캐 시 디 c e s a r o t t i 체 사 로 티 c h a p l i n 채 플 린 c h a u m o n t 쇼 몽 c h e d d a r 체 더 c h e r n o v 체 르 노 프 c h e s t e r 체 스 터 c i n d y 신 디 c i r i a c o 크 리 아 코 c o i m b r a 코 임 브 라 c o l o m b o 콜 롬 보 c o l t 콜 트 c o n d o r c e t 콩 도 르 세 c o n s t a n c e 콘 스 탄 스 c o p e n h a g e n 코 펜 하 겐 c o s s a 코 사 c r a n a c h 크 라 나 흐 c r a w f o r d 크 로 퍼 드 c r o c e 크 로 체 c r o n a c a 크 로 나 카 c u b a 쿠 바 c u r t i s 커 티 스 c u r t i z 커 티 스 d a g e r m a n 다 게 르 만 d a k a r 다 카 르 d a m o n 데 이 먼 d a r t 다 트 d a v i d s o n 데 이 비 슨 d e s m o u l i n s 데 물 랭 d i a l l o 디 앨 로 d i c e y 다 이 시 d i e s e l 디 젤 d i x i e 딕 시 d o d g e 다 지 d o i s y 도 이 지 d o n 단 d o n a l d 도 널 드 d o r e e n 도 린 d o r t m u n d 도 르 트 문 트 d o w n s 다 운 스 d o w n s 다 운 즈 d r e x l e r 드 렉 슬 러 d u b l i n 더 블 린 d u d l e y 더 들 리 d u l u t h 덜 루 스 e a s t o n 이 스 턴 e b b i n g h a u s 에 빙 하 우 스 e c k a r d t 에 카 르 트 e d d i n g t o n 에 딩 턴 e i s e n s t a d t 아 이 젠 슈 타 트 e l a m 엘 람 e l i z a b e t h 엘 리 자 베 스 e l y 일 리 e m i n e s c u 에 미 네 스 쿠 e n d r e 엔 드 레 e r i c k 에 릭 e r r o l 에 럴 e s a i a s 에 사 이 아 스 e s e n i n 예 세 닌 e u c l i d 유 클 리 드 e u l e r 오 일 러 e v a n s v i l l e 에 번 즈 빌 e v e r s o n 에 버 슨 e z e k i e l 에 제 키 엘 f a n o 파 노 f e c h n e r 페 히 너 f e r n 펀 f e t 페 트 f i l m e r 필 머 f i n l a n d 핀 란 드 f i o n a 피 오 나 f i o r e n t i n o 피 오 렌 티 노 f i r e s t o n e 파 이 어 스 톤 f i s h e r 피 셔 f l e i s c h e r 플 라 이 셔 f l o r e n c e 플 로 렌 스 f o n t e y n 폰 테 인 f o s t e r 포 스 터 f o u r n i e r 푸 르 니 에 f r a g o n a r d 프 라 고 나 르 f r a n c e s c a 프 란 체 스 카 f r a n c i s 프 랑 시 스 f r a n c i s c o 프 란 시 스 코 f r a n k e n 프 랑 켄 f r a s e r 프 레 이 저 f r a z e r 프 레 이 저 f r i e d m a n 프 리 드 만 f r i s c h 프 리 슈 f r o m e n t i n 프 로 망 탱 f u l l e r 풀 러 f u l l e r t o n 풀 러 턴 f u n k 풍 크 f u r m a n o v 푸 르 마 노 프 g a b r i e l 가 브 리 엘 g a j 가 이 g a j d u s e k 가 이 듀 섹 g a l l o n i 갤 로 니 g a l l u p 갤 럽 g a n c e 강 스 g a n g e s 갠 지 스 g a r f i e l d 가 필 드 g a r n i e r 가 르 니 에 g e o f f r e y 제 프 리 g e o r g e t t e 조 젯 g e o r g i a 그 루 지 아 g e o r g i a 조 지 아 g e r a s i m o v 게 라 시 모 프 g e r l a c h 게 를 라 흐 g e r m a i n 제 르 맹 g i b b o n s 기 번 스 g i g l i 질 리 g i l l e s p i e 길 레 스 피 g i n a s t e r a 히 나 스 테 라 g i u l i a n o 줄 리 아 노 g o e b e l 괴 벨 g o e s 구 스 g o g o l 고 골 리 g o k h a l e 고 칼 레 g o l d b e r g 골 드 버 그 g o l d m a n n 골 드 만 g o m b r i c h 곰 브 리 치 g o r c h a k o v 고 르 차 코 프 g o r e 고 어 g o r t e r 고 르 테 르 g o r t e r 호 르 터 g o t t l i e b 고 틀 리 브 g r a c e 그 라 스 g r e e c e 그 리 스 g r e e r 그 리 어 g r e k o v 그 레 코 프 g r e y 그 레 이 g r o e t h u y s e n 그 레 튀 쟁 g u a d a l u p e 과 달 루 페 g u i l l a u m e 기 욤 g u i l l a u m i n 기 요 맹 g u l d b e r g 굴 드 베 르 그 g u l d b e r g 굴 베 르 그 g u l l s t r a n d 굴 스 트 란 드 g u s t a v e 구 스 타 브 h a b e r 하 버 h a i t i 아 이 티 h a l l w a c h s 할 박 스 h a m b u r g 함 부 르 크 h a n d e l 헨 델 h a n k e l 항 켈 h a r d i e 하 디 h a r s a n y i 허 샤 니 h a s e n c l e v e r 하 젠 클 레 버 h a s k e l l 하 스 켈 h a u s h o f e r 하 우 스 호 퍼 h a w o r t h 하 스 h a y d n 하 이 든 h e a l e y 힐 리 h e l d 헬 드 h e l m s 헬 름 스 h e l s i n k i 헬 싱 키 h e r r i o t 에 리 오 h e r s h e y 허 시 h e r t f o r d 하 트 퍼 드 h e y m a n s 하 이 만 스 h i b e r n i a 하 이 버 니 아 h i l f e r d i n g 힐 퍼 딩 h i n t o n 힌 턴 h o d g s o n 호 지 슨 h o l l o w a y 홀 러 웨 이 h o l t 홀 트 h o u d o n 우 동 h o w e l l s 하 우 얼 스 h u g u e n o t 위 그 노 h u g u e t t e 위 게 트 h u r l e y 헐 리 h u t c h e s o n 허 치 슨 h u t c h i n s o n 허 친 슨 h y a t t 하 이 엇 i l o n a 일 로 나 i m b e r t 임 베 르 트 i n d r a 인 드 라 i r v i n g 어 빙 i s k a n d a r 이 스 칸 달 i s l a m a b a d 이 슬 라 마 바 드 i s l e r 아 이 슬 러 i s r a e l 이 스 라 엘 j a g a n 제 이 건 j a m s a 잠 사 j a n i c e 제 니 스 j a q u e s 자 크 j e n a 예 나 j e n n y 제 니 j e p s e n 제 프 슨 j e r e m i a h 예 레 미 야 j e r r o l d 제 럴 드 j e r z y 예 지 j e s s 제 스 j o f f r e 조 프 르 j o h n s o n 욘 손 j o h n s o n 존 슨 j o i n v i l l e 주 앵 빌 j o s p i n 조 스 팽 j o u v e t 주 베 j u l i a n 율 리 아 누 스 j u l i e 줄 리 k a l i m a n t a n 칼 리 만 탄 k a m a l 카 말 k a n d e l 캔 들 k a n t o r 캔 터 k a r p 카 프 k a y 케 이 k a z a n 카 잔 k e k k o n e n 케 코 넨 k e l l e r m a n n 켈 러 만 k e n 켄 k e n t 켄 트 k e p l e r 케 플 러 k e y s e r l i n g 카 이 절 링 k h a c h a t u r y a n 하 차 투 리 안 k i s s i n g e r 키 신 저 k l i m t 클 림 트 k l i n g e r 클 링 거 k l u g e 클 루 게 k o e n i g s b e r g e r 퀴 니 스 버 거 k o h l r a u s c h 콜 라 우 슈 k o k 코 크 k o l a r o v 콜 라 로 프 k r a k o w 크 라 코 프 k r a s n o y a r s k 크 라 스 노 야 르 스 크 k u l i k o v 쿨 리 코 프 k u s c h 쿠 시 k y d 키 드 l a g o s 라 고 스 l a o 라 오 l a s k y 래 스 키 l a u r e l 라 우 렐 l e m a i t r e 르 메 트 르 l e n z 렌 츠 l e o n 레 옹 l e o n 리 옹 l e p s i u s 렙 시 우 스 l e s z e k 레 셰 크 l e v 예 프 l e y t e 레 이 테 l i b y a 리 비 아 l i e 리 l i n d g r e n 린 드 그 렌 l i s t e r 리 스 터 l o f t u s 로 프 터 스 l o m b r o s o 롬 브 로 소 l o n d o n 런 던 l o w e l l 로 웰 l o w i e 로 위 l u b a 루 바 l u c a s 루 카 스 l u c i e n 뤼 시 앵 l u j o 루 조 l u t h e r 루 터 l u t o s l a w s k i 루 토 슬 라 프 스 키 l y m a n 라 이 먼 l y o n 리 옹 l y s e n k o 리 센 코 l y t t o n 리 턴 m a c y 메 이 시 m a d a g a s c a r 마 다 가 스 카 르 m a g e e 매 기 m a g g i e 매 기 m a g n i t o g o r s k 마 그 니 토 고 르 스 크 m a h e n d r a 마 헨 드 라 m a i m o n 마 이 몬 m a i o r 마 이 오 르 m a l a w i 말 라 위 m a l d e n 몰 덴 m a l i k 말 리 크 m a l o n e y 멀 로 니 m a l t h u s 맬 서 스 m a l u s 말 뤼 스 m a m a l o n i 마 말 로 니 m a n d e r 만 데 르 m a n d e v i l l e 맨 더 빌 m a r a 마 라 m a r c 마 르 크 m a r g e r y 마 제 리 m a r i o n 매 리 언 m a r i u s 마 리 우 스 m a r t i n o 마 르 티 노 m a r t i n s o n 마 르 틴 손 m a r x 마 르 크 스 m a r y l a n d 메 릴 랜 드 m a t h e s o n 마 테 존 m a u r i z i o 마 우 리 치 오 m a x i m 맥 심 m a x i m e 막 심 m a x i m i l i a n 막 시 밀 리 안 m a y a 마 야 m b a s o g o 음 바 소 고 m e c k l e n b u r g 메 클 렌 부 르 크 m e l v i l l e 멜 빌 m e l v i n 멜 빈 m e r c o u r i 메 르 쿠 리 m e s s e r e r 메 세 레 르 m e s s i a e n 메 시 앙 m e s s i e r 메 시 에 m i a m i 마 이 에 미 m i k h a i l o v 미 하 일 로 프 m i l l e t 밀 레 m i l n e 밀 른 m i r i a m 미 리 엄 m i t s c h e r l i c h 미 처 리 히 m o l i n a 몰 리 나 m o l o t o v 몰 로 토 프 m o n d r i a a n 몬 드 리 안 m o n g e 몽 주 m o o d 무 드 m o r g a n 모 르 건 m o u s a 무 사 m u r m a n s k 무 르 만 스 크 m u s c a t 무 스 카 트 m u s k o g e e 무 스 코 기 n ' d i a y e 느 쟈 예 n a d a r 나 다 르 n a i r 나 이 르 n a t 냇 n a t o r p 나 토 르 프 n a z a r e t h 나 사 렛 n e b o j s a 네 보 이 사 n e f f 네 프 n e k r a s o v 네 크 라 소 프 n e r u d a 네 루 다 n e r v a 네 르 바 n e y 네 n i c h o l s 니 콜 스 n i c o l e 니 콜 n i j m e g e n 네 이 메 겐 n i k e 나 이 키 n i k e 니 케 n i x o n 닉 슨 n o r f o l k 노 퍽 n o r t h c l i f f e 노 스 클 리 프 n o r t h u m b e r l a n d 노 섬 벌 랜 드 n o v i k o v 노 비 코 프 n o v o s i b i r s k 노 보 시 비 르 스 크 o a x a c a 오 악 사 카 o b 오 브 o c h o a 오 초 아 o g i l v y 오 글 비 o h a n a 오 하 나 o l g a 올 가 o l i v i a 올 리 비 아 o l y m p i a 올 림 피 아 o m s k 옴 스 크 o r e g o n 오 리 건 o r w e l l 오 웰 p a c h e r 파 허 p a d g e t t 패 젯 p a i n e 페 인 p a n k h u r s t 팽 크 허 스 트 p a o l o 파 올 로 p a r a m a r i b o 파 라 마 리 보 p a r e t o 파 레 토 p a r i n i 파 리 니 p a r i s h 패 리 쉬 p a s t o r 파 스 터 p a t t e r s o n 패 터 슨 p a u l i n e 폴 린 p a v l o v 파 블 로 프 p e a r l 펄 p e d r o 페 드 로 p e l t i e r 펠 티 에 p e m b r o k e 펨 브 룩 p e r d u e 퍼 듀 p e r m 페 름 p e r r i e r 페 리 에 p e r r i n 페 랭 p e r s s o n 페 르 손 p e t i p a 페 티 파 p e t t i t 페 티 트 p f i t z n e r 피 츠 너 p h i l i p p i 빌 립 보 p i a z z e t t a 피 아 체 타 p i c a r d 피 카 르 p i c k e r i n g 피 커 링 p i o t r o w s k i 피 오 트 로 프 스 키 p i r q u e t 피 르 케 p i s a r e v 피 사 레 프 p i t m a n 피 트 먼 p i t t 피 트 p i z a r r o 피 사 로 p l e k h a n o v 플 레 하 노 프 p o l l a c k 폴 락 p o m p a d o u r 퐁 파 두 르 p o m p i d o u 퐁 피 두 p o m p o n a z z i 폼 포 나 치 p o n c h i e l l i 폰 키 엘 리 p o r t e r 포 터 p o t a n i n 포 타 닌 p r a t a 프 라 타 p r i n c i p e 프 린 시 페 p r o c t e r 프 록 터 p u c k 퍽 p u n s a l m a a g i y n 푼 살 마 긴 p y m 핌 q u e b e c 퀘 벡 q u e n t i n 퀀 틴 q u i n t o n 퀸 턴 q u i r k 쿽 크 q u i s l i n g 크 비 슬 링 r a f a e l 라 파 엘 r a f i k 라 피 크 r a m e a u 라 모 r a m o n 라 몬 r a n a s i n g h e 라 나 싱 헤 r a n d o l p h 랜 돌 프 r a n k o v i c 랑 코 비 치 r a t h e n a u 라 테 나 우 r e a d 리 드 r e b e c c a 레 베 카 r e i d 리 드 r e i n e r 라 이 너 r e i n h a r d t 라 인 하 르 트 r e n a n 르 낭 r h i n e 라 인 r i c h t e r 리 히 터 r i c k e t t s 리 케 츠 r i e m e n s c h n e i d e r 리 멘 슈 나 이 더 r i v e r s i d e 리 버 사 이 드 r o b b i n s 로 빈 스 r o d g e r s 로 저 스 r o m b e r g 롬 버 그 r o o s e v e l t 루 스 벨 트 r o s a l i e 로 잘 리 r o t h s c h i l d 로 스 차 일 드 r o y c e 로 이 스 r u b i n s t e i n 루 빈 슈 타 인 r y a n 라 이 언 s a b i n e 사 빈 s a l e 사 르 s a l i m 살 림 s a l m o n 살 몽 s a l o m o n 살 로 몬 s a l w e e n 살 윈 s a m o a 사 모 아 s a n t e r 상 테 르 s a r a j e v o 사 라 예 보 s a r g e n t 사 전 트 s a u s s u r e 소 쉬 르 s c h e l l i n g 셸 링 s c h i c k e l e 시 켈 레 s c h m a l e n b a c h 슈 말 렌 바 흐 s c h m i t t 슈 미 트 s c h r e k e r 슈 레 커 s c h u l t z 슐 츠 s c h w a b e 슈 바 베 s c h w a r z 슈 왈 츠 s c h w i n g e r 슈 윙 거 s e g a n t i n i 세 간 티 니 s e i p e l 자 이 펠 s e m 셈 s e v e r o 세 베 로 s e y f e r t 시 퍼 트 s h c h e p k i n 시 쳅 킨 s h e r i d a n 셰 리 던 s h o c k l e y 쇼 클 리 s h o l o k h o v 숄 로 호 프 s i b e l i u s 시 벨 리 우 스 s i d n e y 시 드 니 s i e m e n s 지 멘 스 s i k o r s k i 시 코 르 스 키 s i m o n e 시 모 네 s i n g h 싱 s l o b o d a n 슬 로 보 단 s l o v e n i a 슬 로 베 니 아 s m e d l e y 스 메 들 리 s m e l l i e 스 멜 리 s o l 솔 s o l o w 솔 로 s p o h r 슈 포 어 s t a f f o r d 스 태 포 드 s t a u b 스 타 웁 s t e a d 스 테 드 s t e e l e 스 틸 s t e f f e n 스 테 픈 s t e i n e r 슈 타 이 너 s t e l l a 스 텔 라 s t e p h e n 스 티 븐 s t o c k t o n 스 톡 턴 s t o k e s 스 토 크 스 s t r i c k l a n d 스 트 릭 랜 드 s u l l a 술 라 s u m a t r a 수 마 트 라 s u m m e r s 서 머 스 s u p e r v i e l l e 쉬 페 르 비 엘 s u r i k o v 수 리 코 프 s u t t e r 수 터 s w e e l i n c k 스 벨 링 크 s w i f t 스 위 프 트 s y l v e s t e r 실 베 스 터 t a j i k i s t a n 타 지 키 스 탄 t a l l i s 탤 리 스 t a r k i n g t o n 타 킹 턴 t e n n a n t 테 넌 트 t e n n e s s e e 테 네 시 t h a t c h e r 대 처 t h o m a s 도 마 t h o m a s 토 마 스 t h o m s e n 톰 센 t h o r p e 소 프 t i s o 티 소 t o g l i a t t i 톨 리 아 티 t o n y 토 니 t o w n s e n d 타 운 센 드 t r i c i a 트 리 시 아 t r o l l o p e 트 롤 럽 t r u d e a u 트 뤼 도 u s t i n o v 유 스 티 노 프 u t r e c h t 위 트 레 흐 트 u w e 우 베 v a l e n t i n e 발 렌 타 인 v a l e r i e 발 레 리 v a n e 베 인 v a r r o 바 로 v a u g h a n 본 v e c e l l i o 베 첼 리 오 v e r m o n t 버 몬 트 v e r s a i l l e s 베 르 사 유 v e r t o v 베 르 토 프 v i e u x t e m p s 비 외 탕 v i r c h o w 피 르 호 v l a d i v o s t o k 블 라 디 보 스 토 크 v o l t a 볼 타 v o r o s h i l o v 보 로 실 로 프 v o y n i c h 보 니 치 w a g n e r 바 그 너 w a k e f i e l d 웨 이 크 필 드 w a l t e r 발 터 w a l t h e r 발 터 w a t e r b u r y 워 터 베 리 w e i e r s t r a s s 바 이 어 슈 트 라 스 w e i l 바 일 w e l l e s l e y 웰 즐 리 w e n d 웬 드 w e s t i n g h o u s e 웨 스 팅 하 우 스 w e s t o n 웨 스 턴 w e y d e n 바 이 덴 w h i t w o r t h 휘 트 워 스 w i l k e s 윌 크 스 w i l l c o c k s 윌 콕 스 w i l l e m s t a d 빌 렘 스 타 트 w i l l i 빌 리 w i l l i a m s o n 윌 리 엄 슨 w i m b l e d o n 윔 블 던 w i t t i g 비 티 히 w o l f e r s 월 퍼 스 w o l l s t o n e c r a f t 울 스 턴 크 래 프 트 w o o d r o w 우 드 로 w o o l l e y 울 리 x i e 셰 y a s s i n 야 신 y a t e s 예 이 츠 y e h u d i 예 후 디 z a c h a r i a s 자 카 리 아 스 z a i r e 자 이 르 z a m b e z i 잠 베 지 z a n e t t i 사 네 티 z a n z i b a r 잔 지 바 르 z e m a n 제 만 z e p p e l i n 체 펠 린
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function [x,y,typ]=lpf_2(job,arg1,arg2) // Copyright INRIA x=[];y=[];typ=[]; select job case 'plot' then standard_draw(arg1) case 'getinputs' then [x,y,typ]=standard_inputs(arg1) case 'getoutputs' then [x,y,typ]=standard_outputs(arg1) case 'getorigin' then [x,y]=standard_origin(arg1) case 'set' then x=arg1; graphics=arg1.graphics;exprs=graphics.exprs model=arg1.model; while %t do [ok,in_out_num,ibias1,ibias2,exprs]=getvalue('Set 2nd Order LPF Parameters',['Number of 2nd Order LPF blocks';'First Stage Bias';'Second Stage Bias'],list('vec',1,'vec',-1,'vec',-1),exprs) if ~ok then break,end if length(ibias1) ~= in_out_num then message('The number of first stage bias values that you have entered does not match the number of 2nd Order LPF blocks.'); ok=%f; end if length(ibias2) ~= in_out_num then message('The number of second stage bias values that you have entered does not match the number of 2nd Order LPF blocks.'); ok=%f; end if ok then model.in=in_out_num model.out=in_out_num model.ipar=in_out_num model.rpar = [ibias1;ibias2] model.state = zeros(2*in_out_num,1) graphics.exprs=exprs; x.graphics=graphics;x.model=model break end end case 'define' then ibias1 = 40e-9 ibias2 = 40e-9 xx=[0;0] in_out_num =1 model=scicos_model() model.sim=list('lpf_2_c',5) model.in=in_out_num model.in2=-1 model.intyp=-1 model.out=in_out_num model.out2=-1 model.outtyp=-1 model.rpar = [ibias1;ibias2] model.ipar=in_out_num model.state=xx model.blocktype='d' model.dep_ut=[%f %t] exprs=[sci2exp(in_out_num); sci2exp(ibias1) ; sci2exp(ibias2)] gr_i=['txt=''2nd Order LPF '';';'xstringb(orig(1),orig(2),txt,sz(1),sz(2),''fill'')'] x=standard_define([6 3],model,exprs,gr_i) end endfunction
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function f=%p_i_r(i,j,f2,f) // %p_i_r(i,j,f2,f) <=> f(i,j)=f2 for polynomial matrices //! // Copyright INRIA if type(i)==10 then // s2('num'),s2('den'),sl('dt') [lhs,rhs]=argn(0) if rhs<>3 then error(21),end nams=['num','den','dt'] kf=find(i==nams) if kf==[] then error(21),end f=f2;kf=kf+1 if kf==4 then error('inserted element '+i+' has incorrect type'),end if size(f(kf))<>size(j) then warning('inserted element '+i+' has inconsistent dimension') end f(kf)=j return end [n,d]=f(2:3),[ld,cd]=size(d),l=maxi(i),c=maxi(j) if l>ld then d(ld+1:l,:)=ones(l-ld,cd),ld=l,end if c>cd then d(:,cd+1:c)=ones(ld,c-cd),end n(i,j)=f2,[l,c]=size(f2),d(i,j)=ones(l,c) f(2)=n,f(3)=d
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clear close delta_t=0.001 t = (0:delta_t:10); t = t' ifinal=size(t);ifinal=ifinal(1); F = t; a = 1; b = 2; s = poly(0, 's'); g = syslin('c', a/(s + b)) y = csim(F', t', g)'; filtro = 1/(s+1)^2; hf = syslin('c', filtro); u_fil = csim(F', t', hf); y_fil = csim(y', t', hf); dy_fil = csim(y', t', s*hf); P = 10000*eye(2, 2); theta_plot = zeros(2, ifinal); p = zeros(ifinal); p(1) = norm(P, 'fro') theta = [10;10]; y0 = [0]; right_y0 = y0; omega_n = 5; zeta = 0.9; signal = [ones(2*ifinal/10,1); zeros(2*ifinal/10,1); ones(2*ifinal/10,1); zeros(2*ifinal/10,1); ones(2*ifinal/10 + 1,1)]; y_plot = zeros(ifinal,1) y_plot(1) = y0; right_ki = omega_n^2/a right_kp = (2*zeta*omega_n - b)/a; integral_error = 0; right_integral_error = 0; for i=2:ifinal fi = [u_fil(i) -y_fil(i)]'; K =P*fi/(1+fi'*P*fi); P = (eye(2,2) - K*fi')*P; p(i) = norm(P, 'fro') theta = theta + K*(dy_fil(i) - fi'*theta); theta_plot(:,i) = theta ki = omega_n^2/theta(1) kp = (2*zeta*omega_n - theta(2))/theta(1); signal_error = signal(i)-y0; integral_error = integral_error + delta_t*signal_error; uc = ki*integral_error + kp*signal_error y0 = (delta_t*a*uc+y0)/(1+b*delta_t); right_signal_error = signal(i)-right_y0; right_integral_error = right_integral_error + delta_t*right_signal_error; uc = right_ki*right_integral_error + right_kp*right_signal_error right_y0 = (delta_t*a*uc+right_y0)/(1+b*delta_t); y_plot(i) = y0 y_right_plot(i) = right_y0 end figure(1) plot(t,theta_plot') figure(2) plot(t,p) figure(3) plot(t,signal) plot(t,y_right_plot, '-r') plot(t,y_plot, '-k')
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clc //initialisation of variables k= 0.384 //Btu/hr ft F Tsat= 170.03 //F hfg= 996.2 //Btu/lbm T= 130 //F l= 5 //ft P= 6 //psia g= 4.17*10^8 //ft/h^2 d= 0.042 //ft p= 61.2 //lbm/ft^3 u= 1.05 //lbm/ft h //CALCULATIONS dt= Tsat-T Tf= (Tsat+T)/2 hc= 0.943*((k^3*p^2*g*hfg)/(l*u*dt))^(1/4) hc1= 0.725*((k^3*p^2*g*hfg)/(d*u*dt))^(1/4) //RESULTS printf ('Condensation heat tranfer coefficient if the tube is vertical= %.f Btu/h ft^2 F',hc) printf (' \n Condensation heat tranfer coefficient if the tube is horizontally= %.f Btu/h ft^2 F',hc1)
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clc; clear; disp('Ex-14.8'); //theoretical printf('The reaction can be rewritten as follows U1+U--->S+S1. which implies that U and U1 annihiliate creating S and S1\n'); disp('The pi+ has the quark composition Ud1.Since no quarks are present in the final state. One possible way to get rid of the quarks is to change U into d'); printf('U--->d+W(+). Hence the remaining processes are d+d(+)--->energy and \n W(+)--->u(+) and vu.');
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//Tested on Windows 7 Ultimate 32-bit //Chapter 6 Single Staje BJT Amplifiers Pg no. 191 and 192 clear; clc; //Given Data //Figure 6.9 VCC=15;//collector supply voltage in volts RC=1D3;//collector resistance in ohms RE=390;//emitter resistance in ohms R1=18D3;//divider network resistance R1 in ohms R2=3.9D3;//divider network resistance R2 in ohms VBE=0.7;//forward voltage drop of emitter diode in volts Bdc=120;//DC CE current gain beta Bac=130;//AC CE current gain beta VT=25D-3;//voltage equivalent of temperature in volts Vs=5D-3;//source rms voltage in volts Rs=600;//source internal impedance in ohms re=5;//equivalent BJT model emitter resistance in ohms RL=6.8D3;//load resistance in ohms C2=50D-6;//emitter bypass capacitance in farads //Solution disp("(i)"); RL_dash=RC*RL/(RC+RL);//a.c. value of collector resistance in ohms Gv=RL_dash/re;//a.c. voltage gain printf("A.C. Voltage gain Gv = %.1f\n",Gv); disp("(ii)"); Rin_dash=Bac*(RE+re);//internal resistance of BJT in ohms Rin=1/(1/R1+1/R2+1/Rin_dash);//total internal resistance is Rin=R1||R2||Rin' f=Rin/(Rs+Rin);//input attenuation factor Gv_dash=f*Gv;//overall a.c. voltage gain printf("Overall A.C. Voltage gain Gv'' = %.1f\n",Gv_dash); //gain deviation due to approximations in textbook
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//Ex 2.9.9 clc;clear;close; format('v',8); //Given : Vs=5;//Volt Eta=1;//constant VT=26/1000;//V //I=I0 so exp(V1/Eta/VT)-1=1 V1=log(1+1)*Eta*VT;//Volt V2=Vs-V1;//volt disp(V1,"Voltage across diode D1 in V : "); disp(V2,"Voltage across diode D2 in V : ");
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clear; //clc(); r=14; x=48; i=x; vs=70; vr=66; function [mag,theta]=c(r,i) mag=sqrt(r*r + i*i) theta=atand(i/r) endfunction previousprot = funcprot(0) funcprot(0) [mag,theta]=c(r,i); z=r + (%i)*x; y=(%i)*4*10^(-4); A=1 + 0.5*z*y; [mag,theta]=c(real(A),imag(A)); a=theta; A1=mag; B=z; function [mag,theta]=c(r,i) mag=sqrt(r*r + i*i) theta=atand(i/r) endfunction [mag,theta]= c(r,i); b=theta; B1=mag; pr0=-(A1*vr^2)*cosd(b-a)/(B1); qr0=-(A1*vr^2)*sind(b-a)/(B1); pr=vs*vr/B1; pl=0; q=sqrt(pr^(2) - (pr0 - pl)^(2)) + qr0; qpm=q; s=24; prat=s*0.8; q=sqrt(pr^(2) - (pr0 - prat)^(2)) + qr0; qpmrat=prat*tand(acosd(0.8))-q; printf("\n the rating of the synchronous phase modifier is: %.2f MVAr\n",qpmrat);
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//exapple 7.3 clc; funcprot(0); // Initialization of Variable dr=2;//dia of column mu=2.02/10^5; rho=998; K=5.1; g=9.81; Q=10000/3600; l=50.8/1000; d=l; n=5790; len=18; thik=6.35/1000; pi=3.1414; //part1 //calculation CA=pi*dr^2/4;//cross sectional area u=Q/CA; Vs=pi*d^2/4*l-pi*l/4*(d-2*thik)^2;//volume of each ring e=1-Vs*n; Surfacearea=pi*d*l+2*pi*d^2/4+pi*(d-2*thik)*l-2*pi*(d-2*thik)^2/4; S=Surfacearea/Vs; S=round(S*10)/10; delP=K*S^2/e^3*mu*len*u*(1-e)^2; delh=delP/rho/g; disp(delh*100,"pressure drop in terms of (cm of H20)")
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clear; //clc(); d=6; s=0.3; r=12.5/1000; dab=6; dbc=6; dca=12; dsl=sqrt(0.7788*r*s); dm=(dab*dbc*dca)^(1/3); lb=2*log([dm/dsl])/10; xl=2*(%pi)*50*lb; ds1=0.7788*r*sqrt(2); l1=2*log([dm/ds1])/10; xl1=2*(%pi)*50*l1; printf("\n the line inductance is: %.3f Ohm/km\n",xl1/1000); pu_red=(xl1-xl)/xl1; printf("\n the pu reduction is: %.3f\n",pu_red);
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alpha1 = 0.4; plane_in_region1 = 1/3; plane_in_region2 = 1/3; plane_in_region3 = 1/3; prob1 = (alpha1*plane_in_region1)/((alpha1*plane_in_region1)+ 1*plane_in_region2 + 1*plane_in_region3); prob2 = (1*plane_in_region2)/((alpha1*plane_in_region1)+ 1*plane_in_region2 + 1*plane_in_region3); disp(prob1 , "The probability that the planes is in region 1 given that the search of region 1 did not uncover it "); disp(prob2 , "The probability that the planes is in region 2/3 given that the search of region 1 did not uncover it ");
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// Creates two plots: The first contains numerical solutions for two different methods // (Euler and Heun) for the differential equation y'(t) = 2*t*y^2(t); 0<=t<=0.9; y(0) = 1 // for different amount of nodes // The second contains a graphical comparison between the two methods by calculation // the difference from the analytic solution for 2,4,6,...,1000 nodes clear function y = f_analytic(t) // Returns the value for the analytic solution of the differential equation // y'(t) = 2*t*y^2(t); 0<=t<=0.9; y(0) = 1 // y(t) = 1/(1-t^2) // Input: t = number or vector // Output: f = number or vector y = 1 ./(1-t.^2) endfunction function z = f(t,y) // Returns the value for f(t,y) = 2*t*y^2 // Input: t = number // y = number // Output: z = number z = 2*t*y^2 endfunction function unp1 = euler(un,tn,h,f) // Returns the value u_(n+1) for the numerical solution of the differential equation // y'(t) = 2*t*y^2(t); 0<=t<=0.9; y(0) = 1 // using euler method // Input: un = number (startvalue for y) // tn = number (startvalue for x (boundary condition)) // h = number (delta x) // f = function (=y'(t)) // Output: unp1 = number (=y_(i+1)) tn = tn + h unp1 = un + h*f(tn,un) endfunction function unp1 = heun(un,tn,h,f) // Returns the value u_(n+1) for the numerical solution of the differential equation // y'(t) = 2*t*y^2(t); 0<=t<=0.9; y(0) = 1 // using heun's method // Input: un = number (startvalue for y) // tn = number (startvalue for x (boundary condition)) // h = number (delta x) // f = function (=y'(t)) // Output: unp1 = number (=y_(i+1)) tn1 = tn + h unp1 = un + (h/2)*(f(tn,un)+f(tn1,un+h*f(tn,un))) endfunction function plots(lower,upper,N,y0,subplt,col1,col2) // Creates the plots // Input: lower = number (lower bound) // upper = number (upper bound) // N = number (amount of nodes) // y0 = number (boundary condition) // subplt = number (subplot number) // col = string (color) x = linspace(lower,upper,N)' h = x(2)-x(1) y(1,1) = y0 y(1,2) = y0 for i = 1:1:length(x)-1 y(i+1,1) = euler(y(i,1),x(i+1),h,f) y(i+1,2) = heun(y(i,2),x(i+1),h,f) end subplot(subplt) plot(x,y(1:$,1),col1) plot(x,y(1:$,2),col2) endfunction function bsp17() // Presents the solution y0 = 1 x = linspace(0,0.9,100)' subplot(121) plot(x,f_analytic(x),'k') plots(0,0.9,10,y0,121,'r','r--') plots(0,0.9,20,y0,121,'g','g--') plots(0,0.9,30,y0,121,'b','b--') plots(0,0.9,40,y0,121,'c','c--') plots(0,0.9,50,y0,121,'y','y--') title('Numerical solution') xlabel('x') ylabel('f(x)') legend(['Analytic', 'Euler N = 10', 'Heun N = 10', 'Euler N = 20', 'Heun N = 20', 'Euler N = 30', 'Heun N = 30', 'Euler N = 40', 'Heun N = 40', 'Euler N = 50', 'Heun N = 50'],2) for j = 2:2:1000 x = linspace(0,0.9,j)' h = x(2)-x(1) y(1,1) = y0 y(1,2) = y0 for i = 1:1:length(x)-1 y(i+1,1) = euler(y(i,1),x(i+1),h,f) y(i+1,2) = heun(y(i,2),x(i+1),h,f) end eps(j/2,1) = abs(y($,1)-f_analytic(0.9)) eps(j/2,2) = abs(y($,2)-f_analytic(0.9)) end x = linspace(2,1000,500)' subplot(122) plot(log(x),log(eps(1:$,1)),'r') plot(log(x),log(eps(1:$,2)),'b') title('Convergence') legend('Euler''s method', 'Heun''s method') xlabel('ln(N)') ylabel('ln(ε)') endfunction bsp17()
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// C-Exercise 01 // Nattawut Phanrattinon // Jurian Kahl // (a) Import data data = csvRead('dax_data.csv', ';', '.','double',[],[],[],1); ts = data(:,2); // Plot time series data plot(ts); title('Daily Closing Prices'); xlabel('number of observation'); ylabel('DAX closing prices'); // (b) Compute daily log returns x=diff(log(ts)); scf;,clf; // Plot daily log returns plot(x); title('DAX daily Log Returns'); ylabel('log returns'); // (c) Plot histogram of the log returns using 30 intervals scf;clf; histplot(30,x); title ('Histogram Of DAX daily Log Returns'); xlabel('log returns'); // (d) Compute mu and sigma mu = mean(x); sigma = sqrt(variance(x)); // (e) Plot density of a normal distribution using mu & sigma from (d) x_density = min(x):0.007:max(x) plot(x_density,1/(sqrt(2*%pi)*sigma)*exp(-((x_density-mu)/sigma)^2/2))
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// Scilab code Ex3.8: Pg 93 (2005) clc; clear; // Part (a) h = 6.63e-34; // Plank's constant, Js q = 1.6e-19; // Electric charge, C m_e = 9.11e-31; // Mass of electron, kg c = 3e+08; // Velocity of light, m/s theta = ((%pi)/180)*90; // Angle, radians delta_lamda = (h/(m_e*c)*(1-cos(theta))); // Compton shift, Angstrom lamda_C = 0.0106; // Wavelength of gamma-rays from Cobalt, f_dl_C = delta_lamda/ lamda_C; // Fractional change in wavelength of gamma rays from cobalt printf("\nFractional change in wavelength of gamma rays from Cobalt = %4.2f", f_dl_C*1e+10); lamda_Mo = 0.712; // Wavelength of gamma-rays from Molybdenum, Angstrom f_dl_Mo = delta_lamda/ lamda_Mo; // Fractional change in wavelength of gamma rays from Molybdenum printf("\nFractional change in wavelength of gamma rays from Molybdenum = %6.4f", f_dl_Mo*1e+10); lamda_Hg = 5461; // Wavelength of gamma-rays from Mercury, Angstrom f_dl_Hg = delta_lamda/ lamda_Hg; // Fractional change in wavelength of gamma rays from mercury printf("\nFractional change in wavelength of gamma rays from Mercury = %4.2fe-06", f_dl_Hg*1e+16); // Part (b) lamda = 0.712e-10; // Wavelength of X-rays, Angstrom E = (h*c)/(q*lamda); // Energy of X-rays' photon, eV printf("\nEnergy of X-rays photon = %5.0f eV\n", E); // Result // Fractional change in wavelength of gamma rays from Cobalt = 2.29 // Fractional change in wavelength of gamma rays from Molybdenum = 0.0341 // Fractional change in wavelength of gamma rays from Mercury = 4.45fe-06 // Energy of X-rays photon = 17460 eV
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sce
R-99 Close Fast Strafes.sce
Name=R-99 Close Fast Strafes PlayerCharacters=Apex purple armor R-99 BotCharacters=Apex_bot_close.bot IsChallenge=true Timelimit=60.0 PlayerProfile=Apex purple armor R-99 AddedBots=Apex_bot_close.bot PlayerMaxLives=0 BotMaxLives=0 PlayerTeam=1 BotTeams=2 MapName=boxer.map MapScale=2.0 BlockProjectilePredictors=true BlockCheats=true InvinciblePlayer=true InvincibleBots=false Timescale=1.0 BlockHealthbars=false TimeRefilledByKill=0.0 ScoreToWin=50000.0 ScorePerDamage=50.0 ScorePerKill=200.0 ScorePerMidairDirect=0.0 ScorePerAnyDirect=0.0 ScorePerTime=0.0 ScoreLossPerDamageTaken=0.0 ScoreLossPerDeath=0.0 ScoreLossPerMidairDirected=0.0 ScoreLossPerAnyDirected=0.0 ScoreMultAccuracy=true ScoreMultDamageEfficiency=false ScoreMultKillEfficiency=false GameTag=Apex WeaponHeroTag=R-99 DifficultyTag=3 AuthorsTag= BlockHitMarkers=false BlockHitSounds=false BlockMissSounds=true BlockFCT=false Description=R-99 against a hard to hit target. GameVersion=2.0.1.2 ScorePerDistance=0.0 MBSEnable=false MBSTime1=0.25 MBSTime2=0.5 MBSTime3=0.75 MBSTime1Mult=1.0 MBSTime2Mult=2.0 MBSTime3Mult=3.0 MBSFBInstead=false MBSRequireEnemyAlive=false LockFOVRange=false LockedFOVMin=60.0 LockedFOVMax=120.0 LockedFOVScale=Clamped Horizontal [Aim Profile] Name=Default MinReactionTime=0.3 MaxReactionTime=0.4 MinSelfMovementCorrectionTime=0.001 MaxSelfMovementCorrectionTime=0.05 FlickFOV=30.0 FlickSpeed=1.5 FlickError=15.0 TrackSpeed=3.5 TrackError=3.5 MaxTurnAngleFromPadCenter=75.0 MinRecenterTime=0.3 MaxRecenterTime=0.5 OptimalAimFOV=30.0 OuterAimPenalty=1.0 MaxError=40.0 ShootFOV=15.0 VerticalAimOffset=0.0 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 AimingStyle=Original ScanSpeedMultiplier=1.0 MaxSeekPitch=30.0 MaxSeekYaw=30.0 AimingSpeed=5.0 MinShootDelay=0.3 MaxShootDelay=0.6 [Bot Profile] Name=Apex_bot_close DodgeProfileNames=Short Strafes Apex;Close Very Short Strafes;Circle Strafe DodgeProfileWeights=1.0;1.0;1.0 DodgeProfileMaxChangeTime=5.0 DodgeProfileMinChangeTime=1.0 WeaponProfileWeights=1.0;1.0;1.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=Default;Default;Default;Default;Default;Default;Default;Default WeaponSwitchTime=3.0 UseWeapons=true CharacterProfile=Apex purple armor no gun SeeThroughWalls=false NoDodging=false NoAiming=false AbilityUseTimer=0.1 UseAbilityFrequency=1.0 UseAbilityFreqMinTime=0.3 UseAbilityFreqMaxTime=0.6 ShowLaser=false LaserRGB=X=0.810 Y=0.200 Z=0.000 LaserAlpha=1.0 [Character Profile] Name=Apex purple armor R-99 MaxHealth=200.0 WeaponProfileNames=;R99;;;;;; MinRespawnDelay=1.0 MaxRespawnDelay=5.0 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=2.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=4.0 MovementType=Base MaxSpeed=1200.0 MaxCrouchSpeed=500.0 Acceleration=7000.0 AirAcceleration=16000.0 Friction=4.0 BrakingFrictionFactor=2.0 JumpVelocity=800.0 Gravity=3.0 AirControl=0.25 CanCrouch=true CanPogoJump=false CanCrouchInAir=true CanJumpFromCrouch=false EnemyBodyColor=X=0.771 Y=0.000 Z=0.000 EnemyHeadColor=X=1.000 Y=1.000 Z=1.000 TeamBodyColor=X=1.000 Y=0.888 Z=0.000 TeamHeadColor=X=1.000 Y=1.000 Z=1.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=0.0 MainBBType=Cuboid MainBBHeight=260.0 MainBBRadius=50.0 MainBBHasHead=true MainBBHeadRadius=18.0 MainBBHeadOffset=0.0 MainBBHide=true ProjBBType=Cylindrical ProjBBHeight=260.0 ProjBBRadius=55.0 ProjBBHasHead=true ProjBBHeadRadius=45.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.2 JetpackFullFuelTime=4.0 JetpackFuelIncPerSec=1.0 JetpackFuelRegensInAir=false JetpackThrust=6000.0 JetpackMaxZVelocity=400.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=false AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.5 AllowBufferedJumps=true BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=0.75 HealthRegainedonkill=0.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.0 ThirdPersonCamera=false TPSArmLength=300.0 TPSOffset=X=0.000 Y=150.000 Z=150.000 BrakingDeceleration=2048.0 VerticalSpawnOffset=0.0 TerminalVelocity=0.0 CharacterModel=Meso CharacterSkin=Default SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=false ViewBobTime=0.0 ViewBobAngleAdjustment=0.0 ViewBobCameraZOffset=0.0 ViewBobAffectsShots=false IsFlyer=false FlightObeysPitch=false FlightVelocityUp=800.0 FlightVelocityDown=800.0 [Character Profile] Name=Apex purple armor no gun MaxHealth=200.0 WeaponProfileNames=;;;;;;; MinRespawnDelay=1.0 MaxRespawnDelay=5.0 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=2.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=4.0 MovementType=Base MaxSpeed=1200.0 MaxCrouchSpeed=500.0 Acceleration=7000.0 AirAcceleration=16000.0 Friction=4.0 BrakingFrictionFactor=2.0 JumpVelocity=800.0 Gravity=3.0 AirControl=0.25 CanCrouch=true CanPogoJump=false CanCrouchInAir=true CanJumpFromCrouch=false EnemyBodyColor=X=0.771 Y=0.000 Z=0.000 EnemyHeadColor=X=1.000 Y=1.000 Z=1.000 TeamBodyColor=X=1.000 Y=0.888 Z=0.000 TeamHeadColor=X=1.000 Y=1.000 Z=1.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=0.0 MainBBType=Cuboid MainBBHeight=260.0 MainBBRadius=55.0 MainBBHasHead=true MainBBHeadRadius=18.0 MainBBHeadOffset=0.0 MainBBHide=true ProjBBType=Cylindrical ProjBBHeight=260.0 ProjBBRadius=55.0 ProjBBHasHead=true ProjBBHeadRadius=45.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.2 JetpackFullFuelTime=4.0 JetpackFuelIncPerSec=1.0 JetpackFuelRegensInAir=false JetpackThrust=6000.0 JetpackMaxZVelocity=400.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=[ADM]Sprint.abilsprint;;; HideWeapon=false AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=0.75 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.5 AllowBufferedJumps=true BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=1.0 HealthRegainedonkill=0.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.0 ThirdPersonCamera=false TPSArmLength=300.0 TPSOffset=X=0.000 Y=150.000 Z=150.000 BrakingDeceleration=2048.0 VerticalSpawnOffset=0.0 TerminalVelocity=0.0 CharacterModel=Meso CharacterSkin=Default SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=false ViewBobTime=0.0 ViewBobAngleAdjustment=0.0 ViewBobCameraZOffset=0.0 ViewBobAffectsShots=false IsFlyer=false FlightObeysPitch=false FlightVelocityUp=800.0 FlightVelocityDown=800.0 [Dodge Profile] Name=Short Strafes Apex MaxTargetDistance=700.0 MinTargetDistance=600.0 ToggleLeftRight=true ToggleForwardBack=false MinLRTimeChange=0.2 MaxLRTimeChange=0.5 MinFBTimeChange=0.2 MaxFBTimeChange=0.5 DamageReactionChangesDirection=false DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=50.0 DamageReactionResetTimer=0.5 JumpFrequency=0.0 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.3 TargetStrafeOverride=Ignore TargetStrafeMinDelay=0.125 TargetStrafeMaxDelay=0.25 MinProfileChangeTime=0.0 MaxProfileChangeTime=0.0 MinCrouchTime=0.1 MaxCrouchTime=0.6 MinJumpTime=0.3 MaxJumpTime=0.6 LeftStrafeTimeMult=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.5 BlockedMovementReactionMin=0.125 BlockedMovementReactionMax=0.2 WaypointLogic=Ignore WaypointTurnRate=200.0 MinTimeBeforeShot=0.15 MaxTimeBeforeShot=0.25 IgnoreShotChance=0.0 ForwardTimeMult=1.0 BackTimeMult=1.0 DamageReactionChangesFB=false [Dodge Profile] Name=Close Very Short Strafes MaxTargetDistance=700.0 MinTargetDistance=0.0 ToggleLeftRight=true ToggleForwardBack=false MinLRTimeChange=0.1 MaxLRTimeChange=0.2 MinFBTimeChange=0.2 MaxFBTimeChange=0.5 DamageReactionChangesDirection=false DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=50.0 DamageReactionResetTimer=0.5 JumpFrequency=0.0 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.0 TargetStrafeOverride=Ignore TargetStrafeMinDelay=0.125 TargetStrafeMaxDelay=0.25 MinProfileChangeTime=0.5 MaxProfileChangeTime=0.9 MinCrouchTime=0.3 MaxCrouchTime=0.6 MinJumpTime=0.3 MaxJumpTime=0.6 LeftStrafeTimeMult=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.5 BlockedMovementReactionMin=0.125 BlockedMovementReactionMax=0.2 WaypointLogic=Ignore WaypointTurnRate=200.0 MinTimeBeforeShot=0.15 MaxTimeBeforeShot=0.25 IgnoreShotChance=0.0 ForwardTimeMult=1.0 BackTimeMult=1.0 DamageReactionChangesFB=false [Dodge Profile] Name=Circle Strafe MaxTargetDistance=1245.901611 MinTargetDistance=373.770477 ToggleLeftRight=true ToggleForwardBack=false MinLRTimeChange=0.2 MaxLRTimeChange=0.5 MinFBTimeChange=0.2 MaxFBTimeChange=0.5 DamageReactionChangesDirection=true DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=0.0 DamageReactionResetTimer=0.1 JumpFrequency=0.5 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.0 TargetStrafeOverride=Oppose TargetStrafeMinDelay=0.125 TargetStrafeMaxDelay=0.25 MinProfileChangeTime=0.0 MaxProfileChangeTime=0.0 MinCrouchTime=0.3 MaxCrouchTime=0.6 MinJumpTime=0.3 MaxJumpTime=0.6 LeftStrafeTimeMult=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.5 BlockedMovementReactionMin=0.125 BlockedMovementReactionMax=0.2 WaypointLogic=Ignore WaypointTurnRate=200.0 MinTimeBeforeShot=0.15 MaxTimeBeforeShot=0.25 IgnoreShotChance=0.0 ForwardTimeMult=1.0 BackTimeMult=1.0 DamageReactionChangesFB=false [Weapon Profile] Name=R99 Type=Hitscan ShotsPerClick=1 DamagePerShot=11.0 KnockbackFactor=0.0 TimeBetweenShots=0.05556 Pierces=false Category=FullyAuto BurstShotCount=1 TimeBetweenBursts=0.5 ChargeStartDamage=10.0 ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000 ChargeTimeToAutoRelease=2.0 ChargeTimeToCap=1.0 ChargeMoveSpeedModifier=1.0 MuzzleVelocityMin=X=2000.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=2000.000 Y=0.000 Z=0.000 InheritOwnerVelocity=0.0 OriginOffset=X=0.000 Y=0.000 Z=0.000 MaxTravelTime=5.0 MaxHitscanRange=100000.0 GravityScale=1.0 HeadshotCapable=true HeadshotMultiplier=1.5 MagazineMax=27 AmmoPerShot=1 ReloadTimeFromEmpty=0.6 ReloadTimeFromPartial=0.1 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=11.0 DelayBeforeShot=0.0 ProjectileGraphic=Ball VisualLifetime=10.0 BounceOffWorld=false BounceFactor=0.0 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=1.0 CanAimDownSight=true ADSZoomDelay=0.1 ADSZoomSensFactor=1.0 ADSMoveFactor=0.86 ADSStartDelay=0.0 ShootSoundCooldown=0.0001 HitSoundCooldown=0.0001 HitscanVisualOffset=X=0.000 Y=0.000 Z=-80.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=0.0 RecoilNegatable=false DecalType=1 DecalSize=10.0 DelayAfterShooting=0.0 BeamTracksCrosshair=true AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=0.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=6.0 TaggingDuration=0.0 TaggingMaxFactor=1.0 TaggingHitFactor=1.0 RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=true AimPunchAmount=0.0 AimPunchResetTime=0.1 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=true MinimumDecelVelocity=0.0 PSRManualNegation=true PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=27 CancelReloadOnKill=true FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=No Scope ADSFOVOverride=78.260002 ADSFOVScale=Apex Legends ADSAllowUserOverrideFOV=true IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.1 WeaponModel=Machine Pistol WeaponAnimation=Primary UseIncReload=false IncReloadStartupTime=0.0 IncReloadLoopTime=0.0 IncReloadAmmoPerLoop=1 IncReloadEndTime=0.0 IncReloadCancelWithShoot=true WeaponSkin=Default ProjectileVisualOffset=X=0.000 Y=0.000 Z=0.000 SpreadDecayDelay=0.0 ReloadBeforeRecovery=true 3rdPersonWeaponModel=Pistol 3rdPersonWeaponSkin=Default ParticleMuzzleFlash=Surge Pistols ParticleWallImpact=None ParticleBodyImpact=None ParticleProjectileTrail=None ParticleHitscanTrace=Bullet ParticleMuzzleFlashScale=1.0 ParticleWallImpactScale=1.0 ParticleBodyImpactScale=1.0 ParticleProjectileTrailScale=1.0 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=0.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=1.0,1.0,-1.0,0.0 SpreadSCA=1.0,1.0,-1.0,0.0 SpreadMSA=1.0,1.0,-1.0,0.0 SpreadMCA=1.0,1.0,-1.0,0.0 SpreadSSH=1.0,1.0,-1.0,0.0 SpreadSCH=1.0,1.0,-1.0,0.0 SpreadMSH=1.0,1.0,-1.0,0.0 SpreadMCH=1.0,1.0,-1.0,0.0 MaxRecoilUp=0.0 MinRecoilUp=0.0 MinRecoilHoriz=0.0 MaxRecoilHoriz=0.0 FirstShotRecoilMult=1.0 RecoilAutoReset=false TimeToRecoilPeak=0.05 TimeToRecoilReset=0.35 AAMode=0 AAPreferClosestPlayer=false AAAlpha=0.5 AAMaxSpeed=1.0 AADeadZone=0.0 AAFOV=30.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=false TriggerBotDelay=0.0 TriggerBotFOV=1.0 StickyLock=false HeadLock=false VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=true PSRLoopStartIndex=0 PSRViewRecoilTracking=1.0 PSRCapUp=90.0 PSRCapRight=90.0 PSRCapLeft=90.0 PSRTimeToPeak=0.17 PSRResetDegreesPerSec=38.0 PSR0=0.3655,0.1275 PSR1=0.3655,-0.0085 PSR2=0.3145,-0.1785 PSR3=0.51,0.136 PSR4=0.714,0.2125 PSR5=0.5865,0.2125 PSR6=0.527,-0.2125 PSR7=0.4845,0.1955 PSR8=0.493,-0.017 PSR9=0.442,-0.221 PSR10=0.4165,-0.3485 PSR11=0.3655,-0.068 PSR12=0.4675,-0.1275 PSR13=0.2295,0.085 PSR14=0.051,0.374 PSR15=0.1105,0.187 PSR16=0.0595,0.3485 PSR17=0.2125,-0.3485 PSR18=0.0,-0.391 PSR19=0.1105,-0.4165 PSR20=0.102,-0.289 PSR21=0.1275,-0.374 PSR22=0.051,0.2805 PSR23=0.0085,0.5015 PSR24=-0.0085,0.4165 PSR25=-0.0085,0.2295 UsePerBulletSpread=false PBS0=0.0,0.0 [Sprint Ability Profile] Name=[ADM]Sprint MaxCharges=1.0 ChargeTimer=0.1 ChargesRefundedOnKill=0.0 DelayAfterUse=0.0 FullyAuto=false AbilityDuration=0.0 BlockAttackWhileSprinting=false AbilityBlockedWhenAttacking=true SpeedModifier=1.333333 45DegreeSprint=true 90DegreeSprint=false 135DegreeSprint=false 180DegreeSprint=false TapToSprint=true Block45DegreesWhenSprinting=false AIUseInCombat=true AIUseOutOfCombat=true AIUseOnGround=true AIUseInAir=false AIReuseTimer=0.1 AIMinSelfHealth=0.0 AIMaxSelfHealth=100.0 AIMinTargHealth=0.0 AIMaxTargHealth=100.0 AIMinTargDist=250.0 AIMaxTargDist=10000.0 AIMaxTargFOV=90.0 AIDamageReaction=true AIDamageReactionIgnoreChance=0.0 AIDamageReactionMinDelay=0.18 AIDamageReactionMaxDelay=0.25 AIDamageReactionCooldown=2.0 AIDamageReactionThreshold=1.0 AIDamageReactionResetTimer=0.1 [Map Data] reflex map version 8 global entity type WorldSpawn String32 targetGameOverCamera end UInt8 playersMin 1 UInt8 playersMax 16 brush vertices -576.000000 0.000000 256.000000 448.000000 0.000000 256.000000 448.000000 0.000000 -768.000000 -576.000000 0.000000 -768.000000 -576.000000 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errcatch(-1,"stop");mode(2);// Exa 1.13 ; ; // Given data V1 = 12;// in V V2 = 0.3;// in V V_o = V1-V2;// in V disp(V_o,"The output voltage in V is"); exit();
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Bt=12.5*10^6 Bc=200*10^3 Ns=8 N=Bt/Bc Ns=8 Nu=N*Ns K=4//frequency reuse factor SysC=Nu/K//system capacity M=(Bt/Bc)*Ns*(1/K)//system capacity using alternate method disp(SysC,'System capacity per cell in (users/cell)') disp(M,'System capacity per cell,M,in (users/cell) using alternate method')
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//Variable Declaration EIRP1=34 //desired carrier EIRP from satellite(dB) G1=44 // ground station receiving antenna gain(dB) G2=24.47 //Gain in desired direction(dB) EIRP2=34 //EIRP by interfering satellite(dB) PD=4 //Polarization discrimination(dB) //Calculation CIR=EIRP1-EIRP2+G1-G2+PD //Carrier to Interference ratio(dB) //Result printf("The Carrier to interfernce ratio at the ground receiving antenna is %.2f dB",CIR)
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// problem 2.14 l=60 b=9 w=16*1000000 w1=160*1000 y=6 q=3 s.p=10104 i=0.75*l*b*b*b/12 v=w/s.p bm=i/v gm=(w1*y)/(w*tand(q)) mcd=2-bm cogd=gm+mcd disp(gm,"metacentric height") disp(cogd,"position of centre of gravity below the water line")
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//Chemical Engineering Thermodynamics //Chapter 6 //Thermodynamic Relations clear; clc; //Given //The chapter does not contain any example which involve numerical computation //end
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<cmd> ../build/42sh</cmd> <ref> bash</ref> <stdin> while ! ls; do while ! ls; do while ! ls; do while ! ls; do echo a ne pas ecrire; done; done; done; done; echo a ecrire; </stdin>
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clc m=220/60; //kg/s C1=320; //m/s p1=6*10^5; //N/m^2 u1=2000*10^3; //J/kg v1=0.36; //m^3/kg C2=140; //m/s p2=1.2*10^5; //N/m^2 u2=1400*10^3; //J/kg v2=1.3; //m^3/kg Q=100*10^3; //J/s W=(m*[(u1-u2)+ (p1*v1 - p2*v2) + (C1^2-C2^2)/2] -Q)/10^6; disp("power capacity of the system = ") disp(W) disp("MW")
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//identificação de sistemas utilizando LMS clear; clc; rand("normal"); N = 2000; hn = [1.2 0.8 0.6]; sigma1 = 0.2; E = rand(1,N); xn = filter(hn,1,E)'; W = [1 2 3]; n = sigma1*rand(1,N); rx = xcorr(xn,2,'biased'); Rx = [rx(3:5) rx(2:4) rx(1:3)]; tr = Rx(1,1)+Rx(2,2)+Rx(3,3); [Q,lambda]=spec(Rx); lambdamax=max(lambda); // Computacao iterativa c = 0.1 mi = c/(2*lambdamax+tr); wn = [0 0 0]'; // filtro unitario inicial d = filter(W,1,xn)+n'; w = zeros(3,N); xb = [0 0 0]'; for n=1:length(xn) xb = [xn(n);xb(1:2)]; yn = wn'*xb; y(n) = yn; e(n) = d(n)-y(n); // calculo do grad estimado grade = -2*e(n)*xb; wn = wn - mi*grade; w(:,n) = wn end plot2d(w');
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// Example 2.9 // Calculation of Core radius // Page no 481 clc; clear; //Given data lambda=0.85*10^-6; // Wavelength of fiber delta=0.015; // Relative refractive index n1=1.48; // Refractive index of core v=2.403; // Normalized frequency for single mode fiber // Computation of core radius a=v*lambda/(2*%pi*n1*sqrt(2*delta)); a=a*10^6; //Displaying result in the command window printf("\n Radius of core (in micrometer) = %0.1f ",a);
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Chapter4_Example4.sce
clc clear //Input data w=[5000,5100]//Wavelengths of light in Armstrongs N=6000//Number of lines drawn on the grating per cm n=1//Order of diffraction F=1//Focal length of the lens in m //Calculations q1=asind(N*100*n*w(1)*10^-10)//Angle of diffraction for D1 line in degrees q2=asind(N*100*n*w(2)*10^-10)//Angle of diffraction for D1 line in degrees x=F*(tand(q2)-tand(q1))*1000//Seperation of the two lines in mm //Output printf('Seperation of two lines in the first order spectrum is %3.1f mm',x)
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function [tabla]= diferencias(X,Y) // make table of divided differences n=length(x); // Cantidad de puntos. tabla=zeros(n,n); //Defino una matriz de ceros. La dimension nos la da la cantidad de puntos. tabla(:,1)=Y; //El primer valor va directo por definicion. for j=2:n //Defino dos punteros for i=j:n tabla(i,j)=(tabla(i,j-1)-tabla(i-1,j-1))/(X(i)-X(i-j+1)); //Realizo diferencias divididas hacia adelante. end end endfunction;
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d1=6//inch d2=4//inches a=3//lb/inch^2(p1-p2) s=0.9//specific gravity of oil
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clear all; clc; // A Textbook on HEAT TRANSFER by S P SUKHATME // Chapter 2 // Heat Conduction in Solids // Example 2.9 // Page 51 printf("Example 2.9, Page 51 \n\n") k = 330; //thermal conductivity in W/m K a = 95*10^(-6); //thermal expansion coefficient R = 0.01; //radius in meters To = 77; //temperature in kelvins Tf = 273+50; //temperature in kelvins theta1 = To - Tf; T = 273+10; //temperature in kelvins theta = T - Tf; h = 20; //heat transfer coefficient in W/m^2 K printf("\n Theta1 = %d K",theta1); printf("\n Theta = %d K ",theta); printf("\n v/A = %.3f m",R/2); printf("\n k/a = %.4f*10^(6) J/m^3 K",(k/a)*10^(-6)); time = (k/a)*(R/2)/h*log(theta1/theta); printf("\n Time taken by the rod to heat up = %.1f secs",time); Bi = h*R/k; printf("\n Biot number Bi = %.2f*10^(-4) ",Bi*10^4); printf("\n Since Biot number is much less than 0.1,therefore assumption that internal temperature gradients are negligible is a good one");
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// scilab Code Exa 18.12 turbo prop Gas Turbine Engine Ti=268.65; // in Kelvin n_C=0.8; // Compressor Efficiency c1=85; // entry velocity in m/s m=50; // mass flow rate of air in kg/s R=287; gamma=1.4; // Specific Heat Ratio cp=1.005; // Specific Heat at Constant Pressure in kJ/(kgK) u=500/3.6; // speed of a turbo prop aircraft in m/s delT=225; // temperature rise through the compressor(T02-T01) in K pi=.701; // Initial Pressure in bar n_D=0.88; // inlet diffuser efficiency a_i=sqrt(gamma*R*Ti); Mi=u/a_i; Toi_i=1/0.965; // (Toi/Ti)from isentropic flow gas tables at Mi and gamma values T01=Ti*Toi_i; T1=T01-(0.5*(c1^2)/(cp*1e3)); //part(a) T1s_i=1+n_D*((T1/Ti)-1); // (T1s/Ti)isentropic temperature ratio through the diffuser p1_i=T1s_i^(gamma/(gamma-1)); // (p1s/pi)isentropic pressure ratio p1=p1_i*pi; delp_D=p1-pi; disp("bar",delp_D,"(a)isentropic pressure rise through the diffuser is") // part(b) compressor pressure ratio T02s=T01+(delT*n_C); r_oc=(T02s/T01)^(gamma/(gamma-1)); //compressor pressure ratio(p02/p01) disp(r_oc,"(b)compressor pressure ratio is") // part(c) P=m*cp*delT; disp("MW",P*1e-3,"(c)power required to drive the compressor is")
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errcatch(-1,"stop");mode(2);//Caption: SNR //Example 4.27.i //page no 200 //Find Signal to quantization noise ratio ; ; Nq=127.15*10^-6 Meansignal=2; P=Meansignal/1; SNR=P/Nq; SNRq=10*log10(SNR); disp("dB",SNRq,"Signal to quantization noise ratio"); exit();
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response-model.tst
${ using Typewriter.Extensions.Types; using System.Text.RegularExpressions; static string debugInfo = ""; string PrintDebugInfo(Class c){ return debugInfo; } Template(Settings settings) { settings. IncludeProject("Jering.VectorArtKit.WebApi"). IncludeProject("Jering.Mvc"); settings.OutputFilenameFactory = file => { return PascalToKebab($"{file.Classes.First().Name}.ts"); }; } static string PascalToKebab(string value){ string extensionAdded = value.Replace("ResponseModel", ".response-model"); string dashesAdded = Regex.Replace( extensionAdded, "(?<!^)([A-Z])", "-$1", RegexOptions.Compiled); return dashesAdded .Trim() .ToLower(); } static List<string> ImportedInterfaces = new List<string>(); // Adds import statement for property type if necessary static string ImportInterface(Property property){ string interfaceName = TypeExtensions.ClassName(property.Type); if(!ImportedInterfaces.Contains(interfaceName)) { ImportedInterfaces.Add(interfaceName); return $"import {{{interfaceName}}} from './{PascalToKebab(interfaceName)}';"; } else { return null; } } static List<Type> AddedTypes = new List<Type>(); IEnumerable<Type> DefinedTypes(Class c) { AddedTypes.Clear(); List<Type> result = new List<Type>(); GetDependencies(c, null, result); return result; } void GetDependencies(Class root, Type type, List<Type> types){ // Prevent duplicate interfaces if(AddedTypes.Any(t => type != null && t.Name == type.Name)){ return; } else if(type != null) { AddedTypes.Add(type); types.Add(type); } PropertyCollection properties = type == null ? root.Properties : type.Properties; IEnumerable<Type> dependencies = properties. Where(p => p.Type.Unwrap().IsDefined && !p.Type.Unwrap().IsEnumerable). Select(p => p.Type.Unwrap()); foreach(Type t in dependencies){ GetDependencies(null, t, types); } } } $Classes(*ResponseModel)[ export interface $Name {$Properties[ $name?: $Type;] } $DefinedTypes[ export interface $Name { $Properties[ $name?: $Type;] }] $PrintDebugInfo ]
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//ex3.5 V_Z=5.1; I_ZT=49*10^-3; I_ZK=1*10^-3; Z_Z=7; R=100; P_D_max=1; //At I_ZK, output voltage V_out=V_Z-(I_ZT-I_ZK)*Z_Z; V_IN_min=I_ZK*R+V_out; I_ZM=P_D_max/V_Z; //at I_ZM, output voltage V_out=V_Z+(I_ZM-I_ZT)*Z_Z; V_IN_max=I_ZM*R+V_out; disp(V_IN_max,'maximum input voltage in volts that can be regulated by the zener diode') disp(V_IN_min,'minimum input voltage in volts that can be regulated by the zener diode')
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11_3_soln.sce
clc; pathname=get_absolute_file_path('11_3_soln.sce') filename=pathname+filesep()+'11_3_data.sci' exec(filename) // Solution: // heat generation rate, kW=((p*10^5)*Q)/1000; //kW // oil flow-rate, Q_kg_s=895*Q; //kg/s // temperature increase, T_increase=kW/(1.8*Q_kg_s); //deg C // downward oil temperature, T_downward=T_oil+T_increase; //deg C // Results: printf("\n Results: ") printf("\n The downstream oil temperature is %.1f deg C.",T_downward)
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function [L,U]=mylu3b(A) n=size(A,1) for k=1:n-1 for i=k+1:n m(i,k)=A(i,k)/A(k,k) b(i)=b(i)-m(i,k)*b(k) for j=k+1:n A(i,j)=A(i,j)-m(i,k)*A(k,j); end end end //calcul de U par la fonction prédéfinie U=triu(A) //calcul de L par la fonction prédéfinie L=tril(A) endfunction disp('L=',L) disp('U=',U)
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tagrename.tst
## Tag renaming test read <sample1.fi tag annotated rename foobar write -
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// Calculate voltage gain Av // Basic Electronics // By Debashis De // First Edition, 2010 // Dorling Kindersley Pvt. Ltd. India // Example 7-57 in page 359 clear; clc; close; // Given data gm=2*10^-3; // Transconductance in mA/V rd=10*10^3; // Dynamic resistance in K-ohms C=0.025*10^-6; // Capacitance in microF // Calculation Rl=(30*30)/(30+30); Av=(-gm*rd*Rl*10^3)/(Rl+rd); f1=1/(2*%pi*37.5*10^3*C); Avl=Av/sqrt(1+(f1/(5*10^3))^2); printf("(a)Av = %0.0f\n(b)Avl = %0.2f",Av,Avl); // Result // (a) Av = -30 // (b) Avl = -29.94
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// Exa 17.4 //To calculate the cell radius. clc; clear all; Pt=36;//Base station transmitted power in dBm Pms=24;//mobile station transmitted power in dBm Nms=8;//mobile station noise figure in dB Nbs=5;//Base station nise figure in dB Ga=18;//Base station transmit and receive antenna gain in dBi Gm=0;//Mobile antenna gain in dBi SNR=12;// in dB Lc_TX=5;//BS transmit antenna cable, connector, and filter losses in dB Lc_RX=2;//BS receiver antenna cable, connector, and filter losses in dB Bodyloss=3;// Body losses at mobile fading=10.2;// in dB ThermalNoise=-174;// in dBm/Hz Gdiversity=5;//Antenna diversity gain at BS in dB //Assuming standard value of RF channel as RFch=200*10^3; //in Hz //solution N=ThermalNoise+10*log10(RFch)+Nms; Smin=N+SNR; Smean=Smin+fading+Bodyloss; Lp=Pt-Lc_TX+Ga-Smean; N1=ThermalNoise+10*log10(RFch)+Nbs; Smin=N1+SNR-Gdiversity; Smean1=Smin+fading+Bodyloss; Lp1=Pms-Smean1+Ga-Lc_RX; disp("Using uplink path loss and Hata model to calculate cell radius"); R=10^((Lp1-133.2)/33.8); printf(' Cell radius is %.1f km \n',R);
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Ex4_2.sce
//Exa 4.2 clc;clear;close; format('v',6); Lt=3000;//kW//Total Load pf=0.8;//Power factor Lagging I=150;//A ZA=0.4+%i*12;//ohm//synchronous impedence ZB=0.5+%i*10;//ohm//synchronous impedence Vt=6.6;//kV//Terminal Voltage L=Lt/2;//kW//Load supplied by each machine LA=L;//kW LB=L;//kW //LB=sqrt(3)*Vt*IB*cosd(theta_B); theta_B=acosd(LB/sqrt(3)/Vt/I);//degree IB=I*(cosd(theta_B)-%i*sind(theta_B));//A I_total=Lt/sqrt(3)/Vt/pf;//A//Total Current IA_plus_IB=I_total*(0.8-%i*0.6);//A IA=IA_plus_IB-IB;//A cos_thetaA=real(IA)/abs(IA);//lagging power factor EA=Vt/sqrt(3)+IA*ZA/1000;//kV per phase del_A=atand(imag(EA)/real(EA));//degree//Load Angle emf_A=abs(EA);//kV per phase//Induced emf of machine A EB=Vt/sqrt(3)+IB*ZB/1000;//kV per phase del_B=atand(imag(EB)/real(EB));//degree//Load Angle emf_B=abs(EB);//kV per phase//Induced emf of machine A IA=abs(IA);//A disp(IA,"Current on machine A(A) : "); pfA=cos_thetaA;//power factor disp(pfA,"Lagging power factor of machine A"); format('v',5); disp(emf_A,"Induced emf of machine A(kV per phase)"); disp(del_A,"Load angle of machine A(degree)"); disp(del_B,"Load angle of machine B(degree)"); disp(emf_B,"Induced emf of machine B(kV per phase)"); //Answer in the textbook is not accurate.
6b5938d72355a97621be76495a842c7b0f0c9f68
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/macros/autoCorrelator.sci
991b903c6de5f815737df12d2183d611abc566f9
[]
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gursimarsingh/FOSSEE_Image_Processing_Toolbox
76c9d524193ade302c48efe11936fe640f4de200
a6df67e8bcd5159cde27556f4f6a315f8dc2215f
refs/heads/master
2021-01-22T02:08:45.870957
2017-01-15T21:26:17
2017-01-15T21:26:17
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sci
autoCorrelator.sci
function relation = autoCorrelator(inputMatrix) //Calculate 2-D auto correlation of input matrix // //Calling Sequence // relation=autoCorrelator(inputMatrix) // //Parameters // inputMatrix: input matrix to calculate auto correlation // //Description //This function computes 2-D auto correlation of input matrix // // Examples // rel = autoCorrelator([3 1;2 4]) // examples of use [lhs rhs]=argn(0); if rhs<1 then error(msprintf("Wrong arguments: Need atleast one argument")) end [r,c,channels] = size(inputMatrix); if channels<> 1 then error(msprintf("Auto correlator function do not support more than two dimensions")) elseif type(inputMatrix)<> 1 error(msprintf("Auto correlator function do not support input type %s",typeof(inputMatrix))) end Rep = zeros(r + r*2-2, c + c*2-2); for x = r : r+r-1 for y = c : c+c-1 Rep(x,y) = inputMatrix(x-r+1, y-c+1); end end conjMatrix=conj(inputMatrix); //(mROw,mCols)- It indicates middle value of the output matrix relation = zeros(r+r-1,c+c-1); //output matrix //calculating only half of the output matrix for x = 1 : r+r-1 for y = 1 : c+c-1 for i = 1 : r for j = 1 : c relation(x, y) = relation(x, y) + (Rep(x+i-1, y+j-1) * conjMatrix(i, j)); end end end end //Copying remainig values endfunction
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/test/X06.prev.tst
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X06.prev.tst
# orig Korneck-minus.X06 (6*m^3*t*f+t*(t-m)*(m^4+m^2*t^2+t^4)+3*t*(t+m)*f^2)^3 # flat Korneck-minus.X06 3*f^2*m*t + 6*f*m^3*t - m^5*t + 3*f^2*t^2 + m^4*t^2 - m^3*t^3 + m^2*t^4 - m*t^5 + t^6 # merg Korneck-minus.X06 6*x_y_z^4 + 6*x_y_z^5 # orig Korneck-minus.X06 +(6*m^3*t*f-t*(t-m)*(m^4+m^2*t^2+t^4)-3*t*(t+m)*f^2)^3 # flat Korneck-minus.X06 - 3*f^2*m*t + 6*f*m^3*t + m^5*t - 3*f^2*t^2 - m^4*t^2 + m^3*t^3 - m^2*t^4 + m*t^5 - t^6 # merg Korneck-minus.X06 - 6*x_y_z^4 + 6*x_y_z^5 # orig Korneck-minus.X06 +(-6*t^3*m*f+m*(m-t)*(m^4+m^2*t^2+t^4)+3*m*(m+t)*f^2)^3 # flat Korneck-minus.X06 3*f^2*m^2 + m^6 + 3*f^2*m*t - m^5*t + m^4*t^2 - 6*f*m*t^3 - m^3*t^3 + m^2*t^4 - m*t^5 # merg Korneck-minus.X06 6*x_y_z^4 - 6*x_y_z^5 # orig Korneck-minus.X06 -(6*t^3*m*f+m*(m-t)*(m^4+m^2*t^2+t^4)+3*m*(m+t)*f^2)^3 # flat Korneck-minus.X06 3*f^2*m^2 + m^6 + 3*f^2*m*t - m^5*t + m^4*t^2 + 6*f*m*t^3 - m^3*t^3 + m^2*t^4 - m*t^5 # merg Korneck-minus.X06 6*x_y_z^4 + 6*x_y_z^5 # poly Korneck-minus.X06 0 000018 [3,4,5,6] Korneck-minus.X06 factor=12 parm= [1,2,1] 000018 [3,4,5,6] Korneck-minus.X06 factor=12 parm= [-1,2,1] 000032 [1,9,10,12] Korneck-minus.X06 factor=12 parm= [1,-2,1] 000032 [1,9,10,12] Korneck-minus.X06 factor=12 parm= [-1,-2,1] 000032 [1,9,10,12] Korneck-minus.X06 factor=12 parm= [1,2,-1] 000032 [1,9,10,12] Korneck-minus.X06 factor=12 parm= [-1,2,-1] 000018 [3,4,5,6] Korneck-minus.X06 factor=12 parm= [1,-2,-1] 000018 [3,4,5,6] Korneck-minus.X06 factor=12 parm= [-1,-2,-1] 000140 [27,30,37,46] Korneck-minus.X06 factor=3 parm= [2,2,1] 000140 [27,30,37,46] Korneck-minus.X06 factor=3 parm= [-2,2,1] 000164 [15,42,49,58] Korneck-minus.X06 factor=3 parm= [2,-2,1] 000164 [15,42,49,58] Korneck-minus.X06 factor=3 parm= [-2,-2,1] 000164 [15,42,49,58] Korneck-minus.X06 factor=3 parm= [2,2,-1] 000164 [15,42,49,58] Korneck-minus.X06 factor=3 parm= [-2,2,-1] 000140 [27,30,37,46] Korneck-minus.X06 factor=3 parm= [2,-2,-1] 000140 [27,30,37,46] Korneck-minus.X06 factor=3 parm= [-2,-2,-1] 000018 [3,4,5,6] Korneck-minus.X06 factor=12 parm= [1,1,2] 000018 [3,4,5,6] Korneck-minus.X06 factor=12 parm= [-1,1,2] 000032 [1,9,10,12] Korneck-minus.X06 factor=12 parm= [1,-1,2] 000032 [1,9,10,12] Korneck-minus.X06 factor=12 parm= [-1,-1,2] 000032 [1,9,10,12] Korneck-minus.X06 factor=12 parm= [1,1,-2] 000032 [1,9,10,12] Korneck-minus.X06 factor=12 parm= [-1,1,-2] 000018 [3,4,5,6] Korneck-minus.X06 factor=12 parm= [1,-1,-2] 000018 [3,4,5,6] Korneck-minus.X06 factor=12 parm= [-1,-1,-2] 000140 [27,30,37,46] Korneck-minus.X06 factor=3 parm= [2,1,2] 000140 [27,30,37,46] Korneck-minus.X06 factor=3 parm= [-2,1,2] 000164 [15,42,49,58] Korneck-minus.X06 factor=3 parm= [2,-1,2] 000164 [15,42,49,58] Korneck-minus.X06 factor=3 parm= [-2,-1,2] 000164 [15,42,49,58] Korneck-minus.X06 factor=3 parm= [2,1,-2] 000164 [15,42,49,58] Korneck-minus.X06 factor=3 parm= [-2,1,-2] 000140 [27,30,37,46] Korneck-minus.X06 factor=3 parm= [2,-1,-2] 000140 [27,30,37,46] Korneck-minus.X06 factor=3 parm= [-2,-1,-2] 000058 [7,14,17,20] Korneck-minus.X06 factor=12 parm= [3,2,1] 000058 [7,14,17,20] Korneck-minus.X06 factor=12 parm= [-3,2,1] 000018 [3,4,5,6] Korneck-minus.X06 factor=36 parm= [3,-2,1] 000018 [3,4,5,6] Korneck-minus.X06 factor=36 parm= [-3,-2,1] 000018 [3,4,5,6] Korneck-minus.X06 factor=36 parm= [3,2,-1] 000018 [3,4,5,6] Korneck-minus.X06 factor=36 parm= [-3,2,-1] 000058 [7,14,17,20] Korneck-minus.X06 factor=12 parm= [3,-2,-1] 000058 [7,14,17,20] Korneck-minus.X06 factor=12 parm= [-3,-2,-1] 000376 [2,83,141,150] Korneck-minus.X06 factor=4 parm= [1,3,1] 000376 [2,83,141,150] Korneck-minus.X06 factor=4 parm= [-1,3,1] 000734 [49,130,273,282] Korneck-minus.X06 factor=4 parm= [1,-3,1] 000734 [49,130,273,282] Korneck-minus.X06 factor=4 parm= [-1,-3,1] 000734 [49,130,273,282] Korneck-minus.X06 factor=4 parm= [1,3,-1] 000734 [49,130,273,282] Korneck-minus.X06 factor=4 parm= [-1,3,-1] 000376 [2,83,141,150] Korneck-minus.X06 factor=4 parm= [1,-3,-1] 000376 [2,83,141,150] Korneck-minus.X06 factor=4 parm= [-1,-3,-1] 001014 [95,229,327,363] Korneck-minus.X06 factor=2 parm= [2,3,1] 001014 [95,229,327,363] Korneck-minus.X06 factor=2 parm= [-2,3,1] 000376 [2,83,141,150] Korneck-minus.X06 factor=8 parm= [2,-3,1] 000376 [2,83,141,150] Korneck-minus.X06 factor=8 parm= [-2,-3,1] 000376 [2,83,141,150] Korneck-minus.X06 factor=8 parm= [2,3,-1] 000376 [2,83,141,150] Korneck-minus.X06 factor=8 parm= [-2,3,-1] 001014 [95,229,327,363] Korneck-minus.X06 factor=2 parm= [2,-3,-1] 001014 [95,229,327,363] Korneck-minus.X06 factor=2 parm= [-2,-3,-1] 000678 [103,140,204,231] Korneck-minus.X06 factor=4 parm= [3,3,1] 000678 [103,140,204,231] Korneck-minus.X06 factor=4 parm= [-3,3,1] 000870 [44,199,300,327] Korneck-minus.X06 factor=4 parm= [3,-3,1] 000870 [44,199,300,327] Korneck-minus.X06 factor=4 parm= [-3,-3,1] 000870 [44,199,300,327] Korneck-minus.X06 factor=4 parm= [3,3,-1] 000870 [44,199,300,327] Korneck-minus.X06 factor=4 parm= [-3,3,-1] 000678 [103,140,204,231] Korneck-minus.X06 factor=4 parm= [3,-3,-1] 000678 [103,140,204,231] Korneck-minus.X06 factor=4 parm= [-3,-3,-1] 000058 [7,14,17,20] Korneck-minus.X06 factor=12 parm= [3,1,2] 000058 [7,14,17,20] Korneck-minus.X06 factor=12 parm= [-3,1,2] 000018 [3,4,5,6] Korneck-minus.X06 factor=36 parm= [3,-1,2] 000018 [3,4,5,6] Korneck-minus.X06 factor=36 parm= [-3,-1,2] 000018 [3,4,5,6] Korneck-minus.X06 factor=36 parm= [3,1,-2] 000018 [3,4,5,6] Korneck-minus.X06 factor=36 parm= [-3,1,-2] 000058 [7,14,17,20] Korneck-minus.X06 factor=12 parm= [3,-1,-2] 000058 [7,14,17,20] Korneck-minus.X06 factor=12 parm= [-3,-1,-2] 000384 [22,75,140,147] Korneck-minus.X06 factor=4 parm= [1,3,2] 000384 [22,75,140,147] Korneck-minus.X06 factor=4 parm= [-1,3,2] 001664 [250,412,465,537] Korneck-minus.X06 factor=4 parm= [1,-3,2] 001664 [250,412,465,537] Korneck-minus.X06 factor=4 parm= [-1,-3,2] 001664 [250,412,465,537] Korneck-minus.X06 factor=4 parm= [1,3,-2] 001664 [250,412,465,537] Korneck-minus.X06 factor=4 parm= [-1,3,-2] 000384 [22,75,140,147] Korneck-minus.X06 factor=4 parm= [1,-3,-2] 000384 [22,75,140,147] Korneck-minus.X06 factor=4 parm= [-1,-3,-2] 002454 [291,502,794,867] Korneck-minus.X06 factor=1 parm= [2,3,2] 002454 [291,502,794,867] Korneck-minus.X06 factor=1 parm= [-2,3,2] 006674 [658,1743,1954,2319] Korneck-minus.X06 factor=1 parm= [2,-3,2] 006674 [658,1743,1954,2319] Korneck-minus.X06 factor=1 parm= [-2,-3,2] 006674 [658,1743,1954,2319] Korneck-minus.X06 factor=1 parm= [2,3,-2] 006674 [658,1743,1954,2319] Korneck-minus.X06 factor=1 parm= [-2,3,-2] 002454 [291,502,794,867] Korneck-minus.X06 factor=1 parm= [2,-3,-2] 002454 [291,502,794,867] Korneck-minus.X06 factor=1 parm= [-2,-3,-2] 000888 [93,242,244,309] Korneck-minus.X06 factor=4 parm= [3,3,2] 000888 [93,242,244,309] Korneck-minus.X06 factor=4 parm= [-3,3,2] 001676 [76,411,562,627] Korneck-minus.X06 factor=4 parm= [3,-3,2] 001676 [76,411,562,627] Korneck-minus.X06 factor=4 parm= [-3,-3,2] 001676 [76,411,562,627] Korneck-minus.X06 factor=4 parm= [3,3,-2] 001676 [76,411,562,627] Korneck-minus.X06 factor=4 parm= [-3,3,-2] 000888 [93,242,244,309] Korneck-minus.X06 factor=4 parm= [3,-3,-2] 000888 [93,242,244,309] Korneck-minus.X06 factor=4 parm= [-3,-3,-2] 000376 [2,83,141,150] Korneck-minus.X06 factor=4 parm= [1,1,3] 000376 [2,83,141,150] Korneck-minus.X06 factor=4 parm= [-1,1,3] 000734 [49,130,273,282] Korneck-minus.X06 factor=4 parm= [1,-1,3] 000734 [49,130,273,282] Korneck-minus.X06 factor=4 parm= [-1,-1,3] 000734 [49,130,273,282] Korneck-minus.X06 factor=4 parm= [1,1,-3] 000734 [49,130,273,282] Korneck-minus.X06 factor=4 parm= [-1,1,-3] 000376 [2,83,141,150] Korneck-minus.X06 factor=4 parm= [1,-1,-3] 000376 [2,83,141,150] Korneck-minus.X06 factor=4 parm= [-1,-1,-3] 001014 [95,229,327,363] Korneck-minus.X06 factor=2 parm= [2,1,3] 001014 [95,229,327,363] Korneck-minus.X06 factor=2 parm= [-2,1,3] 000376 [2,83,141,150] Korneck-minus.X06 factor=8 parm= [2,-1,3] 000376 [2,83,141,150] Korneck-minus.X06 factor=8 parm= [-2,-1,3] 000376 [2,83,141,150] Korneck-minus.X06 factor=8 parm= [2,1,-3] 000376 [2,83,141,150] Korneck-minus.X06 factor=8 parm= [-2,1,-3] 001014 [95,229,327,363] Korneck-minus.X06 factor=2 parm= [2,-1,-3] 001014 [95,229,327,363] Korneck-minus.X06 factor=2 parm= [-2,-1,-3] 000678 [103,140,204,231] Korneck-minus.X06 factor=4 parm= [3,1,3] 000678 [103,140,204,231] Korneck-minus.X06 factor=4 parm= [-3,1,3] 000870 [44,199,300,327] Korneck-minus.X06 factor=4 parm= [3,-1,3] 000870 [44,199,300,327] Korneck-minus.X06 factor=4 parm= [-3,-1,3] 000870 [44,199,300,327] Korneck-minus.X06 factor=4 parm= [3,1,-3] 000870 [44,199,300,327] Korneck-minus.X06 factor=4 parm= [-3,1,-3] 000678 [103,140,204,231] Korneck-minus.X06 factor=4 parm= [3,-1,-3] 000678 [103,140,204,231] Korneck-minus.X06 factor=4 parm= [-3,-1,-3] 000384 [22,75,140,147] Korneck-minus.X06 factor=4 parm= [1,2,3] 000384 [22,75,140,147] Korneck-minus.X06 factor=4 parm= [-1,2,3] 001664 [250,412,465,537] Korneck-minus.X06 factor=4 parm= [1,-2,3] 001664 [250,412,465,537] Korneck-minus.X06 factor=4 parm= [-1,-2,3] 001664 [250,412,465,537] Korneck-minus.X06 factor=4 parm= [1,2,-3] 001664 [250,412,465,537] Korneck-minus.X06 factor=4 parm= [-1,2,-3] 000384 [22,75,140,147] Korneck-minus.X06 factor=4 parm= [1,-2,-3] 000384 [22,75,140,147] Korneck-minus.X06 factor=4 parm= [-1,-2,-3] 002454 [291,502,794,867] Korneck-minus.X06 factor=1 parm= [2,2,3] 002454 [291,502,794,867] Korneck-minus.X06 factor=1 parm= [-2,2,3] 006674 [658,1743,1954,2319] Korneck-minus.X06 factor=1 parm= [2,-2,3] 006674 [658,1743,1954,2319] Korneck-minus.X06 factor=1 parm= [-2,-2,3] 006674 [658,1743,1954,2319] Korneck-minus.X06 factor=1 parm= [2,2,-3] 006674 [658,1743,1954,2319] Korneck-minus.X06 factor=1 parm= [-2,2,-3] 002454 [291,502,794,867] Korneck-minus.X06 factor=1 parm= [2,-2,-3] 002454 [291,502,794,867] Korneck-minus.X06 factor=1 parm= [-2,-2,-3] 000888 [93,242,244,309] Korneck-minus.X06 factor=4 parm= [3,2,3] 000888 [93,242,244,309] Korneck-minus.X06 factor=4 parm= [-3,2,3] 001676 [76,411,562,627] Korneck-minus.X06 factor=4 parm= [3,-2,3] 001676 [76,411,562,627] Korneck-minus.X06 factor=4 parm= [-3,-2,3] 001676 [76,411,562,627] Korneck-minus.X06 factor=4 parm= [3,2,-3] 001676 [76,411,562,627] Korneck-minus.X06 factor=4 parm= [-3,2,-3] 000888 [93,242,244,309] Korneck-minus.X06 factor=4 parm= [3,-2,-3] 000888 [93,242,244,309] Korneck-minus.X06 factor=4 parm= [-3,-2,-3]
574b451572b490f538a797b38a90a209547ad2bd
52cff1a2ef2292f8b9acf18dcfe1d4b0df75c558
/LAB 8/60002190043_SCILAB 8_IMPULSE RESPONSE.sce
b4fcf5c5504c53c464107040b4c20523ce7fd80d
[]
no_license
Hetankshi/SCILAB
692a3abc71e6686f40745d69a66e4511db244491
424d4cc3459bb535e2f6793249f6a583374820ad
refs/heads/main
2023-01-16T05:39:22.830875
2020-11-25T12:23:14
2020-11-25T12:23:14
315,916,735
0
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null
null
null
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UTF-8
Scilab
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false
267
sce
60002190043_SCILAB 8_IMPULSE RESPONSE.sce
//unit impulse func clear all; clc; close; L = 4; //Upperlimit n = -L:L; x = [zeros(1,L),1,zeros(1,L)]; b = gca(); b.y_location = "middle"; plot2d3('gnn',n,x) a=gce(); a.children(1).thickness =4; xtitle('unit impulse','n','x[n]');
e20128d938560e5e139b0c5092dbe2ec780305c0
449d555969bfd7befe906877abab098c6e63a0e8
/1055/CH11/EX11.1/ch11_1.sce
77d276d9d0817a098a033da08da40ef341d03e49
[]
no_license
FOSSEE/Scilab-TBC-Uploads
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
refs/heads/master
2020-04-09T02:43:26.499817
2018-02-03T05:31:52
2018-02-03T05:31:52
37,975,407
3
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null
null
null
null
UTF-8
Scilab
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false
385
sce
ch11_1.sce
// To find the inductance and KVA rating of the arc suppressor coil in the system clear clc; C1=2*%pi*(10^-9)/(36*%pi*log((4*4*8)^(1/3)/(10*(10^-3)))); C=C1*192*(10^9);// capacitance per phase (micro farad) L=(10)^6/(3*314*314*C); V=132;//voltage (kV) MVA=V*V/(3*314*L); mprintf("inductance ,L=%.2f H\n",L); mprintf("MVA rating of suppressor coil =%.3f MVA per coil",MVA);
1cce840bedc2bcdfa90ed92b2b81d9bef105b0e6
449d555969bfd7befe906877abab098c6e63a0e8
/1847/CH2/EX2.53/Ch02Ex53.sce
5cd4bd5625f2a18241f1d9aa57328fdfc4474581
[]
no_license
FOSSEE/Scilab-TBC-Uploads
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
refs/heads/master
2020-04-09T02:43:26.499817
2018-02-03T05:31:52
2018-02-03T05:31:52
37,975,407
3
12
null
null
null
null
UTF-8
Scilab
false
false
489
sce
Ch02Ex53.sce
// Scilab Code Ex2.53:: Page-2.37(2009) clc; clear; mu = 1; // Refractive index of the air film b = 1.5/25; // Fringe width, cm lambda = 5893e-008; // Wavelength of light used to illuminate a wedge shaped film, cm // As b = lambda/(2*mu*theta), solving for theta theta = lambda/(2*mu*b); // Angle of the wedge, radian printf("\nThe angle of the wedge shaped air film = %5.3f degrees", theta*180/%pi); // Result // The angle of the wedge shaped air film = 0.028 degrees
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if (blk_name.entries(bl) == "inv_mblif") then fix_vdd = 1; end
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Example2_11.sci
//Chapter 2_Thick Film and Thin Film Hybrid ICs //Caption : Ratio //Example2.11: Two thin resistor are measured at 50 degree celcius and 100degree celsius and are found to have the following values: //Temperatur(degree C) Ra(ohm) Rb(ohm) // 50 50 100 // 100 51 102.1 //Calcullate the ratio TCR in ppm/degree celcius. //Solution: function TCR= ratio(Rat1,Rbt1,Rat2,Rbt2,T1,T2) TCR=(Rat2/Rbt2-Rat1/Rbt1)*10^6/((Rat1/Rbt1)*(T1-T2)) disp('ratio TCR is=")// iinclude ";" at the time of calling the function at last disp('ppm/degree Celsius',TCR)//ppm: part per million endfunction //ratio(100,50,102.1,51,100,50);
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sin2cos2sin4_7v10_negfreq_Gforareachw_forscilab.sci
clear all nmtr=4; l0=20; A=2.2; g=9.81; s=poly(0,'s'); den=[1 0.1 g./l0]; nom=[1]; nomw=poly(nom,'s','c'); denw=poly(den,'s','c'); j=sqrt(-1); pi=3.1415; W=syslin('c',nomw,denw); ci=1; wst=0.5; G1p=cell(1,7); //ñîçäàåì ìàòðèöó íà äèàãîíàëè êîòîðîé ñòîÿò ïåðåäàòî÷íûå ôóíêöèè îò nw //îñòàëüíûå ýëåìåíòû ìàòðèöû - íîëþ. clear den1; for wn=1:1:nmtr+1 den1(wn,3)=den(1).*(wn-1).*(wn-1); den1(wn,2)=-den(2).*(wn-1); den1(wn,1)=den(3); den1c(wn)=poly(den1(wn,:),'s','c'); end clear den2; for wn=1:1:nmtr+1 den2(wn,3)=den(1).*(wn-1).*(wn-1); den2(wn,2)=den(2).*(wn-1); den2(wn,1)=den(3); den2c(wn)=poly(den2(wn,:),'s','c'); end for Wwi=0:1:nmtr Ww(nmtr-Wwi+1,nmtr-Wwi+1)=syslin('c',[1],den1c(Wwi+1)); Ww(nmtr+Wwi+1,nmtr+Wwi+1)=syslin('c',[1],den2c(Wwi+1)); end //%ñîçäàåì ìàòðèöó ñ ýëåìåíòàìè -w äî ñðåäíåé ñòðîêè è w ïîñëå ñðåäíåé ñòðîêè for i=1:1:(nmtr*2+1) Wneg(i,i)=i-nmtr-1; end //ñîçäàåì ìàòðèöó ñ ýëåìåíòàìè -w äî ñðåäíåé ñòðîêè è w ïîñëå ñðåäíåé ñòðîêè f11=0:0.5:6.3; ppp=2; wi=1; fi=1; f=f11(fi); Wsin2wf=zeros(nmtr*2+1,nmtr*2+1); for ni=3:1:(nmtr*2+1) Wsin2wf(ni-2,ni)=(A./2).*exp(j.*0.5.*pi-j.*f); Wsin2wf(ni,ni-2)=-(A./2).*exp(j.*0.5.*pi+j.*f); end Wsin2wf=-g.*(l0.^-2).*Wsin2wf; f1=f+0.5.*pi./2; Wcos2wf=zeros(nmtr*2+1,nmtr*2+1); for ni=3:1:(nmtr*2+1) Wcos2wf(ni-2,ni)=(A./2).*exp(j.*0.5.*pi-j.*f1); Wcos2wf(ni,ni-2)=-(A./2).*exp(j.*0.5.*pi+j.*f1); end Wcos2wf=4.*(l0.^-1).*(s/j).*s.*Wcos2wf; Wsin2wf=Wneg*Wsin2wf; f2=2.*f; Wsin4wf=zeros(nmtr*2+1,nmtr*2+1); for ni=5:1:(nmtr*2+1) Wsin4wf(ni-4,ni)=(A./2).*exp(j.*0.5.*pi-j.*f2); Wsin4wf(ni,ni-4)=-(A./2).*exp(j.*0.5.*pi+j.*f2); end Wsin4wf=-2.*(l0.^-2).*(s/j).*s.*(A.^2).*Wsin4wf; Wsin4wf=Wneg*Wsin4wf;
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//Variable declaration deltavi=0.5 //change in vi(V) deltat=10 //change in time(us) s=1 //slew rate(V/us) //Calculations Kvf=(s*deltat)/deltavi //closed loop gain of amplifier //Results printf ("closed loop gain of amplifier is %.1f",Kvf)
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//Chapter 8 Chemical Equlibrium clc; clear; //Initialisation of Variables T= 65 //C R= 1.98 //cal/mol K kp= 2.8 kp1= 0.141 T1= 25 //C //CALCULATIONS H= log10(kp/kp1)*2.303*R*(273+T1)*(273+T)/(T-T1) H= H+62 //RESULTS mprintf("Average Heat of reaction= %.2f cal",H)
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clc; clear; Sfl=0.05;//slip of full load current disp('during direct switching') Vmp=1; Imp=6*Vmp; Ila=6*Vmp; Ta=0.3*Imp; disp(Ta,Ila,Imp,Vmp,'The motor phase voltage,motor phase current line current and torque during direct switching are:') disp('During stator resistance switching:') Vmpb=0.33; Impb=6*Vmpb; Ilb=6*Vmpb; Tb=0.3*Impb; disp(Tb,Ilb,Impb,Vmpb,'The motor phase voltage,motor phase current line current and torque during stator resistance switching are:') disp('During auto transformer starting with the motor current limied to 2pu') Vmpc=0.33; Impc=6*Vmpc; Ilc=6*Vmpc; Tc=0.3*Impc; disp(Tc,Ilc,Impc,Vmpc,'The motor phase voltage,motor phase current line current and torque during auto transformer starting with the motor current limied to 2pu switching are:') disp('During star delta starting:') Vmpd=0.58; Impd=6*Vmpd; Ild=6*Vmpd; Td=0.3*Impd; disp(Td,Ild,Impd,Vmpd,'The motor phase voltage,motor phase current line current and torque during star delta starting are:') disp('For full load torque ') Ilat=(0.75^2); disp('times the full load current',Ilat,'The line current is:')
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// scilab Code Exa 6.2 radially tipped Centrifugal blower 3000rpm P=150; // Power Output in kW N=3e3; // Speed in RPM d2=40/100; // outer diameter of the impeller in m d1=25/100; // inner diameter of the impeller in m b=8/100; // impeller width at entry in m n_st=0.7; // stage efficiency V1=22.67; // Absolute Velocity at entry in m/s ro=1.25; // density of air in kg/m3 // part(a) determining the pressure developed u2=%pi*d2*N/60; u1=d1*u2/d2; w_ac=u2^2; delh_s=n_st*w_ac; delp=ro*delh_s; disp ("mm W.G." ,delp/9.81,"(a)the pressure developed is") // part (b) determining the power required A1=%pi*d1*b; m=ro*V1*A1; P=m*w_ac/10e2; disp("kW",P,"(b)Power required is")
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function [slp]=projsl(sl,q,m) //slp= projected model of sl q*m is the full rank //factorization of the projection. //! slp=syslin(sl(7),m*sl(2)*q,m*sl(3),sl(4)*q,sl(5),m*sl(6))
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//there is a pole at the origin and contribution of gain k k=10^(14/20) //20*log(k)=14 disp("equation of starting line is y=-20*log(w)+14") wc1=10^(0) disp(wc1,"hence at wc1, 14=-20*log(wc1)+14. that is wc1 = ") y1=poly([1 1/wc1],'s','coeff') disp("equation of next line is y=-40*log(w)+14") wc2=10^(40/40) //-40*log(wc2)=-40 disp(wc2,"wc2=") y2=poly([1 1/wc2],'s','coeff') wc3=50 //given y3=poly([1 1/wc3],'s','coeff') TF= k*(y2)/((y1)*(y3)) disp(TF,"transfer function = ")
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//developed in windows XP operating system 32bit //platform Scilab 5.4.1 clc;clear; //example 16.23w //calculation of the frequency of train whistle heard by the person standing on the road perpendicular to the track //given data v=340//speed(in m/s) of the sound in the air d1=300//distance(in m) of the train from the crossing u=120*10^3/(60*60)//speed(in m/s) of the train nu=640//frequency(in Hz) of the whistle d2=400//distance(in m) of the person from the crossing ,perpendicular to the track //calculation theta=acosd(d1/sqrt(d1^2+d2^2))//pythagoras theorem nudash=(v/(v-(u*cosd(theta))))*nu//frequency of the whistle heard printf('the frequency of train whistle heard by the person standing on the road perpendicular to the track is %d Hz',nudash)
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//Tested on Windows 7 Ultimate 32-bit //Chapter 14 Operational Amplifiers Pg no. 423 clear; clc; //Given Ad=15000;//differential gain Ac=15;//common mode gain //Solution CMRR=Ad/Ac;//common mode rejection ratio CMRR_dB=20*log10(CMRR);//common mode rejection ratio in dB units printf("(CMRR)dB = %.f dB",CMRR_dB);
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//Parameters of the Plane exec('Vtol_Parameters.sce', -1); //States matrix Ap=[0 0 0 1 0 0; 0 0 0 0 1 0; 0 0 0 0 0 1; 0 0 -g -c/m 0 0; 0 0 0 0 -c/m 0; 0 0 0 0 0 0]; Bp=[0 0; 0 0; 0 0; 1/m 0; 0 1/m; r/J 0]; Cp=[1 0 0 0 0 0; 0 1 0 0 0 0]; Dp=[0 0; 0 0]; sys = syslin('c',Ap,Bp,Cp,Dp); //checking controllability and observability [i,j] = size(Ap); // e=[B, AB, A^2 B,..., A^(n-1) B] e = cont_mat(sys.A,sys.B); rankC=rank(e); if i == rankC then disp('Continuous System is Controllable'); end // o=[C; CA; CA^2;...; CA^(n-1) ] o = obsv_mat(sys.A, sys.C); rankO=rank(o); if j == rankO then disp('Continuous System is Observable'); end tranM=ss2tf(sys); // Matriz de transferencia disp('Matriz de Transferencia',tranM); tfc11 = tranM(1,1); tfc22 = tranM(2,2); /* Plot singular values of LTI the model */ tr = trzeros(sys) w = logspace(-3,3); sv = svplot(sys,w); scf(1); plot2d("ln", w, 20*log(sv')/log(10),leg="Input 1@Input 2") xgrid(12) xtitle("Singular values plot","Frequency (rad/s)", "Amplitude (dB)"); //Obtenciion de los polors zeros del modelo de software scf(2); plzr(sys); xtitle("Poles and zeros plot of system","Real", "Imaginarie"); //autovalores evals=spec(Ap); ///////////////////////////////////--------------------------- //Augment Plant with Integrators at Plant Input [ns,nc]=size(Bp); //ns= number of inputs; nc=number of controls Ai=[Ap Bp; 0*ones(nc,ns) 0*ones(nc,nc)]; Bi=[0*ones(ns,nc); eye(nc,nc)]; Ci=[Cp 0*ones(nc,nc)]; Di=0*ones(nc,nc); I=eye(nc,nc); sysi=syslin('c',Ai,Bi,Ci,Di); //View of the singular values of plant with integrator and the poles and //zeros /* Plot singular values of LTI the model */ tri = trzeros(sysi) w = logspace(-3,3); svi = svplot(sysi,w); scf(3); plot2d("ln", w, 20*log(svi')/log(10),leg="Input 1@Input 2") xgrid(12) xtitle("Singular values plot of Plant with Integrator","Frequency (rad/s)", "Amplitude (dB)"); //Obtenciion de los polors zeros del modelo de software scf(4); plzr(sys); xtitle("Design Plant with integrator:poles and zeros","Real", "Imaginarie"); //lqr controller calculation //We use the ricatti equation for calculate de gain of the lqr controller //for this we have A'*X+X*A-X*B*X+C=0 for function X=riccati(A,B,C,'c','eigen') C=0.8*eye(8,8); //State Weighting Matrix rho=1e-0; //Cheap control recovery parameter //The smaller the parameter, the better the recovery. R = rho*eye(nc,nc);//Control Weigthing Matrix //now we calculate B B=Bi*inv(R)*Bi'; A=Ai; //Solv the ricatti equation X=riccati(A,B,C,'c','eigen'); //the value of the gain G G=inv(R)*Bi'*X; //<--this value is important mtfk //--------------------------------------------------------------------- //computing H //The gain H H=(ppol(Ai',Ci',[-10,-11,-12,-13,-14,-15,-16,-17]))';
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clc // Given that Ip = 53 // Angle of polarization of light // Sample Problem 9 on page no. 216 printf("\n # PROBLEM 9 # \n") I_r = 90 - Ip // Angle of refraction mu = tan(Ip*%pi/180) // Refractive index of water printf("Standard formula used \n mu=tan(Ip)\n") printf("\nAngle of refraction is %d degree. \n Refractive index of material is %f",I_r,mu)
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//CHAPTER 7 ILLUSRTATION 2 PAGE NO 197 //TITLE:GOVERNORS //FIGURE 7.5(A),7.5(B) clc clear //=========================================================================================== //INPUT DATA OA=.3// LENGTH OF UPPER ARM IN m m=6// MASS OF EACH BALL IN Kg M=18// MASS OF SLEEVE IN Kg r2=.2// RADIUS OF ROTATION AT BEGINING IN m r1=.25// RADIUS OF ROTATION AT MAX SPEED IN m //=========================================================================================== h1=(OA^2-r1^2)^.5// HIEGHT OF GOVERNOR AT MAX SPEED IN m N1=(895*(m+M)/(h1*m))^.5// MAX SPEED IN rpm h2=(OA^2-r2^2)^.5// HEIGHT OF GONERNOR AT BEGINING IN m N2=(895*(m+M)/(h2*m))^.5// MIN SPEED IN rpm //=========================================================================================== printf('MAX SPEED = %.3f rpm\n MIN SPEED = %.3f rpm\n RANGE OF SPEED = %.3f rpm',N1,N2,N1-N2)
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Ex16_3.sce
clear // //Given //Variable declaration Do=200 //Outer diameter in mm Di=100 //Inner diameter in mm tau=40 //Maximum shear stress in N/sq.mm //Calculation T=int(((%pi)/16*tau*((Do**4-Di**4)/Do)))*1e-3 //Maximum torque transmitted by the shaft in Nm //Result printf("\n Maximum torque transmitted by the shaft = %0.3f Nm",T)
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Ex16_6.sce
clear all clc close C1=0.125*10^-6;//in Farad C2=1*10^-9;//in Farad R1=360;//in ohms R2=544;//in ohms theta = sqrt(C1*C2*R1*R2);//in usec n = 1/[1+(1+(R1/R2))*(C2/C1)]; alpha = (R2*C1)/(2*theta*n); printf("theta parameter of wave eq %f us \n",theta*10^6) printf("n the parameter of circuit eq %f \n",n) printf("alpha parameter of circuit eq %f \n",alpha) T2 = 10.1*theta;//duration of lightning impulse pulse in us T1 = T2/45;//duration of lightning impulse pulse in us printf("duration of lightning impulse pulse %f us \n",T2*10^6) printf("duration of lightning impulse pulse %f us \n",T1*10^6) //answer in the book for T1 is wrong T = T1/T2; printf("generated lighting impulse is %f us \n",T) alpha1 = [alpha-sqrt((alpha^2)-1)]/theta;//in us^-1 alpha2 = [alpha+sqrt((alpha^2)-1)]/theta;//in us^-1 printf("aplha1 parameter of wave eq is %f us^-1 \n",alpha1*10^-6) printf("aplha1 parameter of wave eq is %f us^1 \n",alpha2*10^-6) //answer in the book is slightly different // Now eq of waveform of generated pulse is e(t)=99.75(e^-0.015t - e^-2.77t)
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function [stk,txt,top]=%m2sci() // multiplications //! // Copyright INRIA txt=[] s1=stk(top-1) s2=stk(top) [e1,te1]=s1(1:2); [e2,te2]=s2(1:2); if s1(5)=='10' then e1='str2code('+e1+')''',te1='0',end if s2(5)=='10' then e2='str2code('+e2+')''',te2='0',end // if te2=='2' then e2='('+e2+')',end if te1=='2' then e1='('+e1+')',end if s1(3)=='1'&s1(4)=='1' then stk=list(e1+'*'+e2,'1',s2(3),s2(4),s1(5)) elseif s2(3)=='1'&s2(4)=='1' then stk=list(e1+'*'+e2,'1',s1(3),s1(4),s1(5)) else stk=list(e1+'*'+e2,'1',s1(3),s1(4),s1(5)) end top=top-1
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Ex8_8.sce
//Variable declaration Vs=200 //dc source voltage(V) Il=5 //current to load voltage(A) Vl=15 //load voltage(V) eta=.85 //efficiency f=20 //oscillator frequency(Hz) iSmax=2.6 //peak value of supply current(A) P=100 //full load power supply(W) pdf=0.4 //pulse duty factor //Calculations Isav=(Vl*Il)/(Vs*eta) //average peak supply current(A) iS=(2*Isav)/pdf //supply current(A) T=1000/f //oscillation time period(uS) tp=pdf*T //transistor time(us) d=iS/tp //change in iS with respect to time(A/us) tp1=iSmax/d //transistor time(us) pdf1=tp1/T //pulse duty factor Isav1=(iSmax*pdf1)/2 //average peak supply current(A) eta1=(P*100)/(Vs*Isav1) //efficiency //Results printf ("peak value of supply current is %.3f A",Isav) printf ("pdf is %.3f ",pdf) printf ("overall efficienc is %.1f %%",eta1)
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Ex22_7.sce
clc; //e.g 22.7 VDD=20; RD=2.5*10**3; RS=1.5*10**3; R1=2*10**6; R2=250*10**3; ID=4*10**-3; VG=(R2*VDD)/(R1+R2); VS=ID*RS; VGS=VG-VS; disp('V',VGS*1,"VGS="); VD=VDD-ID*RD; VDS=VD-VS; disp('V',VDS*1,"VDS=");
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Ch3_3_74.sce
clc disp("Example 3.74") printf("\n") disp("Find the Ve, Ic,Vce & Vc. Draw a DC load line for Voltage divider circuit") printf("Given\n") //given Vcc=15 Vbe=0.7 hFE=50 R1=6.8*10^3 R2=3.3*10^3 Rc=0.9*10^3 Re=0.9*10^3 //thevenin voltage Vt=(Vcc*R2)/(R1+R2) //thevenin resistance Rt=(R1*R2)/(R1+R2) //base current Ib=(Vt-Vbe)/(Rt+(1+hFE)*Re) //collector current Icq=hFE*Ib //emitter current Ie=Ib+Icq //emitter voltage Ve=Ie*Re //collector to emitter voltage Vceq=Vcc-(Icq*Rc)-(Ie*Re) //collector voltage Vc=Vce+Ve //to draw DC load line Ic1=Vcc/(Rc+Re) Vce=[Vcc Vceq 0] Ic=[0 Icq Ic1] printf("Q(%f,%f)\n",Vceq,Icq) plot2d(Vce, Ic) xlabel("Vce") ylabel("Ic") xtitle("DC load line for base bias circuit")
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25_18.sce
//ques-25.18 //Calculating volume occupied by oxygen using ideal gas equation and van der Waals equation clc n=3;//moles of oxygen P=50;//pressure (in atm) T=373;//temperature (in K) a=1.36;//(in L^2 atm/mol^2) b=0.0318;//(in L/mol) //Ideal Gas equation V1=(n*0.0821*T)/P; //Van der Waals equation V2=n*b+(n*0.0821*T)/(P+a*n^2/V^2); printf("The volume occupied by oxygen calculated using ideal gas equation is %.2f L and using van der Waals equation is %.2f L.",V1,V2);
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Ex9_1.sce
clear // // //Initilization of Variables L=5000 //mm //Length of strut dell=10 //mm //Deflection W=10 //N //Load //Calculations //Central Deflection of a simply supported beam with central concentrated load is //dell=W*L**3*(48*E*I)**-1 //Let E*I=X X=W*L**3*(48*dell)**-1 //mm //Euler's Load //Let Euler's Load be P P=%pi**2*X*(L**2)**-1 //Result printf("\n Critical Load of Bar is %0.2f N",P)
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clc; clear all; disp("Heat loss calculations") k=1.05;// W/(m*C) ti=600;//degree C to=70;// degree C L=0.12;//m A=0.6*0.6;//m^2 Sfcwall=A/L; D=0.6;//m Sfcedge=0.54*D; Sfccorner=0.15*L; Sfct=6*Sfcwall+12*Sfcedge+8*Sfccorner; Q=k*Sfct*(ti-to); disp("W",Q,"Heat loss through walls, Q =")
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Combined_run.sce
// do all the steps required to get the 3 graphs from raw data // SET THE VARIABLES // resets it back to its default value for quicker processing stacksize(5000000) //num_of_samples is the number of samples of a particular band num_of_samples = 348; //num of bands is the number of bands of spectrum being used // band 1 is 20MHz to 40MHz...band 2 is 40MHz to 60MHz..etc // eg if we are just looking at the fourth band (80 - 100MHz) start_num_of_band = 4; // and end_num_of_band = 4; start_num_of_band = 25; end_num_of_band = 25; // This is the noise floor for the particular band(s) at hand threshold = -80.1; // num_of_data_slots is the number of data slots in each data file, this should not change num_of_data_slots = 501 for k = start_num_of_band:end_num_of_band // First stage // allows each file to be chosen for j = 1:num_of_samples number = string(j); // this loop will only run once if only one band is being analysed // It creates all the csv files with only the 501 trace values needed // A becomes a list of the comma seperated variables in the raw data file A = read_csv('C:\Program Files\Tektronix\SA2600PC\Results'+'/'+ string(k*20) + 'MHz to '+ string((k+1)*20) + 'MHz' + number +'.csv'); // A_values is a matrix of the trace1 values only A_values = A(46:1:546,1); //Create the csv file and saves it to results folder on desktop //write_csv(A_values,'C:\Documents and Settings\pflynn\Desktop\Results' + '/'+ string(k*20) + 'MHz to '+ string((k+1)*20) + 'MHz ' + number +'.csv'); // A becomes a list of the 501 trace1 values // evstr() changes them from string to numerical values because they are stored as strings in the csv files evstr_A_values = evstr(A_values); // B is a list of strings of either 1 or 0 depending on wheather the value // exceeds the threshold or not. //B = string((evstr_A_values>threshold)*1); //end // Creates and saves files used for getting duty cycle plots //write_csv(B,'C:\Documents and Settings\pflynn\Desktop\Threshold data'+ '/th '+ string(T*20) + 'MHz to '+ string((T+1)*20) + 'MHz ' + number +'.csv'); // The first set of threshold data is put into thresh_data if(j == 1) tresh_data = (evstr_A_values>threshold)*1 max_hold_data = evstr_A_values; B = ones(num_of_data_slots,num_of_samples); B(1:num_of_data_slots,j) = evstr_A_values; //The remaining sets of data are added to A (makes duty cycle data) else tresh_data = tresh_data + (evstr_A_values>threshold)*1; // C is a list of 1s and 0s, 1 if B is greater than A at that point, else c is 0 C = evstr_A_values>max_hold_data; // D is the opposite of C D = ~C; // Values in A are updated if values in B are greater than it at particular points max_hold_data = max_hold_data.*D + evstr_A_values.*C; B(1:num_of_data_slots,j) = evstr_A_values; if j == num_of_samples real_tresh_data = tresh_data./num_of_samples end end end end //do all plots // plot max hold graphs // change directory to the desired location to save these plot files cd('C:\Documents and Settings\pflynn\Desktop\Combined plots'); //clear window clf(); x = (k*20):(1/25):(k+1)*20; y = (1:1:num_of_samples); z = evstr(B); zm = min(z); zM = max(z); // setting the colour map // num_of_colours is the amount of different shades in this colour plot num_of_colours = round(((max(z)-min(z))*10)+.49) // num_of_white is the number of colours that are white in order for it to change from white to a colour at the correct threshold num_of_whites = round(((sqrt((min(z) - threshold)*(min(z) - threshold)))*10)+.49) // red colour r = linspace(0,1,(num_of_colours - num_of_whites)); //green colour g = zeros(1,(num_of_colours - num_of_whites)); g(1,1:1:((num_of_colours - num_of_whites)/2)) = linspace(0,1,((num_of_colours - num_of_whites)/2)) g(1,(((num_of_colours - num_of_whites)/2)+1):1:(num_of_colours - num_of_whites)) = linspace(1,0,((num_of_colours - num_of_whites)/2)) // Blue colour b = linspace(1,0,(num_of_colours - num_of_whites)); // sets the color map to white cmap = ones(num_of_colours,3); // puts colour into this section of color map for l = (num_of_whites + 1):num_of_colours cmap(l,1)= r(1,(l-num_of_whites)); cmap(l,2)= g(1,(l-num_of_whites)); cmap(l,3)= b(1,(l-num_of_whites)); end xset('colormap',cmap); subplot(3,2,4) colorbar(zm,zM,[1 , num_of_colours],fmt="%.2f"); //setting the type of colour plot //scf(0); subplot(312) Sgrayplot(x,y,z); // setting the axis lable xtitle("Waterfall plot (power recorded in dBm where detection threshold is exceeded)",'Frequency (MHz)','Time (mins*5)'); // setting the colour bar limits M = read_csv('C:\Documents and Settings\pflynn\Desktop\Duty cycle plot data'+ '/dc '+ string(k*20) + 'MHz to '+ string((k+1)*20) + 'MHz.csv'); subplot(313) plot([k*20:(1/25):(k+1)*20],evstr(M)) // give it titles xtitle('Fraction of Time','Frequency (MHz)','Fraction of Time'); //MAX Hold // plot the actual graph subplot(311) plot([k*20:(1/25):(k+1)*20],max_hold_data) //threshold line plot([k*20:(1/25):(k+1)*20],threshold,'r--') // plots a dash-dotted line with a right-pointing triangle centered on each points // give it titles xtitle('Max Hold','Frequency (MHz)','Power (dBm)'); // exporting the image to jpg file xs2jpg(0,'all plots '+ string(k*20) + 'MHz to '+ string((k+1)*20) + 'MHz.jpg'); xs2jpg(gcf(),'/all plots '+ string(k*20) + 'MHz to '+ string((k+1)*20) + 'MHz.jpg')
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EX_2_59.SCE
// Example 2.59:h parameters and hybrid parameters clc; clear; //H Paramters are hie=1100;//in killo ohms hre=2*10^-4; hfe=50; hoe=2.5*10^-5;// in ampere per volt hic=hie;// hrc=1-hre;// hfc=-(1+hfe);// hoc=hoe;// hib=(hie/(1+hfe));// hrb= ((hie*hoe)/(1+hfe))-hre;// hob=(hoe/(1+hfe));// rbb=100; rbe=(hie-rbb)*10^-3;//in killo ohms rbc= ((hie-rbb)/hre)*10^-6;// gm= ((hfe/(hie-rbb)));// x=hoe-((hfe*hre)/(hie-rbb));// rce=1/(1.25*10^-2);// disp(hic,"hic=",hrc,"hrc=",hfc,"hfc=",hoc,"hoc=","H-parameters for common collector configuration are") disp(hib,"hib=",hrb,"hrb=",hob,"hob=","H-parameters for common collector configuration are") disp(rbe,"rbe(in killo ohms)=",rbc,"rbc(mega ohms)=",gm,"transconductance(mho)=",rce,"rce(in killo ohms)=","hybrid pie paramtere are")
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errcatch(-1,"stop");mode(2);//Example 10.13.1 // sampling rate ; ; //given data : N=10;//number of cycles f=1*10^3;//in Hz sampling_period=N/f; sampling_rate=1/sampling_period; disp(sampling_rate,"sampling rate in samples per second") exit();
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clc // initialization of variables clear // Rod dimensions and material properties b1=60 //mm l1=3 //m l2=1.5 //m h1=40 //mm b2=40 //mm h2=30 //mm G=77.5 //GPa T1=750 //Nm T2=400 //Nm //calculations b1=b1*10^-3 h1=h1*10^-3 b2=b2*10^-3 h2=h2*10^-3 G=G*10^9 // for the left portion of the rod k1l=0.196 k2l=0.231 // for the right portion of the rod k1r=0.178 k2r=0.223 T=T1+T2 tau_maxL=T/(k2l*b1*(h1)^2) tau_maxR=T2/(k2r*b2*(h2)^2) tau_max=max(tau_maxL,tau_maxR) J1=b1*h1^3/12+h1*b1^3/12 J2=b2*h2^3/12+h2*b2^3/12 bet=T*l1/(G*J1)+T2*l2/(G*J2) printf(' The maximum shear stress is = %.1f MPa',tau_max/10^6) printf('\n twist = %.4f rad',bet) //wrong answer for twist in the text
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//Example 13.4 // capacitance and series resistance clc; clear; close; //given data : M=18.35; // in m-H R1=200; // in ohm L1=40.6; // in m-H R2_1=119.5; // in ohm R4=100; // in ohm C2=((M*10^-3)/(R1*R4))*10^6; R2=(R4*(L1-M))/M; Rs=R2-R2_1; disp(C2,"capacitance,C(micro-farad) = ") disp(Rs,"the series resistance,Rs(ohm) = ")
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//******************************************* // This is the Scilab script for Exercise 4. // // Use the help facility for more information // on individual functions used. // // Author: J. Kaempf, 2008 //******************************************** // Animation of the Coriolis force clf(); clear; set("figure_style","new"); a=get("current_axes"); a.parent.figure_size= [600,600]; x=read("output1.txt",-1,3); // read input data fre = x(1,1); dt = x(1,2); ntot = x(1,3); radius = 20; xset('pixmap',1); factor = 0.9; fac2 = factor*radius; // needed for graphics for n=2:ntot scf(0); time = x(n,3); xr = x(n,1); yr = x(n,2); //xbasc() // clears graphic window xset('wwpc'); //clears pixmap // isoview scaling plot2d(0,0,-1,"030"," ",[-20,-20,20,20]); // draw circular, blue dish = our tank xset("color",2) xfarc(-fac2,fac2,2*fac2,2*fac2,0,360*64) // rotate outer ticks to visualise relative rotation of the tank xx = radius*sin(fre*time); yy = radius*cos(fre*time); x1 = [factor*xx xx]; y1 = [factor*yy yy]; xset("color",5) xset("thickness",6) xpoly(x1,y1,"lines",1) xx = radius*cos(fre*time); yy = -radius*sin(fre*time); x2 = [factor*xx xx]; y2 = [factor*yy yy]; xset("color",0) xset("thickness",6) xpoly(x2,y2,"lines",1) xx = -radius*sin(fre*time); yy = -radius*cos(fre*time); x3 = [factor*xx xx]; y3 = [factor*yy yy]; xset("color",0) xset("thickness",6) xpoly(x3,y3,"lines",1) xx = -radius*cos(fre*time); yy = radius*sin(fre*time); x4 = [factor*xx xx]; y4 = [factor*yy yy]; xset("color",0) xset("thickness",6) xpoly(x4,y4,"lines",1) // inner ticks remain motionless xset("color",2) xfarc(-fac2,fac2,2*fac2,2*fac2,0,360*64) x1 = [0 0]; y1 = [factor*fac2 fac2]; xset("color",5) xset("thickness",6) xpoly(x1,y1,"lines",1) x1 = [0 0]; y1 = [-fac2 -factor*fac2]; xset("color",0) xset("thickness",6) xpoly(x1,y1,"lines",1) y1 = [0 0]; x1 = [factor*fac2 fac2]; xset("color",0) xset("thickness",6) xpoly(x1,y1,"lines",1) y1 = [0 0]; x1 = [-fac2 -factor*fac2]; xset("color",0) xset("thickness",6) xpoly(x1,y1,"lines",1) //draw location xset("color",1); xfarc(xr-1,yr+1,2.0,2,0,360*64); xset("color",7); xfarc(xr-0.8,yr+0.8,1.6,1.6,0,360*64); //draw trajectory xset('thickness',4) plot2d(x(2:n,1),x(2:n,2),8,'000','',[-radius,-radius,radius,radius]) //add title t=a.title; t.foreground=1; t.font_size=12; t.font_style=4; t.text="Rotating Frame of Reference"; // creation of GIF files (optional) //if n < 10 then // xs2gif(0,'ex100'+string(n)+'.gif') //else // if n < 100 then // xs2gif(0,'ex10'+string(n)+'.gif') // else // xs2gif(0,'ex1'+string(n)+'.gif') // end //end xpause(5d2); xset('wshow'); end // end of animation
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// Exa 6.21 clc; clear; close; // Given data T_sat = 99.6;// in degree C h_fg = 2258;// in kJ/kg m = 1;// steam output of the boiler in (assumed) m1 = 0.03;// exhaust steam x = 0.9; T1 = 21;// in degree C Cp = 4.187;// kJ/kg-K // Formula m1*(Cp*(T_sat-t)+x*h_fg)= m*Cp*(t-T1) t= (m1*(Cp*T_sat+x*h_fg)+m*Cp*T1)/(Cp*(m+m1)) disp(t,"Temperature of the feed water leaving the heater in degree C is");
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clc //initialisation of variables E= 95300 //cal mole^-1 l= 3000 //A e= 23060 //cal mole^-1 ev^-1 //CALCULATIONS e1= E/e //RESULTS printf (' energy in electron = %.2f electron volts',e1)
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function beauty_axes(x_text, y_text) a = gca(); a.x_label.text = x_text; a.x_label.font_size = 4; a.y_label.text = y_text; a.y_label.font_size = 4; endfunction function beauty_legend(text, place) legend(text, place), a = gca(); a.children(1).font_size = 2; endfunction function beauty_plot(x, y, kolor, thickness, style) plot2d(x, y); a = gca(); a.children(1).children.foreground = kolor; a.children(1).children.thickness = thickness; a.children(1).children.line_style = style; endfunction // THE BEGGINING OF LAB ACTIVITY IS HERE!! A = [0, 1; 1, -1]; b = [2; 1]; Q = [1, 0; 0, 1]; r = 2; x0 = [1; 0]; // object's state initial values // some calculations P = riccati(A, b*inv(r)*b', Q, 'c'); K = inv(r) * b' * P; F = A - b * K; [M, Lambda] = spec(F); R = M' * (Q + r * K' * K) * M; t = 5; J = (inv(M)*x0)' * ( (expm(Lambda*t)*inv(Lambda)*expm(Lambda*t) - 0.5*inv(Lambda)*(expm(Lambda*t))^2) - (expm(Lambda*0)*inv(Lambda)*expm(Lambda*0) - 0.5*inv(Lambda)*(expm(Lambda*0))^2) ) * R * inv(M)*x0 // text output printf("Оптимальный регулятор:\n") disp(P, "P =") disp(K, "K =") disp(F, "F ="); disp(M, "M ="); disp(Lambda, "Lambda ="); disp(R, "R ="); disp(J, "J ="); // import and model appropriate scheme path = get_absolute_file_path('launcher.sce'); scheme_name = path + 'modeling_scheme.zcos'; importXcosDiagram(scheme_name); xcos_simulate(scs_m, 4); //plotting graphs time = state.time; subplot(2,2,1); beauty_plot(time, state.values(:,1), 1, 1, 1); subplot(2,2,2); beauty_plot(time, state.values(:,2), 1, 1, 1); subplot(2,2,3); beauty_plot(time, control.values, 1, 1, 1); subplot(2,2,4); beauty_plot(time, perf_index.values, 1, 1, 1); // change K K = K + 0.20 * K; // remade calculations F = A - b * K; [M, Lambda] = spec(F); R = M' * (Q + r * K' * K) * M; t = 5; J = (inv(M)*x0)' * ( (expm(Lambda*t)*inv(Lambda)*expm(Lambda*t) - 0.5*inv(Lambda)*(expm(Lambda*t))^2) - (expm(Lambda*0)*inv(Lambda)*expm(Lambda*0) - 0.5*inv(Lambda)*(expm(Lambda*0))^2) ) * R * inv(M)*x0 // text output printf("\nНеоптимальный регулятор:\n") disp(K, "K =") disp(F, "F ="); disp(M, "M ="); disp(Lambda, "Lambda ="); disp(R, "R ="); disp(J, "J ="); // import and model appropriate scheme again path = get_absolute_file_path('launcher.sce'); scheme_name = path + 'modeling_scheme.zcos'; importXcosDiagram(scheme_name); xcos_simulate(scs_m, 4); //plotting graphs again time = state.time; subplot(2,2,1); beauty_plot(time, state.values(:,1), 1, 1, 2); beauty_axes("$t\text{, с}$", "$x_1$"); beauty_legend(["Оптим. регулятор", "Неоптимальный"], 1); subplot(2,2,2); beauty_plot(time, state.values(:,2), 1, 1, 2); beauty_axes("$t\text{, с}$", "$x_2$"); beauty_legend(["Оптим. регулятор", "Неоптимальный"], 1); subplot(2,2,3); beauty_plot(time, control.values, 1, 1, 2); beauty_axes("$t\text{, с}$", "$u$"); beauty_legend(["Оптим. регулятор", "Неоптимальный"], 4); subplot(2,2,4); beauty_plot(time, perf_index.values, 1, 1, 2); beauty_axes("$t\text{, с}$", "$J$"); beauty_legend(["Оптим. регулятор", "Неоптимальный"], 4);
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Ex4_6.sce
// Problem no 4.4.6,Page No.95 clc;clear; close; F_C=100 //KN //Pt Load at C F_E=50 //KN //Pt Load at E w=20 //KN/m L_AE=2;L_ED=2;L_DC=2;L_CB=2 //m //Length of AE,ED,DC,CB respectively L=8 //m //Length of Beam //Calculations //Let R_A & R_B be the reactions at A & B //R_A+R_B=190 //Taking Moment at A //M_A=-R_B*L+F_C*(3*L_AE)+w*L_DC*(L_DC*2**-1+2*L_ED)+F_E*L_AE=0 R_B=(F_C*(3*L_AE)+w*L_DC*(L_DC*2**-1+2*L_ED)+F_E*L_AE)*L**-1 R_A=190-R_B //Shear Force Calculations //Shear Force at B V_B=R_B //Shear Force at C V_C1=R_B V_C2=R_B-F_C //Shear Force at D V_D=V_C2-w*L_DC //Shear Force at E V_E1=V_D V_E2=V_D-F_E //Shear Force at A V_A=V_E2 //Point of contraflexure //Let F be the point BF=x //Shear Force at F //V_F=R_B-F_C-w*(L_BF-L_CB) L_FB=-((-R_B+F_C)*w**-1-L_CB) V_F=0 //Bending Moment Calculations //Bending Moment at B M_B=0 //Bending Moment at C M_C=R_B*L_CB //Bending Moment at D M_D=R_B*(L_CB+L_DC)-F_C*L_DC-w*L_DC**2*2**-1 //Bending Moment at E M_E=R_B*(L_CB+L_DC+L_ED)-F_C*(L_ED+L_DC)-w*L_DC*(L_DC*2**-1+L_ED) //Bending Moment at A M_A=R_B*(L_ED+L_DC+L_AE+L_CB)-F_C*(L_ED+L_DC+L_AE)-w*L_DC*(L_DC*2**-1+L_ED+L_AE)-F_E*L_AE //Bending Moment at F L_FC=L_CB-L_CB M_F=R_B*L_FB-F_C*L_FC-w*L_FC**2*2**-1 L_DF=L_DC-L_FC //Result printf("The Shear Force and Bending Moment Diagrams are the results") //Plotting the Shear Force Diagram subplot(2,1,1) X1=[0,L_CB,L_CB,L_CB+L_DC,L_CB+L_DC+L_ED,L_CB+L_DC+L_ED,L_CB+L_DC+L_ED+L_AE] Y1=[V_B,V_C1,V_C2,V_D,V_E1,V_E2,V_A] Z1=[0,0,0,0,0,0,0,] plot(X1,Y1,X1,Z1) xlabel("Length x in m") ylabel("Shear Force in kN") title("the Shear Force Diagram") //Plotting the Bending Moment Diagram subplot(2,1,2) X2=[0,L_CB,L_CB+L_FC,L_CB+L_DC,L_CB+L_DC+L_ED,L_CB+L_DC+L_ED] Y2=[M_B,M_C,M_F,M_D,M_E,M_A] Z2=[0,0,0,0,0,0] plot(X2,Y2) xlabel("Length in m") ylabel("Bending Moment in kN.m") title("the Bending Moment Diagram")
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//[xt]=traj(t) //[xt]=traj(t) // approximation constante par morceaux de l'evolution de la masse // construite sur xk : trajectoire discrete. //! xt=xk(3,maxi(ent(t),1)); // //end
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function Xi = genererRandUniforme(borneA,borneB, iter) Xi = grand(iter,1,'unf',borneA,borneB); endfunction
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x = read_csv("E:\College\Courseware\Bachelor Thesis\programme\source c code\cluster variance\cluster_variance.txt"); x = evstr(x); plot(x,".");
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java trip.Main -m trip-tests/trip1.txt trip-tests/trip1.request
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//example 16.7 //calculate annual average rainfall clc;funcprot(0); //given L=50; //spacing between drains k=1D-5; //permeability coefficient a=10; b=10.3; Q=4*k*(b^2-a^2)/L; Pav=Q*24*3600*100*100/L; mprintf("annual average rainfall=%i cm",Pav);
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//chapter-9 page 411 example 9.2 //============================================================================== clc; clear; L=75*10^(-6);//Device Length in m V=25;//Voltage Pulse Amplified in V f=10*10^9;//Operating Frequency in Hz //CALCULATION Eth=(V/L)/10^5;//Threshold Electric Field in kV/cm //OUTPUT mprintf('\nThreshold Electric Field is Eth=%1.2f kV/cm',Eth); //=========================END OF PROGRAM===============================
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// Example no 4.9 // To find a)the minimum mean square error b)the standard deviation about mean value c)received power at d=2 km d)the likelihood that the received signal level at 2 km e) the percentage of area within 2 km // Page no. 143 clc; clear all; // Given data d0=100; // First receiver distance in meter d1=200; // Second receiver distance in meter d2=1000; // Third receiver distance in meter d3=3000; // Fourth receiver distance in meter p0=0; // Receved power of first receiver in dBm p1=-20; // Receved power of second receiver in dBm p2=-35; // Receved power of third receiver in dBm p3=-70; // Receved power of forth receiver in dBm // a)To find the minimum mean square error n=2887.8/654.306; // Loss exponent after differentiating and equating the squared error function with zero // Displaying the result in command window printf('\n Loss exponent = %0.0f',n); // b)To find the standard deviation about mean value P0=-10*n*log10(d0/100); // The estimate of p0 with path loss model P1=-10*n*log10(d1/100); // The estimate of p1 with path loss model P2=-10*n*log10(d2/100); // The estimate of p2 with path loss model P3=-10*n*log10(d3/100); // The estimate of p3 with path loss model J=(p0-P0)^2+(p1-P1)^2+(p2-P2)^2+(p3-P3)^2; // Sum of squared error SD=sqrt(J/4); // The standard deviation about mean value // Displaying the result in command window printf('\n The standard deviation about mean value = %0.2f dB',SD); // The decimal point is not given in the answer given in book. // c)To find received power at d=2 km d=2000; // The distance of receiver P=-10*n*log10(d/100); // The estimate of p2 with path loss model // Displaying the result in command window printf('\n The received power (at d=2 km) = %0.2f dBm',P); // Answer is varying due to round off error // d)To find the likelihood that the received signal level at 2 km gam=-60; // The received power at 2km will be greater than this power z=(gam-P)/SD; Pr=(1/2)*(1-erf(z/sqrt(2))); // The probability that received signal will be greater than -60dBm // Displaying the result in command window printf('\n The probability that received signal will be greater than -60dBm = %0.1f percent',Pr*100); // Answer is varying due to round off error // e)To find the percentage of area within 2 km A=92; // From figure 4.18, area receives coverage above -60dBm // Displaying the result in command window printf('\n The percentage of area within 2 km = %0.0f percent',A);
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function [x_r, t_r] = impz(b, a, n, fs) // It gives Impulse response of digital filter //Calling Sequence //x_r = impz(b) //x_r = impz(b, a) //x_r = impz(b, a, n) //x_r = impz(b, a, n, fs) //[x_r, t_r] = impz(b, a, n, fs) //Parameters //x_r: impz chooses the number of samples and returns the response in the column vector, x_r. //t_r : impz returns the sample times in the column vector, t_r // b : numerator coefficients of the filter // a : denominator coefficients of the filter // n : samples of the impulse response t(by default ,n = length(t) and is computed automatically. // fs : sampling frequency //Description //[x_r,t_r] = impz(b,a) returns the impulse response of the filter with numerator coefficients, b, and denominator coefficients, a. impz chooses the number of samples and returns the response in the column vector, x_r, and the sample times in the column vector, t_r. t_r = [0:n-1]' and n = length(t) is computed automatically. //Examples //[x_r,t_r]=impz([0 1 1],[1 -3 3 -1],10) //OUTPUT : // t_r = 0. 1. 2. 3. 4. 5. 6. 7. 8. 9 // x_r= 0. 1. 4. 9. 16. 25. 36. 49.....64......81 //[x_r,t_r]=impz(1,[1 1],5) //OUTPUT // t_r = 0. 1. 2. 3. 4 //x_r = 1. - 1. 1. - 1. 1. //This function is being called from Octave funcprot(0); rhs = argn(2) lhs = argn(1) if(rhs<1 | rhs>4) error("Wrong number of input arguments.") end select(rhs) case 1 then if(lhs==1) [x_r] = callOctave("impz",b) elseif(lhs==2) [x_r,t_r] = callOctave("impz",b) end case 2 then if(lhs==1) [x_r] = callOctave("impz",b,a) elseif(lhs==2) [x_r,t_r] = callOctave("impz",b,a) end case 3 then if(lhs==1) [x_r] = callOctave("impz",b,a,n) elseif(lhs==2) [x_r,t_r] = callOctave("impz",b,a,n) end case 4 then if(lhs==1) [x_r] = callOctave("impz",b,a,n,fs) elseif(lhs==2) [x_r,t_r] = callOctave("impz",b,a,n,fs) end end endfunction
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errcatch(-1,"stop");mode(2);//// exec("7.8data.sci"); Vmax = (Et2/Et1)*Vmax1 t = (Km/Vmax)*log(1/(1-X))+Curea0*X/Vmax; disp("t") disp(t) disp("s") exit();
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function r=mtlb_eye(a) // Copyright INRIA if size(a)==[1 1] then r=eye(a,a) else r=eye(a(1),a(2)) end
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FA0 = 0.867; // mol/s X1 = 0.5; X2 = 0.8; rA2 = -(1/800); X = [0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8]'; p = [189 192 200 222 250 303 400 556 800];//1/-rA = 800//dm^3.s/mols
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// Exa 3.3 format('v',6) clc; clear; close; // Given data V = 120;// in V Vz = 50;// in V R = 5;// in k ohm R = R * 10^3;// in ohm I = (V-Vz)/R;// in A R1 = 10;// in k ohm R1 = R1 * 10^3;// in ohm I_L = Vz/R1;// in A // The maximum value of zener diode current I_Zmax = I-I_L;// in A I_Zmax= I_Zmax*10^3;// in mA disp(I_Zmax,"The maximum value of zener diode current in mA is"); V2 = 80;// in V I = (V2-Vz)/R;// in A // The minimum value of zener diode current I_Zmin = I-I_L;// in A I_Zmin=I_Zmin*10^3;// in mA disp(I_Zmin,"The minimum value of zener diode current in mA is");
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//Dikshita Kambri 118A2044 //IPMV -EXPERIMENT 1 //TONAL RESOLUTION// clear all clc; a = imread("C:\Users\hp\Documents\Image Processing-Scilab\Images\coins.png"); a = double(a); //b = max(max(a); b = 256; i =input("How many bits do you want? 1 2 4 8: "); j = b/(2^i); F = floor(a/j); F1 = (F * 255)/max(max(F)); figure(1) imshow(uint8(a)) figure(2) imshow(uint8(F1))
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// Compute 1-, 2-, inf norms of the vector x, if x=[1.25, 0.02, -5.15, 0] clearglobal() clc; x=[1.25 0.02 -5.15 0] printf('x is') disp(x) printf('First Norm of x is') disp(norm(x,1)) printf('Second Norm of x is') disp(norm(x,2)) printf('infinite Norm of x is') disp(norm(x,'inf'))
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clear// //Variable Declaration M=2.21 //Applied moment in kip.ft d=3 //Diameter of the bar in inches sigma_y=40 //Yield strength of the of steel in ksi //Calculations //Part 1 sigma=32*M*12*(%pi*d**3)**-1 //Maximum Bending Stress in ksi T1=sqrt((sigma_y*0.5)**2-5**2)/(12*0.18863) //Maximum Allowable torque in kip.ft //Part 2 R=sqrt((sigma_y**2-5**2)*3**-1) //Maximum shear stress in ksi T2=sqrt(R**2-5**2)/(12*0.18863) //Maximum safe torque in kpi.ft //Result printf("\n Using the maximum shear stress theory T= %0.2f kip.ft",T1) printf("\n Using the maximum sitrotion energy theory T= %0.2f kip.ft",T2)
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clear all; clc; disp("Scilab Code Ex 1.1 :") w_varying = 270; l_crossection = 9; l_cb = 6; l_ac = 2; w_c = (w_varying/l_crossection) * l_cb //By proportion, load at C is found. f_resultant_c = 0.5* w_c *l_cb // Equations of Equilibrium //Balancing forces in the x direction: n_c = 0 //Balncing forces in the y direction: v_c = f_resultant_c // Balncing the moments about C: m_c = - (f_resultant_c*l_ac) // Displaying results: printf('\n\nThe resultant force at C = %.2f N',f_resultant_c); printf('\nThe horizontal force at C = %.2f N',n_c); printf('\nThe vertical force at C = %.2f N',v_c); printf('\nThe moment about C = %.2f Nm',m_c); // ---------------------------------------------------------END-------------------------------------------------
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//Tested on Windows 7 Ultimate 32-bit //Chapter 10 Feedback in Amplifiers Pg no. 346 clear; clc; //Given A0=200;//open loop midband gain B=0.05;//feedback factor beta fH=100D3;//open loop higher cutoff frequency in hertz //Solution fHfb=fH*(1+A0*B);//closed loop higher cutoff frequency in hertz printf("Closed loop higher cutoff frequency (fH)fb = %.1f MHz\n ",fHfb/10^6);
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function y=f(x) y=(1 ./(sqrt(x))) + 2.*log10(%e).*log(0.0000810811 + (2.51 ./ (13743.017 .* sqrt(x)))) endfunction x=0.001:0.001:0.1 //intervalo para estimar a raiz //plot(x,f(x)) //xgrid() // raiz entre 0.01 e 0.05 exec("falsaP.sci"); [raiz,x1,it,ea]=falsaP(0.01,0.05,f,1e-6,200) //raiz = 0.0289678 //iterações = 20 //erro relativo final = 0.0000007 function y=fp(x) y= -(1 ./(2.*(x.^(3/2)))) - log10(%e) .* 2.51 ./(12743.017) .* 1 ./((0.0000810811 + 2.51 ./ (13743.017 .* sqrt(x))) .* x ^(3/2)) endfunction exec("newtonraphson.sci"); //[raiz2,x2,it2,ea2]=newtonraphson(0.008,f,fp,1e-6,200) //raiz = 0.0289678 //iterações = 7 //erro relativo final = 0.00000005 [raiz3,x3,it3,ea3]=newtonraphson(0.08,f,fp,1e-6,3) // max de iterações x=0.01:0.01:1 plot(x,f(x))
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function [xm,fr]=frmag(num,den,npts) //[xm,fr]=frmag(num[,den],npts) //Calculates the magnitude of the frequency respones of //FIR and IIR filters. The filter description can be //one or two vectors of coefficients, one or two polynomials, //or a rational polynomial. //Case 1 (When den is not given): // num :Vector coefficients/Polynomial/Rational // :polynomial of filter //Case 2 (When den is given): // num :Vector coefficients/Polynomial of filter numerator // den :Vector coefficients/Polynomial of filter denominator //Case 1 and 2: // npts :Number of points desired in frequency response // xm :Magnitude of frequency response at the points fr // fr :Points in the frequency domain where // :magnitude is evaluated //! //author: C. Bunks date: 2 March 1988 // Copyright INRIA [lhs,rhs]=argn(0); if rhs==2 then, npts=den; end, fr=(0:.5/(npts-1):.5); dfr=exp(2*%i*%pi*fr); if rhs==2 then, //-compat type(num)==15 retained for list/tlist compatibility if type(num)==15|type(num)==16 then, xm=abs(freq(num(2),num(3),dfr)); else if type(num)==2 then, xm=abs(freq(num,poly(1,'z','c'),dfr)); else if type(num)==1 then, xz=poly(num,'z','c'); xm=abs(freq(xz,1,dfr)) else, error('Error---Input arguments wrong data type') end, end, end, else if rhs==3 then, if type(num)==2 then, xm=abs(freq(num,den,dfr)); else if type(num)==1 then, nz=poly(num,'z','c'); dz=poly(den,'z','c'); xm=abs(freq(nz,dz,dfr)); else, error('Error---Input arguments wrong data type') end, end, end, end
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// Example 4_5 clc;funcprot(0); // Given data Q=3500;// kJ V=2;// m^3 v=0.5342;// m^3/kg h_1=2860;// kJ // Calculation m=V/v;// kg h_2=(Q/m)+h_1;// kJ/kg // From the steam tables this interpolates to T_2=600+((92.6/224)*(100));// °C printf("\nThe final temperature,T_2=%3.0f°C",T_2);
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//CIRCULAR LINKED LIST function[link2]=append(ele,link1) link2=list(0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,,0,0); if(link1(1)(1).add==0) link1(1)(1).data=ele; link1(1)(1).add=1; link1(1)(1).nexadd=1; link2(1)=link1(1)(1); else if(link1(1)(1).nexadd==link1(1)(1).add) lin2=link1(1)(1); lin2.data=ele; lin2.add=link1(1)(1).add+1; link1(1)(1).nexadd=lin2.add; lin2.nexadd=link1(1)(1).add; link2(1)=link1(1)(1); link2(2)=lin2; else lin2=link1(1)(1); i=1; while(link1(i)(1).nexadd~=link1(1)(1).add) i=i+1; end j=i; lin2.data=ele; lin2.add=link1(i).add+1; lin2.nexadd=link1(1)(1).add; link1(i).nexadd=lin2.add; link2(1)=link1(1)(1); i=2; while(link1(i).nexadd~=lin2.add) link2(i)=(link1(i)); i=i+1; end link2(i)=link1(i); link2(i+1)=lin2; end end endfunction function[link2]=add(ele,pos,link1); link2=list(0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,,0,0); i=1; while(i<=pos) if(link1(i).nexadd==link1(1)(1).add) break; else i=i+1; end end if(link1(i).nexadd~=link1(1)(1).add) i=i-1; lin2.data=ele; lin2.add=i; j=i; while(link1(j).nexadd~=link1(1)(1).add) link1(j).add=link1(j).add+1; link1(j).nexadd=link1(j).nexadd+1; j=j+1; end link1(j).add=link1(j).add+1; lin2.nexadd=link1(i).add; link1(i-1).nexadd=lin2.add; k=1; while(k<i) link2(k)=link1(k); k=k+1; end link2(k)=lin2; k=k+1; link2(k)=link1(k-1); k=k+1 l=k-1; while(k~=j) link2(k)=link1(l); k=k+1; l=l+1; end link2(j)=link1(j-1);; link2(j+1)=link1(j); else if(i==pos) k=1; lin2.data=ele; lin2.add=link1(i-1).add+1; link1(i).add=link1(i).add+1; lin2.nexadd=link1(i).add; link1(i).nexadd=link1(1)(1).add; k=1; while(k<pos) link2(k)=link1(k); k=k+1; end link2(k)=lin2; link2(k+1)=link1(k) end end endfunction function[link2]=delete1(pos,link1) link2=list(0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0,,0,0); i=1; j=1; while(i<pos) if((link1(j).nexadd==link1(1)(1).add)) j=1; i=i+1; else i=i+1; j=j+1; end end if(link1(j).nexadd~=link1(1)(1).add) k=1; if(j==1) k=2; while(link1(k).nexadd~=link1(1)(1).add) link2(k-1)=link1(k); k=k+1; end link2(k-1)=link1(k); link2(k-1).nexadd=link2(1).add; else lin2=link1(j); link1(j-1).nexadd=link1(j+1).add; k=1; while(link1(k).nexadd~=link1(j+1).add) link2(k)=link1(k); k=k+1; end link2(k)=link1(k); k=k+2; while(link1(k).nexadd~=link1(1)(1).add) link2(k-1)=link1(k); k=k+1; end link2(k-1)=link1(k); end else link1(j-1).nexadd=link1(1)(1).add; l=1; while(link1(l).nexadd~=link1(1)(1).add) link2(l)=link1(l); l=l+1; end link2(l)=link1(l); end endfunction //Calling Routine: link1=struct('data',0,'add',0,'nexadd',0); link1=append(4,link1);//This will actualy create a list and 4 as start link1=append(6,link1); link1=add(10,2,link1); link1=delete1(4,link1);//As the list is circular the 4'th element refers to actualy the 1'st one disp(link1,"After the above manuplations the list is");