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64ef956e0a0fd9a3dc469e321db6fb161f080dbf
a8447bb190e75c3452a418bcdffbb356b7f3ec43
/LTP RAP 3.0napls/comMMNa.sce
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refs/heads/master
2021-01-22T09:58:19.920934
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comMMNa.sce
#it does not match the risto "optimum MMN" paper scenario = "PS3_roving_combination_MMNa_01072015"; #adapted from "nvMMNa5_napls06122009"; #attenuation updated for ER1 insert earphones and X-fi gamer card #Note: this is based on the baldeweg-style of pitch deviance with #the additional constraint that a transition be no more than 300Hz #--- #Modified Jan 2015 to include the new sequences where we have 3, 8, and 33 #standards preceding deviants instead of the previously used 2, 6, and 36 pcl_file = "nvMMNCommands.pcl"; scenario_type = trials ; write_codes = true ; response_matching = simple_matching ; active_buttons = 2; button_codes = 64, 10; target_button_codes = 255,11; pulse_width = 1 ; default_trial_type = fixed ; default_background_color = 0,0,0 ; begin ; #standard tone: sound{ wavefile {filename = "s50.wav" ;} ; attenuation = 0.3 ;} s633 ; #700Hz sound{ wavefile {filename = "f700Hz.wav" ;} ; attenuation = 0.3 ;} f700Hz ; #750Hz sound{ wavefile {filename = "f750Hz.wav" ;} ; attenuation = 0.3 ;} f750Hz ; #800Hz sound{ wavefile {filename = "f800Hz.wav" ;} ; attenuation = 0.3 ;} f800Hz ; #850Hz sound{ wavefile {filename = "f850Hz.wav" ;} ; attenuation = 0.3 ;} f850Hz ; #900Hz sound{ wavefile {filename = "f900Hz.wav" ;} ; attenuation = 0.3 ;} f900Hz ; #950Hz sound{ wavefile {filename = "f950Hz.wav" ;} ; attenuation = 0.3 ;} f950Hz ; #1000Hz sound{ wavefile {filename = "f1000Hz.wav" ;} ; attenuation = 0.3 ;} f1000Hz ; #1050Hz sound{ wavefile {filename = "f1050Hz.wav" ;} ; attenuation = 0.3 ;} f1050Hz ; #1100Hz sound{ wavefile {filename = "f1100Hz.wav" ;} ; attenuation = 0.3 ;} f1100Hz ; #1150Hz sound{ wavefile {filename = "f1150Hz.wav" ;} ; attenuation = 0.3 ;} f1150Hz ; #1200Hz sound{ wavefile {filename = "f1200Hz.wav" ;} ; attenuation = 0.3 ;} f1200Hz ; #1250Hz sound{ wavefile {filename = "f1250Hz.wav" ;} ; attenuation = 0.3 ;} f1250Hz ; #long duration tones: #700Hz sound{ wavefile {filename = "f700Hz100ms.wav" ;} ; attenuation = 0.3 ;} f700Hz100ms ; #750Hz sound{ wavefile {filename = "f750Hz100ms.wav" ;} ; attenuation = 0.3 ;} f750Hz100ms ; #800Hz sound{ wavefile {filename = "f800Hz100ms.wav" ;} ; attenuation = 0.3 ;} f800Hz100ms ; #850Hz sound{ wavefile {filename = "f850Hz100ms.wav" ;} ; attenuation = 0.3 ;} f850Hz100ms ; #900Hz sound{ wavefile {filename = "f900Hz100ms.wav" ;} ; attenuation = 0.3 ;} f900Hz100ms ; #950Hz sound{ wavefile {filename = "f950Hz100ms.wav" ;} ; attenuation = 0.3 ;} f950Hz100ms ; #1000Hz sound{ wavefile {filename = "f1000Hz100ms.wav" ;} ; attenuation = 0.3 ;} f1000Hz100ms ; #1050Hz sound{ wavefile {filename = "f1050Hz100ms.wav" ;} ; attenuation = 0.3 ;} f1050Hz100ms ; #1100Hz sound{ wavefile {filename = "f1100Hz100ms.wav" ;} ; attenuation = 0.3 ;} f1100Hz100ms ; #1150Hz sound{ wavefile {filename = "f1150Hz100ms.wav" ;} ; attenuation = 0.3 ;} f1150Hz100ms ; #1200Hz sound{ wavefile {filename = "f1200Hz100ms.wav" ;} ; attenuation = 0.3 ;} f1200Hz100ms ; #1250Hz sound{ wavefile {filename = "f1250Hz100ms.wav" ;} ; attenuation = 0.3 ;} f1250Hz100ms ; #silence tone placeholder sound{ wavefile {filename = "s50.wav" ;} ; attenuation = 1 ;} silence ; picture{text { caption = "+" ; font_size = 48 ; font_color = 255,255,255 ;} ; x = 0 ; y = 0 ; } default; trial { stimulus_event { picture{text { caption = "3" ; font_size = 48 ; font_color = 255,255,255 ;} ; x = 0 ; y = 0 ;} ; duration = 1500 ; code = "83" ; port_code = 128 ; } ; stimulus_event { picture{text { caption = "2" ; font_size = 48 ; font_color = 255,255,255 ;} ; x = 0 ; y = 0 ;} ; time = 2000 ; duration = 1500 ; code = "82" ; } ; stimulus_event { picture{text { caption = "1" ; font_size = 48 ; font_color = 255,255,255 ;} ; x = 0 ; y = 0 ;} ; time = 4000 ; duration = 1500 ; code = "81" ; } ; } ; constant_force { duration = 100; axes = 7; direction = 0; magnitude = 1.0; # constant force for 125 ms gain = 1.0; } T; constant_force { duration = 100; axes = 7,8; direction = 0; magnitude = 1.0; # constant force for 175 ms gain = 1.0; #envelope params #attack_level = 0.7; #attack_time = 100; #fade_level = 0.0; #fade_time = 100; } N; constant_force { duration = 200; axes = 8; direction = 0; magnitude = 1.0; # constant force for 250 ms } S; TEMPLATE "ps3MMNrov400.tem"{ #pic word picPort wordPort targResp picTime wrdTime snd1 s1Port snd2 s2Port snd3 s3Port snd4 s4Port snd5 s5Port snd6 s6Port ; pic picPort targResp picTime snd1 s1Port snd2 s2Port snd3 s3Port snd4 s4Port; S 50 2 407 f1100Hz 101 f1100Hz 2 f1100Hz 3 f1100Hz 4 ; N 200 2 453 f1100Hz 5 f1100Hz 6 f1100Hz 7 f1100Hz 8 ; S 50 2 63 f900Hz100ms 1 f900Hz100ms 2 f900Hz100ms 3 f800Hz 1 ; S 50 2 457 f800Hz 2 f800Hz 3 f700Hz100ms 1 f700Hz100ms 2 ; S 50 2 316 f700Hz100ms 3 f850Hz 1 f850Hz 2 f850Hz 3 ; S 50 2 49 f850Hz 4 f850Hz 5 f850Hz 6 f850Hz 7 ; T 100 1 139 f850Hz 8 f950Hz100ms 1 f950Hz100ms 2 f950Hz100ms 3 ; S 50 2 273 f950Hz100ms 4 f950Hz100ms 5 f950Hz100ms 6 f950Hz100ms 7 ; S 50 2 479 f950Hz100ms 8 f950Hz100ms 9 f950Hz100ms 10 f950Hz100ms 11 ; S 50 2 482 f950Hz100ms 12 f950Hz100ms 13 f950Hz100ms 14 f950Hz100ms 15 ; S 50 2 79 f950Hz100ms 16 f950Hz100ms 17 f950Hz100ms 18 f950Hz100ms 19 ; S 50 2 485 f950Hz100ms 20 f950Hz100ms 21 f950Hz100ms 22 f950Hz100ms 23 ; T 100 1 479 f950Hz100ms 24 f950Hz100ms 25 f950Hz100ms 26 f950Hz100ms 27 ; S 50 2 243 f950Hz100ms 28 f950Hz100ms 29 f950Hz100ms 30 f950Hz100ms 31 ; S 50 2 300 f950Hz100ms 32 f950Hz100ms 33 f750Hz 1 f750Hz 2 ; S 50 2 71 f750Hz 3 f750Hz 4 f750Hz 5 f750Hz 6 ; N 200 2 211 f750Hz 7 f750Hz 8 f750Hz 9 f750Hz 10 ; S 50 2 458 f750Hz 11 f750Hz 12 f750Hz 13 f750Hz 14 ; S 50 2 396 f750Hz 15 f750Hz 16 f750Hz 17 f750Hz 18 ; S 50 2 480 f750Hz 19 f750Hz 20 f750Hz 21 f750Hz 22 ; S 50 2 328 f750Hz 23 f750Hz 24 f750Hz 25 f750Hz 26 ; S 50 2 18 f750Hz 27 f750Hz 28 f750Hz 29 f750Hz 30 ; S 50 2 425 f750Hz 31 f750Hz 32 f750Hz 33 f1000Hz100ms 1 ; N 200 2 467 f1000Hz100ms 2 f1000Hz100ms 3 f1200Hz 1 f1200Hz 2 ; S 50 2 339 f1200Hz 3 f1200Hz 4 f1200Hz 5 f1200Hz 6 ; S 50 2 379 f1200Hz 7 f1200Hz 8 f1050Hz100ms 1 f1050Hz100ms 2 ; T 100 1 372 f1050Hz100ms 3 f1050Hz100ms 4 f1050Hz100ms 5 f1050Hz100ms 6 ; S 50 2 196 f1050Hz100ms 7 f1050Hz100ms 8 f1050Hz100ms 9 f1050Hz100ms 10 ; S 50 2 328 f1050Hz100ms 11 f1050Hz100ms 12 f1050Hz100ms 13 f1050Hz100ms 14 ; S 50 2 86 f1050Hz100ms 15 f1050Hz100ms 16 f1050Hz100ms 17 f1050Hz100ms 18 ; S 50 2 353 f1050Hz100ms 19 f1050Hz100ms 20 f1050Hz100ms 21 f1050Hz100ms 22 ; S 50 2 16 f1050Hz100ms 23 f1050Hz100ms 24 f1050Hz100ms 25 f1050Hz100ms 26 ; S 50 2 138 f1050Hz100ms 27 f1050Hz100ms 28 f1050Hz100ms 29 f1050Hz100ms 30 ; T 100 1 23 f1050Hz100ms 31 f1050Hz100ms 32 f1050Hz100ms 33 f900Hz 1 ; S 50 2 49 f900Hz 2 f900Hz 3 f900Hz 4 f900Hz 5 ; S 50 2 412 f900Hz 6 f900Hz 7 f900Hz 8 f900Hz 9 ; T 100 1 347 f900Hz 10 f900Hz 11 f900Hz 12 f900Hz 13 ; S 50 2 159 f900Hz 14 f900Hz 15 f900Hz 16 f900Hz 17 ; S 50 2 475 f900Hz 18 f900Hz 19 f900Hz 20 f900Hz 21 ; S 50 2 17 f900Hz 22 f900Hz 23 f900Hz 24 f900Hz 25 ; S 50 2 219 f900Hz 26 f900Hz 27 f900Hz 28 f900Hz 29 ; S 50 2 191 f900Hz 30 f900Hz 31 f900Hz 32 f900Hz 33 ; S 50 2 383 f1200Hz100ms 1 f1200Hz100ms 2 f1200Hz100ms 3 f1200Hz100ms 4 ; T 100 1 398 f1200Hz100ms 5 f1200Hz100ms 6 f1200Hz100ms 7 f1200Hz100ms 8 ; S 50 2 93 f1200Hz100ms 9 f1200Hz100ms 10 f1200Hz100ms 11 f1200Hz100ms 12 ; S 50 2 245 f1200Hz100ms 13 f1200Hz100ms 14 f1200Hz100ms 15 f1200Hz100ms 16 ; S 50 2 223 f1200Hz100ms 17 f1200Hz100ms 18 f1200Hz100ms 19 f1200Hz100ms 20 ; S 50 2 323 f1200Hz100ms 21 f1200Hz100ms 22 f1200Hz100ms 23 f1200Hz100ms 24 ; N 200 2 355 f1200Hz100ms 25 f1200Hz100ms 26 f1200Hz100ms 27 f1200Hz100ms 28 ; S 50 2 377 f1200Hz100ms 29 f1200Hz100ms 30 f1200Hz100ms 31 f1200Hz100ms 32 ; S 50 2 138 f1200Hz100ms 33 f950Hz 1 f950Hz 2 f950Hz 3 ; T 100 1 340 f950Hz 4 f950Hz 5 f950Hz 6 f950Hz 7 ; S 50 2 328 f950Hz 8 f950Hz 9 f950Hz 10 f950Hz 11 ; S 50 2 81 f950Hz 12 f950Hz 13 f950Hz 14 f950Hz 15 ; S 50 2 59 f950Hz 16 f950Hz 17 f950Hz 18 f950Hz 19 ; N 200 2 249 f950Hz 20 f950Hz 21 f950Hz 22 f950Hz 23 ; S 50 2 480 f950Hz 24 f950Hz 25 f950Hz 26 f950Hz 27 ; S 50 2 170 f950Hz 28 f950Hz 29 f950Hz 30 f950Hz 31 ; S 50 2 293 f950Hz 32 f950Hz 33 f1250Hz100ms 1 f1250Hz100ms 2 ; S 50 2 112 f1250Hz100ms 3 f1250Hz100ms 4 f1250Hz100ms 5 f1250Hz100ms 6 ; S 50 2 376 f1250Hz100ms 7 f1250Hz100ms 8 f1250Hz100ms 9 f1250Hz100ms 10 ; S 50 2 128 f1250Hz100ms 11 f1250Hz100ms 12 f1250Hz100ms 13 f1250Hz100ms 14 ; S 50 2 253 f1250Hz100ms 15 f1250Hz100ms 16 f1250Hz100ms 17 f1250Hz100ms 18 ; T 100 1 350 f1250Hz100ms 19 f1250Hz100ms 20 f1250Hz100ms 21 f1250Hz100ms 22 ; S 50 2 445 f1250Hz100ms 23 f1250Hz100ms 24 f1250Hz100ms 25 f1250Hz100ms 26 ; N 200 2 480 f1250Hz100ms 27 f1250Hz100ms 28 f1250Hz100ms 29 f1250Hz100ms 30 ; S 50 2 274 f1250Hz100ms 31 f1250Hz100ms 32 f1250Hz100ms 33 f1150Hz 1 ; T 100 1 69 f1150Hz 2 f1150Hz 3 f950Hz100ms 1 f950Hz100ms 2 ; S 50 2 75 f950Hz100ms 3 f950Hz100ms 4 f950Hz100ms 5 f950Hz100ms 6 ; S 50 2 129 f950Hz100ms 7 f950Hz100ms 8 f1050Hz 1 f1050Hz 2 ; S 50 2 420 f1050Hz 3 f1050Hz 4 f1050Hz 5 f1050Hz 6 ; S 50 2 127 f1050Hz 7 f1050Hz 8 f1050Hz 9 f1050Hz 10 ; S 50 2 407 f1050Hz 11 f1050Hz 12 f1050Hz 13 f1050Hz 14 ; S 50 2 122 f1050Hz 15 f1050Hz 16 f1050Hz 17 f1050Hz 18 ; S 50 2 465 f1050Hz 19 f1050Hz 20 f1050Hz 21 f1050Hz 22 ; N 200 2 175 f1050Hz 23 f1050Hz 24 f1050Hz 25 f1050Hz 26 ; S 50 2 98 f1050Hz 27 f1050Hz 28 f1050Hz 29 f1050Hz 30 ; S 50 2 126 f1050Hz 31 f1050Hz 32 f1050Hz 33 f850Hz100ms 1 ; S 50 2 308 f850Hz100ms 2 f850Hz100ms 3 f750Hz 1 f750Hz 2 ; S 50 2 237 f750Hz 3 f750Hz 4 f750Hz 5 f750Hz 6 ; S 50 2 176 f750Hz 7 f750Hz 8 f1050Hz100ms 1 f1050Hz100ms 2 ; S 50 2 415 f1050Hz100ms 3 f1050Hz100ms 4 f1050Hz100ms 5 f1050Hz100ms 6 ; N 200 2 293 f1050Hz100ms 7 f1050Hz100ms 8 f850Hz 1 f850Hz 2 ; S 50 2 275 f850Hz 3 f850Hz 4 f850Hz 5 f850Hz 6 ; S 50 2 459 f850Hz 7 f850Hz 8 f1050Hz100ms 1 f1050Hz100ms 2 ; S 50 2 143 f1050Hz100ms 3 f1050Hz100ms 4 f1050Hz100ms 5 f1050Hz100ms 6 ; T 100 1 379 f1050Hz100ms 7 f1050Hz100ms 8 f850Hz 1 f850Hz 2 ; S 50 2 377 f850Hz 3 f1150Hz100ms 1 f1150Hz100ms 2 f1150Hz100ms 3 ; S 50 2 190 f1150Hz100ms 4 f1150Hz100ms 5 f1150Hz100ms 6 f1150Hz100ms 7 ; S 50 2 284 f1150Hz100ms 8 f900Hz 1 f900Hz 2 f900Hz 3 ; S 50 2 38 f900Hz 4 f900Hz 5 f900Hz 6 f900Hz 7 ; S 50 2 27 f900Hz 8 f750Hz100ms 1 f750Hz100ms 2 f750Hz100ms 3 ; S 50 2 265 f750Hz100ms 4 f750Hz100ms 5 f750Hz100ms 6 f750Hz100ms 7 ; S 50 2 390 f750Hz100ms 8 f750Hz100ms 9 f750Hz100ms 10 f750Hz100ms 11 ; S 50 2 467 f750Hz100ms 12 f750Hz100ms 13 f750Hz100ms 14 f750Hz100ms 15 ; T 100 1 65 f750Hz100ms 16 f750Hz100ms 17 f750Hz100ms 18 f750Hz100ms 19 ; S 50 2 284 f750Hz100ms 20 f750Hz100ms 21 f750Hz100ms 22 f750Hz100ms 23 ; S 50 2 235 f750Hz100ms 24 f750Hz100ms 25 f750Hz100ms 26 f750Hz100ms 27 ; S 50 2 166 f750Hz100ms 28 f750Hz100ms 29 f750Hz100ms 30 f750Hz100ms 31 ; S 50 2 169 f750Hz100ms 32 f750Hz100ms 33 f1050Hz 1 f1050Hz 2 ; N 200 2 81 f1050Hz 3 f1050Hz 4 f1050Hz 5 f1050Hz 6 ; S 50 2 397 f1050Hz 7 f1050Hz 8 f1200Hz100ms 1 f1200Hz100ms 2 ; S 50 2 156 f1200Hz100ms 3 f1200Hz100ms 4 f1200Hz100ms 5 f1200Hz100ms 6 ; S 50 2 264 f1200Hz100ms 7 f1200Hz100ms 8 f1000Hz 1 f1000Hz 2 ; S 50 2 83 f1000Hz 3 f1000Hz 4 f1000Hz 5 f1000Hz 6 ; N 200 2 301 f1000Hz 7 f1000Hz 8 f1000Hz 9 f1000Hz 10 ; S 50 2 131 f1000Hz 11 f1000Hz 12 f1000Hz 13 f1000Hz 14 ; S 50 2 327 f1000Hz 15 f1000Hz 16 f1000Hz 17 f1000Hz 18 ; S 50 2 345 f1000Hz 19 f1000Hz 20 f1000Hz 21 f1000Hz 22 ; N 200 2 374 f1000Hz 23 f1000Hz 24 f1000Hz 25 f1000Hz 26 ; S 50 2 225 f1000Hz 27 f1000Hz 28 f1000Hz 29 f1000Hz 30 ; S 50 2 42 f1000Hz 31 f1000Hz 32 f1000Hz 33 f1250Hz100ms 1 ; T 100 1 114 f1250Hz100ms 2 f1250Hz100ms 3 f1000Hz 1 f1000Hz 2 ; S 50 2 457 f1000Hz 3 f1200Hz100ms 1 f1200Hz100ms 2 f1200Hz100ms 3 ; S 50 2 76 f1100Hz 1 f1100Hz 2 f1100Hz 3 f800Hz100ms 1 ; S 50 2 413 f800Hz100ms 2 f800Hz100ms 3 f950Hz 1 f950Hz 2 ; S 50 2 269 f950Hz 3 f950Hz 4 f950Hz 5 f950Hz 6 ; S 50 2 498 f950Hz 7 f950Hz 8 f950Hz 9 f950Hz 10 ; S 50 2 39 f950Hz 11 f950Hz 12 f950Hz 13 f950Hz 14 ; S 50 2 221 f950Hz 15 f950Hz 16 f950Hz 17 f950Hz 18 ; N 200 2 53 f950Hz 19 f950Hz 20 f950Hz 21 f950Hz 22 ; S 50 2 481 f950Hz 23 f950Hz 24 f950Hz 25 f950Hz 26 ; S 50 2 222 f950Hz 27 f950Hz 28 f950Hz 29 f950Hz 30 ; S 50 2 387 f950Hz 31 f950Hz 32 f950Hz 33 f1250Hz100ms 1 ; T 100 1 409 f1250Hz100ms 2 f1250Hz100ms 3 f1250Hz100ms 4 f1250Hz100ms 5 ; S 50 2 434 f1250Hz100ms 6 f1250Hz100ms 7 f1250Hz100ms 8 f1000Hz 1 ; S 50 2 42 f1000Hz 2 f1000Hz 3 f1000Hz 4 f1000Hz 5 ; S 50 2 200 f1000Hz 6 f1000Hz 7 f1000Hz 8 f900Hz100ms 1 ; S 50 2 130 f900Hz100ms 2 f900Hz100ms 3 f1150Hz 1 f1150Hz 2 ; N 200 2 500 f1150Hz 3 f1250Hz100ms 1 f1250Hz100ms 2 f1250Hz100ms 3 ; S 50 2 216 f1250Hz100ms 4 f1250Hz100ms 5 f1250Hz100ms 6 f1250Hz100ms 7 ; S 50 2 455 f1250Hz100ms 8 f1100Hz 1 f1100Hz 2 f1100Hz 3 ; S 50 2 91 f1100Hz 4 f1100Hz 5 f1100Hz 6 f1100Hz 7 ; S 50 2 132 f1100Hz 8 f1100Hz 9 f1100Hz 10 f1100Hz 11 ; N 200 2 73 f1100Hz 12 f1100Hz 13 f1100Hz 14 f1100Hz 15 ; S 50 2 68 f1100Hz 16 f1100Hz 17 f1100Hz 18 f1100Hz 19 ; S 50 2 435 f1100Hz 20 f1100Hz 21 f1100Hz 22 f1100Hz 23 ; S 50 2 290 f1100Hz 24 f1100Hz 25 f1100Hz 26 f1100Hz 27 ; S 50 2 275 f1100Hz 28 f1100Hz 29 f1100Hz 30 f1100Hz 31 ; S 50 2 72 f1100Hz 32 f1100Hz 33 f950Hz100ms 1 f950Hz100ms 2 ; S 50 2 427 f950Hz100ms 3 f800Hz 1 f800Hz 2 f800Hz 3 ; N 200 2 311 f800Hz 4 f800Hz 5 f800Hz 6 f800Hz 7 ; S 50 2 175 f800Hz 8 f800Hz 9 f800Hz 10 f800Hz 11 ; S 50 2 257 f800Hz 12 f800Hz 13 f800Hz 14 f800Hz 15 ; T 100 1 201 f800Hz 16 f800Hz 17 f800Hz 18 f800Hz 19 ; S 50 2 38 f800Hz 20 f800Hz 21 f800Hz 22 f800Hz 23 ; S 50 2 120 f800Hz 24 f800Hz 25 f800Hz 26 f800Hz 27 ; T 100 1 62 f800Hz 28 f800Hz 29 f800Hz 30 f800Hz 31 ; S 50 2 92 f800Hz 32 f800Hz 33 f1100Hz100ms 1 f1100Hz100ms 2 ; S 50 2 120 f1100Hz100ms 3 f1100Hz100ms 4 f1100Hz100ms 5 f1100Hz100ms 6 ; S 50 2 451 f1100Hz100ms 7 f1100Hz100ms 8 f1200Hz 1 f1200Hz 2 ; S 50 2 472 f1200Hz 3 f1200Hz 4 f1200Hz 5 f1200Hz 6 ; S 50 2 245 f1200Hz 7 f1200Hz 8 f1050Hz100ms 1 f1050Hz100ms 2 ; N 200 2 245 f1050Hz100ms 3 f800Hz 1 f800Hz 2 f800Hz 3 ; S 50 2 169 f800Hz 4 f800Hz 5 f800Hz 6 f800Hz 7 ; S 50 2 450 f800Hz 8 f800Hz 9 f800Hz 10 f800Hz 11 ; T 100 1 185 f800Hz 12 f800Hz 13 f800Hz 14 f800Hz 15 ; S 50 2 56 f800Hz 16 f800Hz 17 f800Hz 18 f800Hz 19 ; S 50 2 390 f800Hz 20 f800Hz 21 f800Hz 22 f800Hz 23 ; S 50 2 195 f800Hz 24 f800Hz 25 f800Hz 26 f800Hz 27 ; T 100 1 121 f800Hz 28 f800Hz 29 f800Hz 30 f800Hz 31 ; S 50 2 202 f800Hz 32 f800Hz 33 f950Hz100ms 1 f950Hz100ms 2 ; S 50 2 48 f950Hz100ms 3 f950Hz100ms 4 f950Hz100ms 5 f950Hz100ms 6 ; S 50 2 66 f950Hz100ms 7 f950Hz100ms 8 f950Hz100ms 9 f950Hz100ms 10 ; S 50 2 471 f950Hz100ms 11 f950Hz100ms 12 f950Hz100ms 13 f950Hz100ms 14 ; S 50 2 478 f950Hz100ms 15 f950Hz100ms 16 f950Hz100ms 17 f950Hz100ms 18 ; S 50 2 288 f950Hz100ms 19 f950Hz100ms 20 f950Hz100ms 21 f950Hz100ms 22 ; N 200 2 30 f950Hz100ms 23 f950Hz100ms 24 f950Hz100ms 25 f950Hz100ms 26 ; S 50 2 117 f950Hz100ms 27 f950Hz100ms 28 f950Hz100ms 29 f950Hz100ms 30 ; S 50 2 177 f950Hz100ms 31 f950Hz100ms 32 f950Hz100ms 33 f1100Hz 1 ; S 50 2 411 f1100Hz 2 f1100Hz 3 f1100Hz 4 f1100Hz 5 ; S 50 2 8 f1100Hz 6 f1100Hz 7 f1100Hz 8 f1100Hz 9 ; S 50 2 22 f1100Hz 10 f1100Hz 11 f1100Hz 12 f1100Hz 13 ; S 50 2 84 f1100Hz 14 f1100Hz 15 f1100Hz 16 f1100Hz 17 ; N 200 2 325 f1100Hz 18 f1100Hz 19 f1100Hz 20 f1100Hz 21 ; S 50 2 366 f1100Hz 22 f1100Hz 23 f1100Hz 24 f1100Hz 25 ; S 50 2 324 f1100Hz 26 f1100Hz 27 f1100Hz 28 f1100Hz 29 ; S 50 2 225 f1100Hz 30 f1100Hz 31 f1100Hz 32 f1100Hz 33 ; T 100 1 274 f800Hz100ms 1 f800Hz100ms 2 f800Hz100ms 3 f700Hz 1 ; S 50 2 148 f700Hz 2 f700Hz 3 f700Hz 4 f700Hz 5 ; S 50 2 372 f700Hz 6 f700Hz 7 f700Hz 8 f700Hz 9 ; 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S 50 2 397 f850Hz100ms 30 f850Hz100ms 31 f850Hz100ms 32 f850Hz100ms 33 ; } ; trial { stimulus_event { picture{ text { caption = "+"; font_size = 28; font_color = 255,255,255; }; x = 0; y = 0; }; time = 2000; duration = 1000; port_code = 129; }; };
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//Section-14,Example-2,Page no.-PC.129 //To find the Molarity of given sulphuric acid solution. clc; N_T=0.1354 V_T=42.20 V_S=50.00 //N_S=N_H_2SO_4(let) and M_S=M_H_2SO_4 N_S=(N_T*V_T)/V_S M_S=(N_S/2) disp(M_S,'Molarity of H_2SO_4')
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inf = float('inf') # sampling time delta_t = 0.5 # pvt simulator state required for initializing the simulator plant_pvt_init_data = None ############################# # P1: Property Description ############################# # Time Horizon T = 30.0 # Rectangular bounds on initial plant states X0[0, :] <= X <= X0[1, :] # [plant outputs, plant states] # vehicle speed[output], wheel speed, engine rpm initial_set = [[0.0, 10.0, 1000.0], [0.0, 10.0, 1000.0]] # Unsafe Boxed Region error_set = [[-inf, -inf, 3000.0], [inf, inf, 4000.0]] # rectangular bounds on exogenous inputs to the contorller. Such as, controller # disturbance: Throttle, Brake Torque ci = [[0.0, 0.0],[100.0, 300]] ############################ # Results Scratchpad: # vio = _/100k took _ mins [plotting, logging?] # SS = falsified in _ [plotting, logging?] # grid_eps = <[0.0, 0.0]> # num_samples = <2> # SS + symex: falsified in _ [plotting, logging?] ######################## # Abstraction Params ######################## # initial abstraction grid size grid_eps = [100.0, 5.0, 1000.0] min_smt_sample_dist = 1.0; # number of samples at every scatter step num_samples = 1 # maximum iteration before SS iter outs. MAX_ITER = 5 # minDist=0.05 ######################## # initial controller states which are C ints # temporalCounter_i1, is_active_c1_shift_controller, is_gear_state, is_active_gear_state, # is_selection_state, is_active_selection_state initial_controller_integer_state = [0]*6 # initial controller states which are C doubles # disturbance[0], disturbance[1], Gear initial_controller_float_state = [0.0]*3 # number of control inputs to the plant num_control_inputs = 3 ################################ # Unimplemented ################################ # Initial plant discrete state: List all states initial_discrete_state = [0] # Rectangularly bounded exogenous inputs to the plant (plant noise). pi = [[],[]] # Initial pvt simulator state, associated with with an execution trace. initial_pvt_states = [] ################################ ################ # Simulators ################ ## Plant ## # is the plant simulator implemented in Python(python) or Matlab(matlab)? plant_description = 'matlab' # relative/absolute path for the simulator file containing sim() plant_path = 'plant.m' ## Controller ## # relative/absolute path for the controller .so controller_path = 'autotrans_controller.so' # relative path for the directory containing smt2 files for each path controller_path_dir_path = './paths' ############### ################ # DO NOT MODIFY ################ #CONVERSION_FACTOR = 1.0 refinement_factor = 2.0
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//Scilab Code for Example 4.5 of Signals and systems by //P.Ramakrishna Rao //x(t)=cos pi*t, |t|>0.5, zero otherwise clear; clc; //Fourier Transform for f=-20:1:20; X(f+21)=integrate('cos(%pi*t)*cos(2*%pi*f*t)','t',-0.5,0.5); end disp(X,'X(0)-->X(20)'); t=-0.5:0.01:0.5; q=cos(%pi*t); a = gca (); a.y_location ="origin"; a.x_location ="origin"; plot(t,q); xlabel ( 'Time in Seconds' ); title ('Signal x(t)'); figure(1); a = gca (); a.y_location ="origin"; a.x_location ="origin"; f=-20:1:20; plot (f, X); xlabel ( 'Frequency in Hz ' ); title ('Continuous Time Fourier Transform X(jW)');
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//Resistance R, Voltage V close(); clear; clc; V = 110;//V //From previous question Rao = 1.5;//ohm Rbo = 1; Rco = 3; Rcd = 3; Rth = Rao + Rbo*(Rco+Rcd)/(Rbo+Rco+Rcd); //For maximum power Rad = Rth; mprintf('Rad = %0.2f ohm',Rad);
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clc //initialisation of variables clear W= 38 //rev/sec w= 62.4 //lbf/ft^3 m= 2000 //lbm/sec g= 32.2 //ft/sec^2 ps= 5000 //lbf/ft^2 S3= 4.6 e= 0.91 //CALCULATIONS S1= W*(w*m^2/(g*ps)^3)^0.25 D= S3*(m^2/(w*g*ps))^0.25 //RESULTS printf ('S1 = %.3f',S1) printf ('\n Diameter = %.2f ft',D) printf ('\n efficiency = %.2f ',e)
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// Exa 1.26 format('v',7); clc; clear; close; // Given data // omega_t= Ao*omega_b // 2*%pi*f_t = Ao*2*%pi*f_b // f_t= Ao*f_b // Part (i) Ao1= 10^5; f_b1= 10^2;// in Hz f_t1= Ao1*f_b1;// in Hz // Part (ii) Ao2= 10^6; f_t2= 10^6;// in Hz f_b2= f_t2/Ao2;// in Hz // Part (iii) f_b3= 10^3;// in Hz f_t3= 10^8;// in Hz Ao3= f_t3/f_b3; // Part (iv) f_b4= 10^-1;// in Hz f_t4= 10^6;// in Hz Ao4= f_t4/f_b4; // Part (v) Ao5= 2*10^5; f_b5= 10;// in Hz f_t5= Ao5*f_b5;// in Hz disp(f_t1,"The value of f_t1 in Hz is : ") disp(f_b2,"The value of f_b2 in Hz is : ") disp(Ao3,"The value of Ao3 is : ") disp(Ao4,"The value of Ao4 is : ") disp(f_t5,"The value of f_t5 in Hz is : ")
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syms s U T=(2*s^2+s+5)/(s^3+6*s^2+11*s+4) disp("state modle is") A=[0 1 0; 0 0 1; -4 -11 -6] B=[0;0;1]*U X=[X1;X2;X3] C=[5 1 2] D=0 disp(A*X+B,"[diff(X1);diff(X2);diff(X3)]=") disp(C*X+D,"and Y = ")
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clc; clear; //Example3.2 //Given mu=15*10^-6 //sq m /s v=2 //m/s L=2 //[m] length of plate Nre_x=3*10^5 xc=Nre_x*mu/v //critical length at whihc the transition takes place //Since xc is less than 2 m.Therefore the flow is laminar //at any distance x,.it is calculated from //del/x=4.64/(sqrt(NRe,x)) //At x=L=2 m Nre_l=v*L/mu del_l=4.64*L/sqrt(Nre_l) del_l=del_l*1000 //[mm] printf("Boundary layerthickness at the trailing edge is %f mm",del_l);
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// Book - Power System: Analysis & Design 5th Edition // Authors - J. Duncan Glover, Mulukutla S. Sharma, Thomas J. Overbye // Chapter - 4 : Example 4.3 // Scilab Version 6.0.0 : OS - Windows clc; clear; f = 60; // Single Phase line operating fruquency in Hz S = 12; // Strand Copper conductors Dxy = 5; // Geometrical Mean Distance between conductor centers in ft Dxx =0.01750; // Geometrical Mean Radiance of Copper Conductor in feet from Table A.3 Dyy = Dxx; l = 20; // Line length in miles Lx = (2*10^-7)*log(Dxy/Dxx)*1609*l; // Line Inductance in Henry per conductor Ly = Lx; L = Lx+Ly; // Total Inductance in Henry per Circuit Xl = (2*%pi*f*L); // Total Inductive Reactance in Ohm per circuit printf('Line Inductance is (Lx) = %f H per conductor',Lx); printf('\nTotal Inductance is (L) = %0.5f H per circuit',L); printf('\nTotal Inductive Reactance is (Xl) = %0.2f Ohm per circuit',Xl);
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###grammar S -> a B C B -> b B -> C -> c C -> ###input a ###pformat S( a B() C() ) ###pformat_ext S( #1 a B( #3 ) C( #5 ) )
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// Example 7.16:oscillation frequency clc; clear; close; C1=120;//capacitance of tunned circuit in PICO farad C2=1500;//capacitance of tunned circuit in pico farad C3=15;//capacitance of tunned circuit in pico farad Cx=(C1*C2)/(C1+C2);//capacitance in pico farad Ct=(Cx*C3)/(Cx+C3);//total capacitance in pico farad L=10;//INDUCTANCE of tunned circuit in micro henry fo=(1/(2*%pi*sqrt(L*10^-6*Ct*10^-12)))*10^-6;//tunned frequency in mega hertz foa= (1/(2*%pi*sqrt(L*10^-6*C3*10^-12)))*10^-6;//actual resonant frequency in mega hertz disp(fo,"tunned frequency in killo mega is") disp(foa,"actual resonant frequency in mega hertz")
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clc mode(1) pause //Zadatak 1 //a 3*456/23+31.54+2^6 //b sqrt(2)*log(10) //c cos(%pi/3)+sin(%pi/2)*exp(3) //d atan(5)+log10(20) pause //Zadatak 2 //a zeros(5,9) //b ones(7,2) //c eye(5,5) //d A=[1, -4*%i, sqrt(2); log(-1), sin(%pi/2), cos(%pi/3);asin(0.5), acos(0.8),exp(0.8)] pause //Zadatak 3 //a A.' //b A' //c A-A.' //d A*A.' A.'*A //e det(A) sum(A) sum(A,1) sum(A,2) pause //Zadatak 4 //a A(2,:) //b A(:,3) //c A(2,3) //d B=A(1:2,2:3) pause //Zadatak 5 a=[ones(1,3);3*ones(1,3);2*ones(1,3)] b=[9:-1:7;6:-1:4;3:-1:1] //a c=cos(b) //b c=sin(b).*cos(a) //c c=b^(1/5) //d c=a.^(1/3) pause //Zadatak 6 //a a=1:50 //b b=49:-1:0 //c c=0:5:45 pause //Zadatak 7 //a x=-%pi:%pi/50:%pi; y=cos(x); plot(x,y) pause clf //b x=linspace(1,7,100); y=sin(1 ./ x); plot(x,y,'k') pause //c y= sin(2*x); plot(x,y,'bo') pause clf //Zadatak 8 x=linspace(-8,8,100); y=linspace(-8,8,100); [X,Y]=meshgrid(x,y); Z=X.^2+Y.^2; surf(X,Y,Z); pause //Zadatak 9 //a function [zbir,razlika] = Rezultat(x,y) zbir=x+y; razlika=x-y; endfunction //Primjer [z,r]=Rezultat(5,3) pause //b function [s] = Suma (A) s=0; for i=1:size(A,'r') for j=1:size(A,'c') s=s+A(i,j); end; end; endfunction //Primjer Suma(A) pause //Zadatak 10 //a function [] = z10a(s) x=linspace(-2,2,100); y=evstr(s); subplot(1,2,1); plot(x,y,'b'); subplot(1,2,2); plot(x,y,'k+'); endfunction z10a('x^2') pause clf //b function [] = z10b(s) X=linspace(-4,4,100); Y=linspace(-4,4,100); [x,y]=meshgrid(X,Y); z=evstr(s) surf(x,y,z); endfunction z10b('x.^2+y.^2')
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clc //initialisation of variables M= 38.3 //mg cm^-1 d= 13.55 //g cm^-3 p= 0.9982 //g cm^-3 g= 980.7 //cm/sec^2 l= 4.96 //cm //CALCULATIONS r= sqrt(M*10^-3/(d*%pi)) R= r*p*g*l/2 //RESULTS printf (' surface tension = %.1f ergs cm^-2 ',R)
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function [fd,err]=savevtk_xyv(x,y,vx,vy,VarName) // Save Sci variables in VTK format // x is a list of points // y is a list of values in the x points // VarName is the Variable Name // Example: // // mtst=[11 12 13 14; 21 22 23 24]; // [sy,sx]=size(mtst); // savevtk_xyv(1:sx,1:sy,mtst,mtst,'2DVectors'); // // Coded by Sebastian Jardi Estadella // http://www.tinet.org/~sje/index_en.htm // // rotates the matrix -90 º. vx=vx'; vy=vy'; nx=length(x); ny=length(y); [nfvx,ncvx]=size(vx); // number for rows and columns [nfvy,ncvy]=size(vy); if nx<>ncvx then disp('length(x) and ncvx have to be equals.'); disp(nx); disp(ncvx); abort; end if nx<>ncvy then disp('length(x) and ncvy have to be equals.'); disp(nx); disp(ncvy); abort; end if ny<>nfvx then disp('length(x) and nfvx have to be equals.'); disp(ny); disp(nfvx); abort; end if ny<>nfvy then disp('length(x) and nfvy have to be equals.'); disp(ny); disp(nfvy); abort; end filename=sprintf('%s.vtk',VarName); mputl('# vtk DataFile Version 2.0',filename); // Delete previous content in filename [fd,err]=mopen(filename, 'a'); // Opens the file to Append. mfprintf(fd,'Structured Grid\n'); mfprintf(fd,'ASCII\n'); mfprintf(fd,'\n'); mfprintf(fd,'DATASET RECTILINEAR_GRID\n'); mfprintf(fd,'DIMENSIONS %d %d %d\n',nx,ny,1); //?? mfprintf(fd,'X_COORDINATES %d double\n',nx); for i=1:nx mfprintf(fd,'%f\n',x(i)); end mfprintf(fd,'\n'); mfprintf(fd,'Y_COORDINATES %d double\n',ny); for i=1:ny mfprintf(fd,'%f\n',y(i)); end mfprintf(fd,'\n'); mfprintf(fd,'Z_COORDINATES 1 double\n'); mfprintf(fd,'0 \n'); mfprintf(fd,'\n'); mfprintf(fd,'POINT_DATA %d\n',nx*ny); mfprintf(fd,'VECTORS '); mfprintf(fd,VarName); mfprintf(fd,' double\n'); for i_f=1:nfvx for i_c=1:ncvx mfprintf(fd,'%f %f 0.0\n',vx(i_f,i_c),vy(i_f,i_c)); end end mfprintf(fd,'\n'); err=mclose(fd); endfunction
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ex11_3.sce
errcatch(-1,"stop");mode(2);// Example 11.3, page no-332 ts=937//MPa bhn=ts/3.45 printf("The Brinell Hardness Number is %.2f",bhn) exit();
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Ex2_6.sce
//To find the voltage V_0 in the given circuit. clc; R=30 Z=[31 -13 0 0 0 -10 0 0 0;-13 35 -9 0 -11 0 0 0 0;0 -9 31 -10 0 0 0 0 0;0 0 -10 79 -30 0 0 0 -9;0 -11 0 -30 53 -7 0 -5 0;-10 0 0 0 -7 47 -30 0 0;0 0 0 0 0 -30 41 0 0;0 0 0 0 -5 0 0 27 -2;0 0 0 -9 0 0 0 -2 29] D=det(Z) Z_4=[31 -13 0 -15 0 -10 0 0 0;-13 35 -9 27 -11 0 0 0 0;0 -9 31 -23 0 0 0 0 0;0 0 -10 0 -30 0 0 0 -9;0 -11 0 -20 53 -7 0 -5 0;-10 0 0 12 -7 47 -30 0 0;0 0 0 -7 0 -30 41 0 0;0 0 0 7 -5 0 0 27 -2;0 0 0 -10 0 0 0 -2 29] D_4=det(Z_4) i_4=D_4/D //Current(A) V_0=R*i_4 disp(V_0,'Required voltage(V)') //Negative sign indicates opposite direction of current. //Answer in the book is wrong.
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Ex2_1.sce
//Chapter 2: Antenna Basics //Example 2-3.1 clc; //Variable Initialization e_half_power = 1/sqrt(2) //E(theta) at half power (relative quantity) //Calculation theta = acos(sqrt(e_half_power)) // theta (radians) hpbw = 2*theta*180/%pi // Half power beamwidth (degrees) //Result mprintf("The Half Power Beamwidth is %.0f degrees",hpbw)
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EX2_3_c.sce
clc; t=-12:0.01:12 x=sin(2*t)+cos(t)+0.5*(sin(3*t)-sin(t)) h=-sin(2*t)+cos(t)-0.5*(sin(3*t)-sin(t)) e=cos(t)//(x+h)/2 o=(x-h)/2//sin(t)+0.5*(sin(3*t)-sin(t)) subplot(3,1,1) plot(t,e) xtitle('even signal') subplot(3,1,2) plot(t,o) xtitle('odd signal')
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Ex5_9.sce
// Display mode mode(0); // Display warning for floating point exception ieee(1); clear; clc; disp("Engineering Thermodynamics by Onkar Singh Chapter 5 Example 9") T1=500;//temperature of system in K T2=300;//temperature of reservoir in K disp("system and reservoir can be treated as source and sink.device thought of can be a carnot engine operating between these two limits.maximum heat available from system shall be the heat rejected till its temperature drops from 500 K to 300 K") disp("therefore,maximum heat(Q1)=(C*dT)in J") disp("here C=0.05*T^2+0.10*T+0.085 in J/K") disp("so Q1=(0.05*T^2+0.10*T+0.085)*dT") function y = f(T), y = (0.05*T^2+0.10*T+0.085), endfunction Q1 = intg(T1, T2, f) Q1=-Q1 disp("entropy change of system,deltaS_system=C*dT/T in J/K") disp("so deltaS_system=(0.05*T^2+0.10*T+0.085)*dT/T") function y = k(T), y = (0.05*T^2+0.10*T+0.085)/T, endfunction deltaS_system = intg(T1, T2, k) disp("deltaS_reservoir=Q2/T2=(Q1-W)/T2") disp("also,we know from entropy principle,deltaS_universe is greater than equal to 0") disp("deltaS_universe=deltaS_system+deltaS_reservoir") disp("thus,upon substituting,deltaS_system+deltaS_reservoir is greater than equal to 0") disp("W is less than or equal to(Q1+deltaS_system*T2)/1000 in KJ") W=(Q1+deltaS_system*T2)/1000 disp("hence maximum work=W in KJ") W
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Chapter16_example2.sce
clc clear //Input data T1=(50+273)//Initial temperature of the liquid in K M1=0.1//Mass of water in kg T2=(40+273)//Final temperature of the liquid in K t1=(5*60)//Time taken by the water to cool from 50 degrees C to 40 degrees C M2=0.085//Mass of the liquid in kg M=0.1//Mass of the calorimeter in kg t2=(2*60)//Time taken by the liquid to cool from 50 degrees C to 40 degrees C S=385//Specific heat of the calorimeter in J/kg.K S1=4190//Specific heat of the water in J/kg.K //Calculations S2=(((M1*S1+M*S)*(t2/t1))-(M*S))/M2//Specific heat of the liquid in J/kg.K //Output printf('Specific heat of the liquid is %3.0f J/kg.K',S2)
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eventual.sce
// 最終スライディングモード制御 L=[1 0; 0 1]; // 入力行列(アクチュエータに加わる力を表す行列) k=10; //到達則のスカラ関数 m1=1; m2=1; //質量 k1=1; k2=2; //ばね定数 d1=1; d2=2; //減衰定数 M=[m1 0; 0 m2]; // K = [k1 -k1; -k1 k1+k2]; D = [d1 -d1; -d1 d1+d2]; AF = [zeros(2,2) eye(2,2); -M*K -M*D]; BF = [zeros(2,2); L ]; // 平滑関数のパラメータ(チャタリング除去用) P=4; Q=1; // 切換超平面Sの定義(極配置法で設計済) S1=[4 0; 0 3]; S2=[eye(2,2)]; S = [S1 S2]; //切換超平面 // コンソールでフィードバックゲインの値を確認 F={L*inv(S*BF)*S*AF}; // 離散化 h = 0.02; // サンプリング時間 cont = syslin('c',AF,BF,S); disc = dscr(cont,h); [A,B,Sd] = abcd(disc); // 初期値 X=[0.5 1.0 1.5 2.0]'; // シミュレーションループ lines(0); for i = 1:250; // 外乱パラメータ w=1;t=i; // SMCの切換関数・制御入力・状態方程式 sigma = S*X; U = -inv(S*BF)*{(S*AF*X)+Q*sign(sigma)+P*sigma};//等価制御入力 dX =A*X+B*U;//+[0; 0; 1 ; 1 ]*0.1*sin(w*t); //状態方程式 // データ格納 Xh1(:,i) = X; Uh1(:,i) = U; Sh1(:,i) = sigma; X = dX; end // プロット clf() tt =0:h:(i-1)*h; // グラフ描画 // 制御入力(第1象限) subplot(222),plot(tt,Uh1(1,:),tt,Uh1(2,:)),xgrid(2) title('制御入力') xlabel('Time [s]') ylabel('Control Input [N]') // 状態変数(第2象限) subplot(221),plot(tt,Xh1(1,:),tt,Xh1(2,:),tt,Xh1(3,:),tt,Xh1(4,:)),xgrid(2) title('状態変数') xlabel('Time [s]') ylabel('Displacement [m]') // 切換関数(第3象限) subplot(223),plot(tt,Sh1),xgrid(2) title('切換関数') xlabel('Time [s]') ylabel('Swiching Function') // 位相平面(第4象限) subplot(224),plot(Xh1(1,:),Xh1(3,:),Xh1(2,:),Xh1(4,:)),xgrid(2) title('位相平面') xlabel('x1') ylabel('x2')
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1_1.sce
clear clc disp('Exa-1.1'); Mn=1.008665;Mp=1.007276 //Given mass of an electron and a proton in terms of u Md= Mn-Mp; //mass difference printf('Mass difference in terms of U is %f ',Md); Md=Md*931.50; //converting u into Mev/c^2 by multiplying by 931.5 MeV/c^2 printf('which equals %.3f Mev/c^2.',Md);
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2DiferenciasFinitasAltoOrden.sce
clc() clear all function [diferenciaAdelante, diferenciaAtras, diferenciaCentrada]=diferenciasFinitasSegundoOrden(h,x,funcion) xanterior = x - h xanterioranterior = x - 2*h xposterior = x+h xposteriorposterior = x + 2*h fxanterioranterior = horner(funcion,xanterioranterior) fxanterior = horner(funcion,xanterior) fx = horner(funcion,x) fxposterior = horner(funcion,xposterior) fxposteriorposterior = horner(funcion,xposteriorposterior) diferenciaAdelante = (-fxposteriorposterior+4*fxposterior-3*fx)/(2*h) diferenciaAtras = (3*fx-4*fxanterior+fxanterioranterior)/(2*h) diferenciaCentrada = (-fxposteriorposterior+8*fxposterior-8*fxanterior+fxanterioranterior)/(12*h) endfunction //Definir función x = %s; f = -0.1*x^4-0.15*x^3-0.5*x^2-0.25*x+1.2; x0 = 0.5 //Evaluar derivada df = derivat(f); h = 0.25 disp("derivada exacta") derivada = horner(df,x0) disp(derivada) [diffAdelante, diffAtras, diffCentrada] = diferenciasFinitasSegundoOrden(h,x0,f) disp("Diferencia adelante") disp(diffAdelante) disp("error") disp((derivada-diffAdelante)*100/derivada) disp("Diferencia atrás") disp(diffAtras) disp("error") disp((derivada-diffAtras)*100/derivada) disp("Diferencia centrada") disp(diffCentrada) disp("error") disp((derivada-diffCentrada)*100/derivada)
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Ex4_21.sce
// exa 4.21 Pg 126 clc;clear;close; // Given Data // Hole - d=25;//mm w=150;//mm Kt=2.56;// stress concentration factor P=50;// kN sigma_max=100;// N/mm.sq t=Kt*P*1000/(w-d)/sigma_max;// mm printf('Calculating for hole - \n thickness is : %.2f mm',t) // Notch - d=30;//mm w=120;//mm w=150;//mm Kt=2.3;// stress concentration factor P=50;// kN sigma_max=100;// N/mm.sq t=Kt*P*1000/(w-d)/sigma_max;// mm printf('\n Calculating for notch - \n thickness is : %.2f mm',t) disp('Suggestion, Adopt t = 11 mm')
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9_6.sce
clc; // page no 358 // prob no 9.6 m=21; // The correct number of check bits is the smallest number that satisfy the equation 2^n >= m+n+1; for n=1:1:10 // we choose range of 1 to 10 a=m+n+1; b=2^n; if(b>=a) disp(n,'hammming bits are required') break; end end
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EX11_6.sce
//Example11.6 // determine the analog output voltage and feed back current If clc; clear; close; Vref = 12 ; BI = 1001 ; BI = 1101 ; BI = 1010 ; BI = 0011 ; Rf = 25 ; // K ohm R = 0.25*Rf ; // The output voltage of given binary weighted resistor D/A converter is defined as // Vo = -(Rf*Vref/R)*(2^0*b0+2^-1*b1+2^-2*b2+2^-3*b3) ; // Vo = -(Rf*Vref/R)*(b0+2^-1*b1+2^-2*b2+2^-3*b3) ; // for the given value Rf,R and Vref the output voltage // Vo = -60*(b0+2^-1*b1+2^-2*b2+2^-3*b3) ; // for the binary input 1001 analog output is b3 = 1 ; b2 = 0 ; b1 = 0 ; b0 = 1 ; Vo = -60*(b0+2^-1*b1+2^-2*b2+2^-3*b3) ; disp('for the binary input 1001 analog output is = '+string(Vo)+ ' V '); // the feedback current If is given by If = -(Vo/Rf) ; disp('the feedback current If is = '+string(If)+ ' mA '); // for the binary input 1101 analog output is b3 = 1 ; b2 = 1 ; b1 = 0 ; b0 = 1 ; Vo = -60*(b0+2^-1*b1+2^-2*b2+2^-3*b3) ; disp('for the binary input 1101 analog output is = '+string(Vo)+ ' V '); // the feedback current If is given by If = -(Vo/Rf) ; disp('the feedback current If is = '+string(If)+ ' mA '); // for the binary input 1010 analog output is b3 = 1 ; b2 = 0 ; b1 = 1 ; b0 = 0 ; Vo = -60*(b0+2^-1*b1+2^-2*b2+2^-3*b3) ; disp('for the binary input 1010 analog output is = '+string(Vo)+ ' V '); // the feedback current If is given by If = -(Vo/Rf) ; disp('the feedback current If is = '+string(If)+ ' mA '); // for the binary input 0011 analog output is b3 = 0 ; b2 = 0 ; b1 = 1 ; b0 = 1 ; Vo = -60*(b0+2^-1*b1+2^-2*b2+2^-3*b3) ; disp('for the binary input 0011 analog output is = '+string(Vo)+ ' V '); // the feedback current If is given by If = -(Vo/Rf) ; disp('the feedback current If is = '+string(If)+ ' mA ');
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//Clearing console clc clear //Intializing variables h = 50 a = 0.5/12 b = 0.5/12 t = 0.5/12 Ta = 68 A = 4*a*b T =[180.000000;180.000000;180.000000;106.528061;111.987760;106.528061;89.057755;90.986763;89.057755] T3 = [T(5,1);T(8,1);T(9,1);T(6,1)] //convective heat flow rate for element 3 due to different surfaces I1 = (2*h*A)*(((T3(1,1)+T3(2,1)+T3(3,1)+T3(4,1))/4)-Ta) I2 = 2*h*t*b*(((T3(2,1)+T3(3,1))/2)-Ta) I3 = 2*h*t*b*(((T3(3,1)+T3(4,1))/2)-Ta) //The total convective heat flow rate for element 3 H = I1+I2+I3 printf('\nResults\n') printf('\nThe total convective heat flow rate for element 3\nH=%fBtu/hr',H)
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//Example No. 10.5.3 clc; clear; close; format('v',6); HPBW=39;//degree(HPBW) alfa=12.5;//degree(Pitch angle) f=475;//MHz(Frequency) c=3*10^8;//m/s(Speed of light) lambda=c/(f*10^6);//m(Wavelength) C=lambda;//m(Circumference) disp("Part (i)"); //it is in axial mode as 3/4*lambda<C<4/3*lambda S=C*tand(alfa);//meter(Spacing) N=52^2/HPBW^2/(S/lambda)/(C/lambda)^2;//turns disp(round(N),"Number of turns : "); disp("Part (ii)"); N=round(N);//turns Do=15*(C/lambda)^2*N*(S/lambda);//unitless(Directivity) Do_dB=10*log10(Do);//dB(Directivity) disp(Do_dB,"Directivity in decibels : "); disp("Part (iii)"); AR=(2*N+1)/2/N;//axial ratio disp(AR,"Axial ratio : "); disp("Part (iv)"); //3/4*lambda<C<4/3*lambda lambda1=C/(3/4);//meter(Wavelength) lambda2=C/(4/3);//meter(Wavelength) f1=c/lambda1;//Hz(Frequency) f2=c/lambda2;//Hz(Frequency) disp("Frequency range is "+string(f1/10^6)+" MHz to "+string(f2/10^6)+" MHz.") disp("Part (v)"); //At design frequency Rin=140*C/lambda;//Ω(Input impedence) disp(Rin,"At design frequency, Input impedence in Ω is : "); //3/4*lambda<C<4/3*lambda //At high frequency end Rin=140*C/lambda2;//Ω(Input impedence) disp(Rin,"At high frequency end, Input impedence in Ω is : "); //At low frequency end Rin=140*C/lambda1;//Ω(Input impedence) disp(Rin,"At low frequency end, Input impedence in Ω is : ");
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1. Design and develop a contex free grammar CFG for a subset of Latex. 2. Design, implement, and test the common CFG which I will provide to you at a later date using Lex Flex and Yacc Bison . 3. Design, implement, and test a syntax directed translator based on part 2 that automatically generates formatted ASCII text from an input Latex source file. - Design a CFG for the project that allows Latex programs e.g., text to be formatted to be recognized. This will provide you with important language design experience. - Calculate FIRST and FOLLOW for the non terminals listed below T^H_ h^H_ i^H_ s^H_ ^H_ i^H_ s^H_ ^H_ a^H_ ^H_ d^H_ e^H_ s^H_ i^H_ g^H_ n^H_ ^H_ p^H_ r^H_ o^H_ j^H_ e^H_ c^H_ t^H_ !^H_ !^H_ !^H_ ^@^H_ demurjs CSE244 SP94
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//page 53 //Example 2.19 clear; clc; close; disp('P = '); disp('cos(thetha) -sin(thetha)'); disp('sin(thetha) cos(thetha)'); disp('Inverse(P) = '); disp('cos(thetha) sin(thetha)'); disp('-sin(thetha) cos(thetha)'); disp('where, thetha is some real number'); disp('The basis for R^2 (B'') is the set consisting of vectors (cos(thetha) , sin(thetha)) and (-sin(thetha) , cos(thetha))'); disp('This basis may be obtained by rotating the standard basis by angle thetha'); disp('a = [x1 x2]'); disp('[a]B'' = '); disp('|cos(thetha) sin(thetha)| * |x1|'); disp('|-sin(thetha) cos(thetha)| |x2|'); disp('or'); disp('x1'' = x1*cos(thetha) + x2*sin(thetha)'); disp('x2'' = -x1*sin(thetha) + x2*cos(thetha)'); //end
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//Script to model influence of uniform e and b field //on charged particle motion exec('lorentz.sce'); exec('bfield.sce'); m=1.6*(10^(-27)); q=1.6*(10^(-19)); dt=5.0*(10^(-9)); it=1:1:1000; //plotid=evstr(x_dialog('plotid ?','1'));; //text=x_dialog('Title?','current'); plotid=1; text='current'; r=zeros(3,1); v=zeros(3,1); partheight=100*(10^3); parttheta=0; partphi=%pi*5/180; rearth=6378.0*(10^3); r(1,1)=(partheight+rearth)*cos(parttheta)*sin(partphi); r(2,1)=(partheight+rearth)*sin(parttheta)*sin(partphi); r(3,1)=(partheight+rearth)*cos(partphi); //v(1,1)=1.0*(10^6); v(2,1)=1.0*(10^6); //i=()*bz*(4*pi); //i=(zŁ2+r$^) mu0=4.0*%pi*(10^(-7)); b=zeros(3,1); e=zeros(3,1); //bfield in z direction b(3,1)=0.1; //efield in y direction //e(2,1)=0.2; //e(3,1)=10*(10^4); ns=200; //calculate effective current for earths bfield mu0=4.0*%pi*(10^(-7)); //lensol=2556*10^3; //length of effective solenoid //used in computation of final field lensol=1; zt=lensol/2; zb=-zt; //http://hyperphysics.phy-astr.gsu.edu/hbase/magnetic/magearth.html#c1 //magnetic field strongest at earths surface i z direction //north and south magnetic poles bz=0.6*(10^(-4)); //effective radius of solenoid //1/3 radius of earths outer core //http://en.wikipedia.org/wiki/Earth#Composition_and_structure //solenoid field calculation //http://www.netdenizen.com/emagnet/solenoids/thinsolenoid.htm //zsol=5100*10^3; //radius of earth - len solenoid //reffsol=1278*(10^3)/3; zsol=rearth-lensol; reffsol=4000*(10^3)/3; nturns=1; rfactor=((lensol+zsol)/((lensol+zsol)^2 + reffsol^2))-(zsol/(zsol^2+reffsol^2)); itot=2*lensol*bz*2/(mu0*nturns*rfactor); itot=1.5*10^9; iperturn=itot/(2*%pi*reffsol*nturns);// used in the computation of the bfield with //the biot savart law //v(2,1)=evstr(x_dialog('value of velocity ?','1.0*(10^6)')); //x_dialog(['Method';'enter velocity'],'1') //m=evstr(x_dialog('enter a 3x1 matrix ',['[0 ';'0 ';'0 ]'])) //labels=["b(1)";"b(2)";"b(3) "]; //[ok,b(1,1),b(2,1),b(3,1)]=getvalue("define b field values",labels,... // list("vec",1,"vec",1,"vec",1),["0.0";"0.0";"0.1"]); //xset('pixmap',1); //xselect(); //raise graphic window //np=10; //t=0:0.1:np*%pi; realtimeinit(0.03); if driver()=='Pos' then st=1.5; else st=0.5; end ar=zeros(ns,3); nx=42; ny=42; nz=42; deltax=6371*10^3; deltay=deltax; deltaz=deltax; inx=-deltax*nx/2; iny=inx; inz=iny; b=zeros(3,nx,nz); //if running using the white rose grid easa application portal //we set the directory to '' //and extract the data //directory='out/' directory='out/' dxdirectory='dx/' jobname='mkgt16'; outfile=directory+'job'+jobname+'.out'; formfile=directory+'jobform'+jobname+'.out'; dxgenfile=directory+'job'+jobname+'.general'; dxformgenfile=directory+'job'+jobname+'_form.general'; fdform=mopen(formfile,'w'); mfprintf(fdform, '%d %d %d\n',nx, ny, nz); mclose(fdform); fd=mopen(outfile,'w'); deltab=%pi/128; mfprintf(fd,'Earth bfield model\n'); mfprintf(fd,'jobname %s\n',jobname); mfprintf(fd,'size %d %d %d \n',nx,ny,nz); mfprintf(fd,'Height effective solenoid(m) %f\n',zsol); mfprintf(fd,'Radius effective solenoid(m) %f\n',reffsol); mfprintf(fd,'deltab %f\n',deltab); mfprintf(fd,'n turns %d\n',nturns); for i1=1:nx //disp(i1); //for i2=1:ny for i3=1:nz y=inx+i1*deltax; //y=iny+i2*deltay; z=inz+i3*deltaz; x=0; r(1,1)=x; r(2,1)=y; r(3,1)=z; //bf=bfield(reffsol,zt,zb,nturns,itot,r,deltab); //bfield(r,ztp,zbot,n,i,rfp,dtheta) rs=reffsol; ztp=zt; zbot=zb; n=nturns; i=itot; rfp=r; dtheta=deltab; //n number of turns //i per turn bt=zeros(3,1); mu0=4.0*%pi*(10^(-7)); dz=(ztp-zbot)/n; ce=zeros(3,1); //calculate field contribution for each turn z=zbot; //z=0; //dz=0; //dr=2*%pi/dtheta; dr=rs*dtheta; //for ic=0:n for theta=0:dtheta:(2*%pi)-dtheta //current element location xi=rs*cos(theta); yi=rs*sin(theta); rcp(1,1)=xi; rcp(2,1)=yi; rcp(3,1)=z; rp(1,1)=rfp(1,1)-rcp(1,1); rp(2,1)=rfp(2,1)-rcp(2,1); rp(3,1)=rfp(3,1)-rcp(3,1); rcpd(1,1)=rs*cos(theta+dtheta); rcpd(2,1)=rs*sin(theta+dtheta); rcpd(3,1)=z; //current element vector //using tangent vector defn. from //http://mathworld.wolfram.com/TangentVector.html //and arc length ds=rdtheta //ce(1,1)=-sin(theta); //ce(2,1)=cos(theta); ce(1,1)=rcpd(1,1)-rcp(1,1); ce(2,1)=rcpd(2,1)-rcp(2,1); ce(3,1)=rcpd(3,1)-rcp(3,1); //evaluate cross product of current element and //field vector cp(1,1)=ce(2,1)*rp(3,1)-ce(3,1)*rp(2,1); cp(2,1)=ce(3,1)*rp(1,1)-ce(1,1)*rp(3,1); cp(3,1)=ce(1,1)*rp(2,1)-ce(2,1)*rp(1,1); rsq=rp(1,1)*rp(1,1)+rp(2,1)*rp(2,1)+rp(3,1)*rp(3,1); bt(1,1)=bt(1,1)+mu0*i*dr*(cp(1,1))/(4*%pi*rsq); bt(2,1)=bt(2,1)+mu0*i*dr*(cp(2,1))/(4*%pi*rsq); bt(3,1)=bt(3,1)+mu0*i*dr*(cp(3,1))/(4*%pi*rsq); end z=z+dz; //end bf=bt; mfprintf(fd, '%f %f %f %f %f %f\n',r(1,1)/rearth,r(2,1)/rearth,r(3,1)/rearth,bf(1,1),bf(2,1),bf(3,1)); b(:,i1,i3)=bf; end // end end mclose(fd); bmag=b(1,:,:).*b(1,:,:)+b(2,:,:).*b(2,:,:)+b(3,:,:).*b(3,:,:); bmag=sqrt(bmag); iax=1:nx; iay=1:ny; bnmag=zeros(nx,ny); bnmag(:,:)=bmag(1,:,:); bxm=zeros(nx,ny); bym=zeros(nx,ny); bxm(:,:)=b(1,:,:); bym(:,:)=b(3,:,:); contour2d(iax,iay,bnmag); champ(iax,iay,bxm,bym); //generate dx general file for this data set //file=out/job.out //grid 51 x 51 //format = ascii //interleaving = field //majority = row //header = lines 1 //series = 24 , 1, 1, separator=lines 1 //field = field0, field1 //structure = 2-vector, scalar //type = float, float //dependency = positions, positions //positions = regular,regular, 0, 1,0,1 //end dxgenfile=dxdirectory+'job'+jobname+'.general'; fdform=mopen(dxgenfile,'w'); mfprintf(fdform, 'file=%s\n', 'out/job'+jobname+'.out'); mfprintf(fdform,'grid= %d x %d x %d\n',nx,ny,nz); mfprintf(fdform,'format = ascii \n interleaving = field \n header = lines 7 \n'); //mfprintf(fdform, 'series = 1 , 1, 1, separator=lines 1\n'); mfprintf(fdform, 'field = locations,bfield \n structure = 3-vector, 3-vector \n type = float, float \n dependency = positions, positions \n end \n '); mclose(fdform); //file=out/jobform.out //grid = 1 //format = ascii //interleaving = record //majority = row //field = nsteps, nx, ny //structure = scalar, scalar, scalar //type = int, int, int //dependency = positions, positions, positions //positions = regular, 0, 1 //end dxformgenfile=dxdirectory+'job'+jobname+'_form.general'; fdform=mopen(dxformgenfile,'w'); mfprintf(fdform, 'file=%s\n', 'out/jobform'+jobname+'.out'); mfprintf(fdform,'grid=1\n'); mfprintf(fdform,'format = ascii \n interleaving = record \n majority = row \n'); mfprintf(fdform, 'field = nr ,ntheta, nphi \n structure = scalar, scalar, scalar \n type = int, int, int \n dependency = positions, positions,positions \n positions = regular, 0, 1 \n end \n '); mclose(fdform); //exit;
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//Chapter-1, Example 1.21, Page 1.49 //============================================================================= clc clear //INPUT DATA R=0.05;//Total resistance of the motor in ohm IL1=120;//Load current in A V=220;//Terminal voltage in V N=1200;//Speed in rpm IL2=60;//Half load current in A //CALCULATIONS //Tnew=0.25*Told //Hence percentage change in torque is 75% since it is (Told-Tnew)/Told*100 Ebnew=(V-(IL1*R));//New back emf in V Ebold=(V-(IL2*R));//Old back emf in V Nnew=(N*Ebnew*IL1)/(Ebold*IL2);//New speed in rpm Pspeed=(Nnew/N)*100;//Percentage change in speed in % //Ianew=(Iaold/sqrt(2)) I=sqrt(2)*100;//Percentage in current N1new=(sqrt(2)*Ebnew*N)/Ebold;//New speed in rpm P1speed=(N1new/N)*100;//Percentage change in speed in % //OUTPUT mprintf('i)Percentage in speed is %3.2f and Percentage in torque is 75\nii)New speed is %3.0f rpm and new current is (1/sqrt(2)) times old current',Pspeed,N1new) //=================================END OF PROGRAM==============================
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// Example no.5.3 // To find quantum efficiency at different wavelength and same responsivity // Page no.199 clc; clear; // Given data lambda1=0.7; // The radiation wavelength in micrometer R=0.4; // The responsivity in A/W lambda2=0.5; // The reduced wavelength in micrometer neta1=(R*1.24)/lambda1; // The quantum efficiency for 0.7micrometer wavelength neta2=neta1*(lambda2/lambda1); // The quantum efficiency for reduced wavelength 0.5micrometer // Display result on command window printf('\n The quantum efficiency for 0.7 micrometer wavelength = %0.4f',neta1) printf('\n The quantum efficiency for reduced wavelength of 0.5 micrometer = %0.3f',neta2)
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<?php include ('knights.php'); $array=newBoard(); $array[1][1]=1; printBoard($array); ?>
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clc Na=3*10^16 disp("Na = "+string(Na)+" /cm^3") //initializing value of acceptor ion concentration. Vms=-1.12 disp("Vms = "+string(Vms)+"V") //initializing value of metal semiconductor work function difference. Er=11.9 disp("Er = "+string(Er)) //initializing value of relative dielectric permittivity constant . Eo=8.854*10^-14 disp("Eo = "+string(Eo)+" F/cm") //initializing value of permittivity of free space. ni=1.5*10^10 disp("ni = "+string(ni)+"cm^-3") //initializing value of intrinsic concentration of electrons. e=1.6*10^-19 disp("e = "+string(e)+" columns") //initializing value of charge of electrons. tox=300*10^-8 disp("tox = "+string(tox)+" cm") //initializing value of thickness of p-type substrate. Vfb=-1.12 disp("Vfb = "+string(Vfb)+" V") //initializing value of flat band voltage. Qss=10^11 disp("Qss = "+string(Qss)+" electronic charge columns/cm^2") //initializing value of charge density on semiconductor surface. Vt=0.0259 disp("Vt = "+string(Vt)+" eV") //initializing value of thermal voltage. er=3.9 disp("er = "+string(er)) //initializing value of relative dielectric permittivity constant Eox=Eo*Er disp("total permittivity,Eox=Eo*Er="+string(Eox)+" F/cm")//calculation Vfp=Vt*(log(Na/(ni))) disp("Potential,Vfp=Vt*(log(Na/(ni))))="+string(Vfp)+" V")//calculation Wd=sqrt((4*Eox*Vfp)/(e*Na)) disp("Maximum depletion width,Wd=sqrt((4*E*Vs)/(e*Nd)))="+string(Wd)+" cm")//calculation QDmax=(e*Na*Wd) disp("Over all maximum depletion width,QDmax=(e*Na*Wd))="+string(QDmax)+" columns/cm^2")//calculation VT=(((QDmax-1.6*10^-8)*tox)/(er*Eo))+(2*Vfp+Vfb) disp("Thresold Voltage,VT=(((QDmax-1.6*10^-8)*tox)/(er*Eo))+(2*Vfp+Vfb)="+string(VT)+" V")//calculation
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//Chapter 5 //Example 5_3 //Page 92 clear;clc; rs=100; exceed=0.15; fr=0.3; x=rs/(fr-exceed); printf("Number of units at which charges due to both tariffs become equal = %.2f units \n\n", x); printf("Tariff (a) is economical if consumption is more than %.2f units \n\n", x);
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PL/SQL Developer Test script 3.0 53 -- Created on 19.02.2018 by V.ZHURAVOV declare -- Local variables here procedure recreate_2ndfl( p_year int, p_ref_id f2ndfl_arh_spravki.id%type ) is l_ref_row f2ndfl_arh_spravki%rowtype; begin -- l_ref_row := f2ndfl_arh_spravki_api.get_reference_row(p_ref_id); -- update f2ndfl_arh_spravki s set s.r_xmlid = null where s.id = p_ref_id; -- f2ndfl_arh_spravki_api.delete_reference( p_ref_id => p_ref_id ); -- f2ndfl_arh_spravki_api.create_reference( p_code_na => 1, p_year => p_year, p_contragent_id => l_ref_row.ui_person, p_ref_num => l_ref_row.nom_spr, p_report_date => to_date(20171231, 'yyyymmdd') ); -- l_ref_row.id := f2ndfl_arh_spravki_api.get_reference_last_id( p_code_na => 1, p_year => p_year, p_ref_num => l_ref_row.nom_spr, p_load_exists => 'N' ); -- update f2ndfl_arh_spravki s set s.r_xmlid = l_ref_row.r_xmlid where s.id = p_ref_id; -- end recreate_2ndfl; begin -- Test statements here /* 2580301 2641748 2641779 */ recreate_2ndfl(2017, 2580301); exception when others then dbms_output.put_line(utl_error_api.get_exception_full); raise; end; 0 0
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clc clear //DATA GIVEN n=6; //no. of cylinders Pdisp=700; //piston disp per cylinder in cm^3 P=78; //power developed in kW N=3200; //engine speed in R.P.M. Mf=27; //mass of fuel used in kg/hr C=44000; //calorific value of fuel used in kJ/kg afr=12; //air fuel ratio Pa=0.9; //intake air pressure in bar Ta=32+273; //intake air tempertaure in K R=0.287; //gas constant for air in kJ/kgK k=0.5; //for 4-stroke cylinder Ma=afr*Mf; //mass of air //by eq. pa*Va=Ma*R*Ta Va=Ma*R*Ta/Pa/100; //volume of intake air in m^3/hr Vswept=(Pdisp/10^6)*n*(N/2)*60; //volume swept in m^3/hr ETAvol=Va/Vswept; //volumetric efficiency //Brake thermal efficiency , ETAbt=brake work/heat supplied by the fuel ETAbt=P/(Mf*C/3600); //Brake Power, BP = (2*pi)N*Tb/(60*1000) kW Tb=P*60/(2*%pi*N); //brake torque in kNm printf(' (i) The Volumetric efficiency is: %5.3f or %5.1f percent. \n',ETAvol,(ETAvol*100)); printf(' (ii) The Brake thermal efficiency is: %5.4f or %5.2f percent. \n',ETAbt,(ETAbt*100)); printf(' (iii) The Brake Torque is: %5.4f kNm. \n',Tb);
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n=6;m=5; A=[1:n]' B=ones(1,m) L=A*B // with only one command L=([1:n]')*ones(1,m)
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// Example 7.5.d: percentage elonagtion clc; clear; close; format('v',4) yl=34;//yeild load in kN ul=61;//ultimate load in kN fl=78;//final length in mm glf=60;//gauge length of fratture in mm fd=7;//final diamtere in mm d=12;//specimen diamtere in mm sl=62.5;//specimen length in mm A=(%pi*(d)^2)/4;// in mm square A1=(%pi*(fd)^2)/4;// in mm square pr=(fl-glf)/glf;// disp(pr*100,"percentage elonagtion is")
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function [stk,txt,top]=sci_cool() // Copyright INRIA txt=[] if rhs<1 then r=gettempvar(1) txt=r+'=(0:31)''/31' stk=list('['+r+',1-'+r+',ones('+r+')]','0','32','3','1') else r=gettempvar(1) if isname(stk(top)(1)) then n=stk(top)(1) txt=[] else n=tempvar(2) txt=n+'='+stk(top)(1)+';' end txt=[txt; r+'=(0:'+n+')''/'+n+';'] stk=list('['+r+',1-'+r+',ones('+r+')]','0',n,'3','1') end
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funcprot(0); cd("C:\projects\flight\math\SciLab"); exec("%s_m_ZQuat.sci"); exec("%ZQuat_conj.sci"); exec("%ZQuat_m_s.sci"); exec("%ZQuat_m_ZQuat.sci"); exec("%ZQuat_norm.sci"); exec("%ZQuat_p.sci"); exec("%ZQuat_r_S.sci"); exec("%ZQuat_size.sci"); exec("%ZQuat_t.sci"); exec("plotter.sci"); exec("ZQ_defQuat.sci"); exec("ZQ_euler2quat.sci"); exec("ZQ_quat2euler.sci"); exec("ZQ_sandwich.sci"); exec("ZQ_quat2matrix.sci"); exec("kinematics.sci"); function [A_q_w, V_w, P_w] = main() // Meter-Kilogram-Second-Radian measure // Right-Hand rules // NWU - North-West-Up // x axis = forward // y axis = left // z axis = up // roll = x axis // pitch = y axis // yaw = z axis // vectors are all column vectors (1 columnm, n rows) // ************* Sample Period and Count ******************* dt = 0.01; samples = 500; // ************* Initial Conditions ******************* // attitude, quaternion, world frame g = 9.81; r = 5; v = 5; initial_altitude = 1; a = v^2/r; theta = atan(v^2/(r*g)); w = g*tan(theta)/v; distance = 2*%pi*r; time = distance/v; samples = time/dt; disp("samples: ") disp(samples) disp("flight time: ") disp(samples*dt) A_q_w = ZQ_euler2quat([theta;0;0]); A_q_w = A_q_w/norm(A_q_w); // velocity V_w = [v;0;0]; // position, world frame P_w = [0;0;initial_altitude]; // ************* Sample Data ******************* // angular velocity, euler, body frame (gyro sample) aV_sample = [0;-w*sin(theta);-w*cos(theta)]; // linear acceleration, body frame (accelerometer sample) lift = sqrt(a^2 + g^2); A_sample = [0;0; lift]; altimeter = initial_altitude; // ************* Logging Setup ******************* A_log = []; A_q_log = []; V_log = []; P_log = []; disp("start position: ") disp(P_w); for i = 1:samples // noise aV_sample_noisy = aV_sample + norm(aV_sample)*((rand()-0.5)/100)*0; A_sample_noisy = A_sample + norm(A_sample)*((rand()-0.5)/100)*0; altimeter_noisy = altimeter * (1+(rand()-0.5)/2000000); A_q_w_0 = A_q_w; V_w_0 = V_w; P_w_0 = P_w; [A_q_w, V_w, P_w] = processSample(dt, A_q_w_0, V_w_0, P_w_0, A_sample_noisy, aV_sample_noisy, altimeter_noisy); // ************* Logging ******************* V_log = [V_log V_w]; P_log = [P_log P_w]; [a,b,c] = ZQ_quat2euler(A_q_w); A_log = [A_log [a;b;c]]; A_q_log = [A_q_log [A_q_w.r; A_q_w.i(1); A_q_w.i(2); A_q_w.i(3);]]; R = ZQ_quat2matrix(A_q_w); VertexData(:,:,i) = GeoVerMakeBlock(P_w',R); [X,Y,Z] = GeoPatMakeBlock(VertexData(:,:,i)); PatchData_X(:,:,i) = X; PatchData_Y(:,:,i) = Y; PatchData_Z(:,:,i) = Z; end disp("end position: ") disp(P_w); // ************* Plots ******************* clf() fig = gcf(); fig.figure_size = [1000,1000]; subplot(221) title("Attitude, Euler") plot([A_log(1,:)' A_log(2,:)' A_log(3,:)']) legend(["X";"Y";"Z"], "in_upper_left") subplot(222) title("Attitude, Quaternion") plot([A_q_log(1,:)' A_q_log(2,:)' A_q_log(3,:)' A_q_log(4,:)']) legend(["R";"X";"Y";"Z"], "in_upper_left") subplot(223) title("Velocity") plot([V_log(1,:)' V_log(2,:)' V_log(3,:)']) legend(["X";"Y";"Z"], "in_upper_left") subplot(224) title("Position") plot([P_log(1,:)' P_log(2,:)' P_log(3,:)']) legend(["X";"Y";"Z"], "in_upper_left") // Draw initial figure figure(1); fig = gcf(); fig.figure_size = [1000,1000]; plot3d(PatchData_X(:,:,1),PatchData_Y(:,:,1),PatchData_Z(:,:,1)); h_fac3d = gce(); h_fac3d.color_mode = 4; h_fac3d.foreground = 1; h_fac3d.hiddencolor = 4; // Axes settings xlabel("x",'fontsize',2); ylabel("y",'fontsize',2); zlabel("z",'fontsize',2); h_axes = gca(); h_axes.font_size = 2; h_axes.isoview = "on"; h_axes.box = "off"; h_axes.rotation_angles = [67,-128]; xgrid; // Find plot extents maxX=-10000; minX=10000; maxY=-10000; minY=10000; maxZ=-10000; minZ=10000; for i=1:samples maxX = max(maxX, P_log(1,i)); maxY = max(maxY, P_log(2,i)); maxZ = max(maxZ, P_log(3,i)); minX = min(minX, P_log(1,i)); minY = min(minY, P_log(2,i)); minZ = min(minZ, P_log(3,i)); end h_axes.data_bounds = [minX-1, minY-1, minZ-1; maxX+1, maxY+1, maxZ+1]; sleep(1000); // Animation Loop for i=1:samples drawlater(); h_fac3d.data.x = PatchData_X(:,:,i); h_fac3d.data.y = PatchData_Y(:,:,i); h_fac3d.data.z = PatchData_Z(:,:,i); drawnow(); // sleep(5); end endfunction main();
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function M = MatSymetrique(n) M = rand(n, n); t1 = triu(M); t2 = t1' - diag(diag(M)); M = t1 + t2; M = floor(100 * M); endfunction
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//Example 4.19 clc; syms s; F=1/((s+1)*(s+2)); f=ilaplace(F); disp(f);
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clc // This GUI file is generated by guibuilder version 3.0 ////////// f=figure('figure_position',[400,50],'figure_size',[646,574],'auto_resize','on','background',[29],'figure_name','Graphic window number %d'); ////////// delmenu(f.figure_id,gettext('File')) delmenu(f.figure_id,gettext('?')) delmenu(f.figure_id,gettext('Tools')) toolbar(f.figure_id,'off') handles.dummy = 0; handles.og1= newaxes();handles.og1.margins = [ 0 0 0 0];handles.og1.axes_bounds = [0.453125,0.13125,0.5,0.21875]; og1a = gca(); handles.adv1= newaxes();handles.adv1.margins = [ 0 0 0 0];handles.adv1.axes_bounds = [0.465625,0.4375,0.490625,0.1833333]; adv1a = gca(); handles.delay1= newaxes();handles.delay1.margins = [ 0 0 0 0];handles.delay1.axes_bounds = [0.471875,0.7208333,0.4859375,0.1833333]; delay1a = gca(); handles.signal=uicontrol(f,'unit','normalized','BackgroundColor',[-1,-1,-1],'Enable','on','FontAngle','normal','FontName','Noto Sans','FontSize',[12],'FontUnits','points','FontWeight','normal','ForegroundColor',[-1,-1,-1],'HorizontalAlignment','left','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.0828125,0.9020833,0.28125,0.05625],'Relief','default','SliderStep',[0.01,0.1],'String','Enter your signal','Style','edit','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','signal','Callback','') handles.value=uicontrol(f,'unit','normalized','BackgroundColor',[-1,-1,-1],'Enable','on','FontAngle','normal','FontName','Noto Sans','FontSize',[12],'FontUnits','points','FontWeight','normal','ForegroundColor',[-1,-1,-1],'HorizontalAlignment','left','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.45625,0.9041667,0.2078125,0.0541667],'Relief','default','SliderStep',[0.01,0.1],'String','Enter your value','Style','edit','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','value','Callback','') handles.og1plot=uicontrol(f,'unit','normalized','BackgroundColor',[-1,-1,-1],'Enable','on','FontAngle','normal','FontName','Noto Sans','FontSize',[12],'FontUnits','points','FontWeight','normal','ForegroundColor',[-1,-1,-1],'HorizontalAlignment','center','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.08,0.68125,0.253125,0.1520833],'Relief','default','SliderStep',[0.01,0.1],'String','ORIGINAL','Style','pushbutton','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','og1plot','Callback','og1plot_callback(handles)') handles.plotadv1=uicontrol(f,'unit','normalized','BackgroundColor',[-1,-1,-1],'Enable','on','FontAngle','normal','FontName','Noto Sans','FontSize',[12],'FontUnits','points','FontWeight','normal','ForegroundColor',[-1,-1,-1],'HorizontalAlignment','center','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.08,0.3770833,0.253125,0.1645833],'Relief','default','SliderStep',[0.01,0.1],'String','ADVANCE','Style','pushbutton','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','plotadv1','Callback','plotadv1_callback(handles)') handles.plotdelay1=uicontrol(f,'unit','normalized','BackgroundColor',[-1,-1,-1],'Enable','on','FontAngle','normal','FontName','Noto Sans','FontSize',[12],'FontUnits','points','FontWeight','normal','ForegroundColor',[-1,-1,-1],'HorizontalAlignment','center','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.08,0.1083333,0.253125,0.125],'Relief','default','SliderStep',[0.01,0.1],'String','DELAY','Style','pushbutton','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','plotdelay1','Callback','plotdelay1_callback(handles)') handles.clear=uicontrol(f,'unit','normalized','BackgroundColor',[-1,-1,-1],'Enable','on','FontAngle','normal','FontName','Noto Sans','FontSize',[12],'FontUnits','points','FontWeight','normal','ForegroundColor',[-1,-1,-1],'HorizontalAlignment','center','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.08,0.02,0.253125,0.06],'Relief','default','SliderStep',[0.01,0.1],'String','CLEAR','Style','pushbutton','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','clear','Callback','clear_callback(handles)') ////////// // Callbacks are defined as below. Please do not delete the comments as it will be used in coming version ////////// function og1plot_callback(handles) //Write your callback for og1plot here x = get(handles.signal, "String"); x = strsplit(x, " "); x = strtod(x); axes = 0:4; sca(og1a); plot2d3(axes,x); replot([-6,0,6,10]); endfunction function plotadv1_callback(handles) //Write your callback for plotadv1 here x = get(handles.signal, "String"); x = strsplit(x, " "); x = strtod(x); value = get(handles.value, "String"); value = strtod(value); axes = 0:4; shift = axes - value; sca(adv1a); plot2d3(shift,x); replot([-6,0,6,10]); endfunction function plotdelay1_callback(handles) //Write your callback for plotdelay1 here //Write your callback for plotadv1 here x = get(handles.signal, "String"); x = strsplit(x, " "); x = strtod(x); value = get(handles.value, "String"); value = strtod(value); axes = 0:4; shift = axes + value; sca(delay1a); plot2d3(shift,x); replot([-6,0,6,10]); endfunction function clear_callback(handles) //Write your callback for clear here delete(og1a.children); delete(adv1a.children); delete(delay1a.children); endfunction
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x= [2: 1: 10] y = x-1 //z = sqrt(4 - x.^2 - y.^2) //z = log(x) plot3d(x,y,log(x-y))
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ex_1_25.sce
//Example 1.25 // diameter of bright ring clc; clear; //given data : w=6D-7;// wavelength used in m R1=3;//radius of curvature of convex lens in m R2=4;//radius of curvature of concave lens in m n=13;// order of ring r=sqrt((2*n-1)*w/(2*(1/R1-1/R2)));// radius of ring disp(2*r,"diameter of bright ring in m")
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6_07.sce
pathname=get_absolute_file_path('6_07.sce') filename=pathname+filesep()+'6_07data.sci' exec(filename) a=atand(1/L_D);disp(a,"a=","tan(a)=1/(L/D)","minimum glide angle a:") R=H*L_D;disp(R,"R=","R=H*L/D","maximum range along ground :") printf("\Answer:\n") printf("\minimum glide angle: %f \n",a) printf("\n\maximum range covered along ground: %f m\n\n",R)
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Zo=50 C=100*10^(-12) a=1.15*10^(-3) //data print printf("\nZo=50 ohm C=100pF/m a=0.01 dB/m\n") //formula and result L=C*Zo^2 R=a*sqrt(L/C) G=R*C/L vp=1/sqrt(L*C) printf("\nresult:-") printf("\n(a)R=a*sqrt(L/C)=%.3f ohm/m",a*sqrt(L/C)) printf("\n(b)L=C*Zo^2=%.3e H/m",C*Zo^2) printf("\n(c)G=R*C/L=%.3e S/m",R*C/L) printf("\n(d)vp=1/sqrt(L*C)=%.1e m/s",1/sqrt(L*C))
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ex6_1.sce
s=%s; p=s^4+8*s^3+18*s^2+16*s+5 r=coeff(p) D1=r(4) d2=[r(4) r(5);r(2) r(3)] D2=det(d2); d3=[r(4) r(5) 0;r(2) r(3) r(4);0 r(1) r(2)] D3=det(d3); d4=[r(4) r(5) 0 0;r(2) r(3) r(4) r(5);0 r(1) r(2) r(3);0 0 0 r(1)] D4=det(d4); disp(D1,"D1=") disp(D2,"D2=") disp(D3,"D3=") disp(D4,"D4=") printf("Since all the determinants are positive the system is stable")
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generateInRangeOM1.sci
function ri=generateInRangeOM1(m,nbrows,nbcols) ri = floor(rand(nbrows,nbcols)*m) endfunction
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clc h0=.761; //m h=.55; //m g=9.79; //m/s^2 rho=13640; //kg/m^3 P=rho*g*(h0+h); //N/m^2 disp("Gas pressure=") disp(P/10^5) disp("bar")
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clear // //case a vl=11000 il=50 pf=0.85 //powerfactor p=vl*il*pf printf("\n Power supplied to the motor is= %0.5f kW",p) //case b vt=6350.85 //at angle 0 zs=25.02 //at angle 0 //subcase 1 powerfactor at 0.85 lag //e=vt-ia*zs //e=6350.85-50(at angle -31.79)*25.02(at angle 87.71) //substituting and solving as in x+iy form we get 5744.08 at angle -10.39 as the value of e printf("\n emf induced=5744.08 at angle -10.39") //subcase 2 //for a 0.85 lead same process as above is followed except angles are considered positive due to lead printf("\n emf induced=7051.44 at angle -8.88")
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for i=1:50 // 50 trajectoires Q = queue(60, 1/2, 1/10); // lambda est 5 fois plus grand que mu plot2d2(Q(:,1), max(Q(:,2) - 1, 0), style=2) // trace la courbe end
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Example2_1.sce
clear //Caption:Program to Caculate force exerted on Q2 by Q1 //Example2.1 //page 29 clc; r2 = [2,0,5]; r1 = [1,2,3]; R12 = norm(r2-r1); aR12 = (r2-r1)/R12; disp(R12,'R12=') disp(aR12,'aR12=') Q1 = 3e-04; //charge 1 in Coulombs Q2 = -1e-04; //charge 2 in Coulombs Eps = 8.854e-12; //free space permittivity F2 = ((Q1*Q2)/(4*%pi*Eps*R12^2))*aR12; F1 = -F2; disp(F2,'Force exerted on Q2 by Q1 in N/m F2 =') disp(F1,'Force exerted on Q1 by Q2 in N/m F1 =') //Result //R12= // 3. //aR12= // 0.3333333 - 0.6666667 0.6666667 //Force exerted on Q2 by Q1 in N/m F2 = // - 9.9863805 19.972761 - 19.972761 //Force exerted on Q1 by Q2 in N/m F1 = // 9.9863805 - 19.972761 19.972761
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patay V;PST patay V;PROG;PRS patay V;PROG;FUT patay V;NFIN patay V;PRF+PROG;PST patay V;PRF;PRS patay V;PROG;PST patay V;PRF;FUT patay V;PRF;PST patay V;PRF+PROG;PRS patay V;PRF+PROG;FUT patay V;FUT patay V;PRS dalagan V;PROG;PST dalagan V;PROG;FUT dalagan V;PRF;FUT dalagan V;PRF+PROG;PST dalagan V;PRF+PROG;PRS dalagan V;PRF+PROG;FUT dalagan V;PST dalagan V;PRS dalagan V;PROG;PRS dalagan V;PRF;PST dalagan V;FUT dalagan V;PRF;PRS dalagan V;NFIN tindog V;PRF+PROG;FUT tindog V;PRF;PST tindog V;PROG;PRS tindog V;NFIN tindog V;FUT tindog V;PRS tindog V;PROG;PST tindog V;PRF;FUT tindog V;PRF+PROG;PST tindog V;PROG;FUT tindog V;PST tindog V;PRF+PROG;PRS tindog V;PRF;PRS gusto/gustuhan V;PST gusto/gustuhan V;PRS gusto/gustuhan V;NFIN tudlo V;FUT tudlo V;PRS tudlo V;PROG;PRS tudlo V;NFIN tudlo V;PRF;PST tudlo V;PRF;PRS tudlo V;PST tudlo V;PRF;FUT tudlo V;PRF+PROG;PST tudlo V;PRF+PROG;FUT tudlo V;PRF+PROG;PRS tudlo V;PROG;PST tudlo V;PROG;FUT himo V;PRF+PROG;PST himo V;PRF;FUT himo V;NFIN himo V;PST himo V;PRF;PRS himo V;PRF+PROG;PRS himo V;PROG;PRS himo V;PRF+PROG;FUT himo V;PROG;PST himo V;PRS himo V;PROG;FUT himo V;FUT himo V;PRF;PST hunahuna V;PST hunahuna V;PRF+PROG;FUT hunahuna V;FUT hunahuna V;PROG;PRS hunahuna V;PROG;PST hunahuna V;PRF;PST hunahuna V;PRF+PROG;PRS hunahuna V;PRF+PROG;PST hunahuna V;PRF;PRS hunahuna V;PROG;FUT hunahuna V;PRF;FUT hunahuna V;PRS hunahuna V;NFIN higugma/higugmaon V;PST higugma/higugmaon V;FUT higugma/higugmaon V;NFIN higugma/higugmaon V;PROG;PRS higugma/higugmaon V;PRF;PST higugma/higugmaon V;PRS higugma/higugmaon V;PRF;FUT higugma/higugmaon V;PROG;PST higugma/higugmaon V;PRF;PRS higugma/higugmaon V;PRF+PROG;PST higugma/higugmaon V;PRF+PROG;FUT higugma/higugmaon V;PRF+PROG;PRS higugma/higugmaon V;PROG;FUT sira V;FUT sira V;PROG;FUT sira V;PRF+PROG;FUT sira V;PROG;PRS sira V;PRF+PROG;PST sira V;PRF;PST sira V;PRS sira V;PROG;PST sira V;PRF;FUT sira V;PRF;PRS sira V;PRF+PROG;PRS sira V;NFIN sira V;PST sugod V;PRF+PROG;PST sugod V;PROG;FUT sugod V;PRF+PROG;PRS sugod V;PRF+PROG;FUT sugod V;PRF;PST sugod V;PRF;PRS sugod V;PROG;PST sugod V;FUT sugod V;NFIN sugod V;PROG;PRS sugod V;PRS sugod V;PRF;FUT sugod V;PST singgit V;PROG;PRS singgit V;PRF;FUT singgit V;PRF+PROG;FUT singgit V;FUT singgit V;PRS singgit V;PROG;FUT singgit V;NFIN singgit V;PRF;PST singgit V;PST singgit V;PRF;PRS singgit V;PRF+PROG;PRS singgit V;PROG;PST singgit V;PRF+PROG;PST kita/pangita V;PRF+PROG;PRS kita/pangita V;PRS kita/pangita V;PRF;PRS kita/pangita V;PROG;FUT kita/pangita V;NFIN kita/pangita V;PROG;PRS kita/pangita V;PRF+PROG;FUT kita/pangita V;PRF;FUT kita/pangita V;FUT kita/pangita V;PST kita/pangita V;PROG;PST kita/pangita V;PRF;PST kita/pangita V;PRF+PROG;PST istar V;NFIN istar V;PRF;FUT istar V;PRF+PROG;PST istar V;PRF+PROG;FUT istar V;PRF;PST istar V;PRS istar V;PRF+PROG;PRS istar V;PRF;PRS istar V;FUT istar V;PST istar V;PROG;FUT istar V;PROG;PRS istar V;PROG;PST lakat V;PRF+PROG;FUT lakat V;PROG;PRS lakat V;PROG;FUT lakat V;PROG;PST lakat V;PRF+PROG;PST lakat V;FUT lakat V;PRF;FUT lakat V;PRF;PRS lakat V;PRS lakat V;NFIN lakat V;PRF+PROG;PRS lakat V;PRF;PST lakat V;PST obra V;PRF;PRS obra V;NFIN obra V;PRF+PROG;FUT obra V;PROG;PRS obra V;PRS obra V;PRF+PROG;PRS obra V;FUT obra V;PRF;PST obra V;PST obra V;PRF;FUT obra V;PROG;FUT obra V;PROG;PST obra V;PRF+PROG;PST halok/halukan V;PROG;PST halok/halukan V;PROG;FUT halok/halukan V;PRF+PROG;PRS halok/halukan V;PRF+PROG;PST halok/halukan V;PROG;PRS halok/halukan V;NFIN halok/halukan V;PRF;PST halok/halukan V;FUT halok/halukan V;PRF;PRS halok/halukan V;PRS halok/halukan V;PRF+PROG;FUT halok/halukan V;PST halok/halukan V;PRF;FUT desisyon V;PRF+PROG;PRS desisyon V;PRF+PROG;PST desisyon V;PST desisyon V;FUT desisyon V;PROG;FUT desisyon V;PRF;FUT desisyon V;PRF;PST desisyon V;PRF+PROG;FUT desisyon V;PRS desisyon V;PRF;PRS desisyon V;PROG;PST desisyon V;NFIN desisyon V;PROG;PRS hampang V;PRF;FUT hampang V;PST hampang V;PROG;PST hampang V;PRF;PRS hampang V;PRF+PROG;FUT hampang V;PRS hampang V;PROG;PRS hampang V;PRF;PST hampang V;NFIN hampang V;PROG;FUT hampang V;PRF+PROG;PRS hampang V;PRF+PROG;PST hampang V;FUT hular V;PST hular V;PROG;PRS hular V;NFIN hular V;PRF;PST hular V;PRF+PROG;PST hular V;PRF+PROG;PRS hular V;PRF+PROG;FUT hular V;PROG;PST hular V;PROG;FUT hular V;PRS hular V;PRF;PRS hular V;PRF;FUT hular V;FUT baton V;PROG;FUT baton V;PRS baton V;PROG;PRS baton V;PRF+PROG;PRS baton V;FUT baton V;PROG;PST baton V;PRF+PROG;FUT baton V;PRF;FUT baton V;PST baton V;PRF+PROG;PST baton V;PRF;PST baton V;NFIN baton V;PRF;PRS
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clear clc //Example 12.7 TEST SECTION SIZE IN SUPERSONIC WIND TUNNEL k=1.4; M=3; //Mach number Ao=10; //area[cm^2] //Cross-sectional area A=Ao*(1/M)*{(1+[(k-1)/2]*M^2)/((k+1)/2)}^((k+1)/(2*(k-1))) //[cm^2] printf("\n The cross-sectional area of the test section, A = %.1f cm^2.\n",A)
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clc a=2500 //doing for the first values only Bf=4 Bp=0.305 q=a/Bf^2 Sep=4 Sef=Sep*(2*Bf/(Bf+Bp))^2 printf('Sef = %f mm',Sef)
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Ex23_4.sce
//Example 23.4 //Also see Example 23.3 delta_theta=%pi/2;//1/4th of a revolution (rad) delta_t=15*10^-3;//Time (s) omega=delta_theta/delta_t;//Angular velocity (rad/s) //Angular velocity in rad/s can be converted to rpm by multiplying by (60/(2*%pi)). Rpm may be found to be 1000 in this example N=200;//Number of loops, See Example 23.3 r=5*10^-2;//Radius of coil (m), See Example 23.3 A=%pi*r^2;//Area of loop (m^2), See Example 23.3 B=1.25;//Magnetic field strength (T), See Example 23.3 emf_0=N*A*B*omega;//Maximum emf (V) printf('Maximum emf, emf_0 = %0.1f V',emf_0) //Answer varies due to round off error //Openstax - College Physics //Download for free at http://cnx.org/content/col11406/latest
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clear; clc; close; Vt=26*(10^(-3)); //thermal voltage=26mV Vi=3*(10^(-3)); Ie=4*(10^(-3));; //emitter current=4mV alpha=0.991; //common base amplification factor Rl=610; //Load Resistance(in ohms) //Part-1 -> Determinig input impedance re = Vt/Ie; disp(re,'Input impedance(ohms) :'); //Part-2 -> Calculating the voltage gain Ii = (Vi/re); Ie = Ii; Ic=alpha*Ie; Vo=Ic*Rl; Av = Vo/Vi; disp(Av,"Voltage gain :"); //Part-3 -> Calculating the output impedance and current gain disp(%inf,"The output impedance(ohms) is :"); Ai = -Ic/Ie; disp(Ai,"Current gain is :");
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clc; clear all; T=300;//temperature in kelvin k=1.38e-23;//boltzman constant h=6.626e-34;//planks constant e = 1.6e-19; // Charge of an electron Eg=1.1; mo =9.1e-31; // mass of electron me=0.31; // Effective mass of electron r = ((2*%pi*k*T*me*mo)/(h^2))^1.5;// Temporary variable s = exp((-Eg*e)/(2*k*T));// Temporary variable ni=2*r*s disp('m^-3',ni,'the intrinsic concentration is:')
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disp("Peo=nc^2/Ne"); Ne1=10^18; nc=1.5*10^10; Peo1=nc^2/Ne1; printf('\n The value of Peo when Ne=10^18 is %f/cm^3',Peo1); Ne2=10^19; Peo2=nc^2/Ne2; printf('\n The value of Peo when Ne=10^19 is %f/cm^3',Peo2); ni=1.5*10^10; a=0.026; //say a=K*T Eg=0.030; //Eg=ΔEg Peo3=(ni^2)*(exp(Eg/a))/Ne1; //considering the effect of bandgap narrowing printf('\n The value of Peo considering the effect of bandgap narrowing is %f/cm^3',Peo3);
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// Scilab Code Ex6.2: : Page-6.19 (2009) clc; clear; e = 1.6e-019; // Energy equivalent of 1 eV, J/eV E_F = 2.0*e; // Fermi level of Po, J m = 9.1e-031; // Mass of an electron, kg // As E_F = 1/2*m*v^2, solving for v v = sqrt(2*E_F/m); // Velocity of electron at Fermi level, m/s printf("\nThe Velocity of electron at Fermi level = %4.2e m/s", v); // Result // The Velocity of electron at Fermi level = 8.39e+05 m/s
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clear // // // //Variable declaration mewr=15 //relative permeability H=250 //magnetic field intensity(amp/m) mew0=4*%pi*10**-7 //Calculation M=H*(mewr-1) //magnetisation(A/m) B=mew0*(H+M) //magnetic flux density(wb/m**2) //Result
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paramopt=[1,1,1,1]; boundsmin=[-0.4,-4]; boundsmax=[ 0.4, 4]; u0=zeros(ncontr,nn-1);
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function [x, f, g, k]= BFGS_Wolfe(t,x0,m,Sim,e) [f g] = Sim(x0) xk = x0, k = 0, m1 = 0.1, m2 = 0.9 Wk = eye(2,2) while (norm(g,%inf) > e) & (k < m) d = -Wk*g xk = x; [fk gk] = Sim(x) x = xk + t*d; [f g] = Sim(x) k = k+1 t = Busca_de_Wolfe(x,d,t,Sim,10,m1,m2,e) sk = x - xk; yk = g - gk Wk = Wk - [(sk*yk'*Wk + Wk*yk*sk')/yk'*sk] + [1 + (yk'*Wk*yk)/yk'*sk]*(sk*sk')/yk'*sk end endfunction
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// Exa 3.9 clc; clear; close; // Given data Rm= 1.0;// in ohm Rse= 4999;// in ohm V=250;// full scale deflection voltage in volt // Formula V= Im*(Rm+Rse) Im= V/(Rm+Rse);// in amp // Part(a) Rs= 1/4999;// in ohm Is= Im*Rm/Rs;//in amp I= Im+Is;// in amp disp(I,"Current range in amp") // Part(b) I=50;// in amp N=I/Im; Rs= Rm/(N-1);// in ohm disp(Rs,"Required shunt resistance in ohm")
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//clear// //Caption:Program to find the unit vector //Example1.1 //page 8 G = [2,-2,-1]; //position of point G in cartesian coordinate system aG = UnitVector(G); disp(aG,'Unit Vector aG =') //Result //Unit Vector aG = // 0.6666667 - 0.6666667 - 0.3333333
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function [stk,txt,top]=sci_sparse() // Copyright INRIA txt=[] V1=gettempvar(1) V1=gettempvar(2) if rhs==6 then rhs=5;top=top-1,end if rhs==1 then stk=list('sparse('+stk(top)(1)+')','0',stk(top)(3),stk(top)(4),'5') elseif rhs==2 then stk=list('sparse([],[],['+stk(top-1)(1)+','+stk(top)(1)+'])','0',stk(top-1)(1),stk(top)(1),'5') top=top-1 elseif rhs==3 then s1=stk(top-2) s2=stk(top-1) s3=stk(top) if s1(4)=='1'&s2(4)=='1' then stk=list('sparse(['+s1(1)+','+s2(1)+'],'+s3(1)+')','0','?','?','5') elseif or(s1(1)==vnms(:,1))&or(s2(1)==vnms(:,1)) then stk=list('sparse(['+s1(1)+'(:),'+s2(1)+'(:)],'+s3(1)+')','0','?','?','5') else txt=[V1+' = '+s1(1)+';'+V1+'='+V1+'(:)'; V2+' = '+s2(1)+';'+V2+'='+V2+'(:)']; stk=list('sparse(['+V1+','+V2+'],'+s3(1)+')','0','?','?','5') end top=top-2 elseif rhs==5 then s1=stk(top-4) s2=stk(top-3) s3=stk(top-2) s4=stk(top-1) s5=stk(top) if s1(4)=='1'&s2(4)=='1' then stk=list('sparse(['+s1(1)+','+s2(1)+'],'+s3(1)+')','0','?','?','5') elseif or(s1(1)==vnms(:,1))&or(s2(1)==vnms(:,1)) then stk=list('sparse(['+s1(1)+'(:),'+s2(1)+'(:)],'+s3(1)+',['+s4(1)+','+s5(1)+'])','0','?','?','5') else txt=[V1+' = '+s1(1)+';'+V1+'='+V1+'(:)'; V2+' = '+s2(1)+';'+V2+'='+V2+'(:)']; stk=list('sparse(['+V1+','+V2+'],'+s3(1)+',['+s4(1)+','+s5(1)+'])','0','?','?','5') end top=top-4 end
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function y=eq(x) y = 2 * x^2 + 3 * x + 4 endfunction
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//DFT and DFS of sinusoids n2=0:1/840:6/21; xt=4*sin(72*%pi*n2')-6*cos(12*%pi*n2'); n=0:1/21:6/21;//F=3/12 hence N=12 xn=4*sin(72*%pi*n')-6*cos(12*%pi*n'); XDFT=abs(dft(xn,-1)); n1=0:6; a=gca(); a.x_location="origin"; plot2d(n2,xt); plot2d3('gnn',n,xn); xset('window',1); b=gca(); b.x_location="origin"; plot2d3('gnn',n1,XDFT);
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clc // // // //Variable declaration lambdaa=4000*10**-10 //Wavelength mul=1.55821 //Refractive index of left landed mur=1.55810 //Refractive index of right landed t=2*10**-3 //thickness //Calculations orot=(180/%pi)*((2*3.14*(t*(mul-mur)))/lambdaa) //Result printf("\n The Amount of optical rotation produced is %3.0f degrees",orot)
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//Chapter-12, Example 12.20, Page 367 //============================================================================= clc clear //INPUT DATA a=10;//conductivity in s/m un=50*10^-4;//electron mobility in m^2/V-s q=1.6*10^-19;//charge in coulombs //CALCULATIONS n=(a/(un*q));//electron concentration in m^-3 mprintf("electron concentration is %g m^-3 ",n) //=================================END OF PROGRAM=======================================================================================================
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//============================================================================== // chapter 6 example 15 clc; clear; //input data n = 12; //number of plates er = 4; //relative permitivty d = 1.0*10^-3; //distance between plates in m A = 120*150*10^-6; //area in m^2 e0 = 8.854*10^-12; // in F/m //calculation c = (n-1)*e0*er*A/d; //capacitance in F //result mprintf('capacitance=%3.4e.F\n',c); //==============================================================================
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// Variable declaration val1 = 0 val2 = 0 Mine1 = [8260,8130,8350,8070,8340] Mine2 = [7950,7890,7900,8140,7920,7840] alpha = 0.01 // level of significance deg = length(Mine1) + length(Mine2) - 2 // Degree of freedom Mean1 = sum(Mine1)/length(Mine1) Mean2 = sum(Mine2)/length(Mine2) // Calculation for i = 1:length(Mine1) val1 = val1 + (Mean1-Mine1(i))^2 end for i = 1:length(Mine2) val2 = val2 + (Mean2-Mine2(i))^2 end var = (val1 + val2)/(length(Mine1)-1 + length(Mine2)-1) std_dev = sqrt(var) t = (Mean1 - Mean2)/(std_dev*(sqrt(1.0/length(Mine1) + 1.0/length(Mine2)))) // Result if(t>3.250) then printf ( "Null hypothesis rejected") printf ( "Average heat producing capacity is not same") else printf ( "Null hypothesis accepted") printf ( "Average heat producing capacity is same") end
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function [X_n]=F_alog_remez(Cprime,X_n) l=0 if X_n(1)<=Cprime & Cprime<X_n(2) if sign(fmoinsp(X_n(2))) == sign(fmoinsp(Cprime)) X_n(2)=Cprime disp('display',10) else [X_n]=F_permut(X_n,Cprime,1) disp('display',20) end l=1 end if l==0 if X_n(n)< Cprime & Cprime <=X_n(n+1) if sign(fmoinsp(X_n(n))) == sign(fmoinsp(Cprime)) X_n(n)=Cprime disp('display',30) else [X_n]=F_permut(X_n,Cprime,-1) disp('display',40) end l=1 end end if l==0 k=3 while (X_n(k)<Cprime) k=k+1 end if sign(fmoinsp(X_n(k)))== -sign(fmoinsp(Cprime)) X_n(k-1)=Cprime disp('display',50) l=1 else X_n(k)=Cprime disp('display',60) l=1 end end endfunction
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Ex4_17.sce
//Example 4_17 clc; clear; close; format('e',9); //given data : Nd=10^17;//atoms/cm^3 ni=1.5*10^10;//atoms/cm^3 n0=Nd;//atoms/cm^3(For Nd>>ni) p0=ni^2/n0;//atoms/cm^3 disp(p0,"Equilibrium hole concentration(cm^-3)")
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Ex4_1.sce
clc// // // //Variable declaration Ev=1; k=1.38*10^-23; //boltzmann constant(J/K) e=1.6*10^-19; //charge(eV) //Calculation r=Ev/(2.303*1000*k/e); n=10^r; //ratio of n1000/n500 //Result printf("\n ratio of vacancies is %0.3f *10^5",n/10^5)
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Ex_9_6.sce
//Example 9.6 // refractive index and 3dB spectral bandwidth clc; clear; close; //given data : lamda=1.5*10^-6;// in m L=300*10^-6;// in m del_lamda=10^-9;// in m n=lamda^2/(2*del_lamda*L); disp(n,"refractive index , n = ") R1=0.3; R2=R1; a=4.8;// in dB Gs=10^(4.8/10); c=3*10^8; B=(c/(%pi*n*L)*asin((1-sqrt(R1*R2)*Gs)/(2*sqrt(sqrt(R1*R2)*Gs))))*10^-9; disp(B," Spectral bandwidth,(GHz) = ")
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clc; funcprot(0);//Example 14.3 //Initializing the variables Za_Zb = 10; f = 0.008; L = 100; d1 = 0.05; g = 9.81; d2 = 0.1; //Calculations function[z] = flowRate(d) D = 1.5 + 4*f*L/d ; // Denominator in case of v1^2 A = %pi*d^2/4; v = sqrt(2*g*Za_Zb/D); z = A*v; endfunction Q1 = flowRate(d1); Q2 = flowRate(d2); Q = Q1+Q2; D = poly(0, 'D'); v = 4*Q/(%pi*D^2); X = 1.5 + 4*f*L/D; f = 10*2*g/(X*v^2) - 1; f = numer(f) ; diameter = roots(f); // Taking roots of numerator denominator will be multiplied by zero i = 1; while (i<=length(diameter)) x = diameter(i); if(imag(x) == 0) then dia = diameter(i); i= i+1; else i = i+1; end end disp(dia*1000,"Diameter of single equivalent pipe(mm) :", Q2 ,"Flow throught pipe 2 (m3/s):", Q1 ,"Flow throught pipe 1 (m3/s):");
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Ch08Ex07.sce
// Scilab code Ex8.7: Pg.332-333 (2008) clc; clear; k = 1.38e-023; // Boltzmann constant, J/m/K T = 2.7; // Temperature to which the blackbody is cooled, K c = 3e+008; // Speed of light, m/s h = 6.63e-034; // Planck's constant, Js rho_photon = 8*%pi*(k*T/(c*h))^3*integrate('x^2/(exp(x)-1)', 'x', 0, 10); printf("\nThe photom density of the universe = %4.2e photons/metre-cube", rho_photon); // Result // The photom density of the universe = 3.96e+008 photons/metre-cube
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2018-02-03T05:31:52
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Example1_7.sce
clear; clc; // Example: 1.7 // Page: 9 // Solution printf("Example: 1.7 - Page: 9\n\n"); //*****Data*****// P = 560*10^3;// [Pa] Vinit = 3;// [cubic m] Vfinal = 5;// [cubic m] Wext = 210*10^3;// [J] //*************// W = P*(Vfinal - Vinit);// [J] // Again the system receives 210 kJ of work from the external agent. W = W - Wext;// [J] printf("Actual Work done by the system is %.1e J\n",W);
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12_7.sce
clc //initialisation of variables x= 0.79 P0= 101 //kPa P= 20 //Mpa V= 0.032 //m^3 //CALCULATIONS p= x*P0 Wrev= P*10^3*V*(log(P/(p*10^-3))+((p*10^-3)/P)-1) //RESULTS printf (' maximum useful work= %.1f kJ',Wrev)
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//Network Theorem 1 //page no-2.40 //example2.38 disp("Applying KCL to node a:"); disp("2*Va-0.5*Vb-0.5*Vc = 5");....//equation 1 disp("Applying KCL to node b:"); disp("-3/2*Va+5/6*Vb+2/3*Vc = -1");...//equation 2 disp("Applying KCL to node c:"); disp("1/2*Va+1/3*Vb-31/30*Vc = -1");...//equation 3 disp("Solving equations 1,2 and 3");...//solving equations in matrix form A=[2 -0.5 -0.5;-3/2 5/6 2/3;0.5 1/3 -31/30 ]; B=[5 -1 0]' X=inv(A)*B; disp(X); disp("Va= 4.303 V"); disp("Vb= 3.87 V"); disp("Vc= 3.33 V");
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ngi pungana V;IRR;PL;3;PST nu thunungam V;SG;2;non{FUT} la ngule V;IRR;SG;1;PST ma ngimi V;IRR;SG;1;PST na tjinangam V;SG;2;non{FUT} i ngu V;IRR;SG;1 mi numi V;IRR;PC;2 e ngerrena V;PL;1;PST ntha nginthanyi V;SG;1;PST na ninnangi V;IRR;PC;2;PST mi mina V;SG;1;PST ma thama V;IRR;SG;2 la thule V;IRR;SG;2;PST mi pumim V;PL;3;non{FUT} mi ngumina V;PC;1;PST rdi kuddi V;IRR;PL;3 mu ngumune V;PC;1;PST mi mim V;SG;3;non{FUT} ntji nantji V;PL;2;PST rdu nguddu V;IRR;PL;1 mu numuy V;IRR;PC;2;PST ma ne V;SG;2;PST ya purne V;PC;3;PST la killa V;IRR;PL;3 mu pumu V;IRR;SG;1+INCL bi dina V;SG;2;PST bu pubune V;PC;3;PST li ngili V;SG;1;PST na ninga V;SG;3;PST bu buy V;IRR;SG;1;PST a ka V;IRR;PC;3 bi ngubi V;IRR;PL;1 ya nurni V;PL;2;PST ntha tjinthanyi V;SG;1+INCL;PST bi nubi V;IRR;PL;2 me ngumena V;PL;1;PST be bena V;IRR;SG;3;PST mu kumuy V;IRR;PC;3;PST nu ngunna V;IRR;PC;1 mu mu V;IRR;SG;1 na nginnanga V;PL;1;PST e ngem V;SG;1;non{FUT} ntji ngantjin V;PL;1;non{FUT} ntji perra V;IRR;PC;3;PST ntji nerra V;IRR;PC;2;PST ni narni V;IRR;PL;2 be bena V;SG;3;PST nu punne V;IRR;PC;3;PST a ngarrane V;PC;1;PST ngu ngunga V;IRR;PC;1 rra pirri V;SG;3;PST buy dana V;SG;2;PST ni thani V;IRR;SG;2 nga tjingam V;SG;2;non{FUT} mi numina V;IRR;PL;2;PST na ninnangam V;PL;2;non{FUT} ba da V;IRR;SG;2 ntji nga V;IRR;SG;1 me numena V;IRR;PL;2;PST rru ngurran V;SG;1;non{FUT} a ngerra V;IRR;PC;1;PST bi bi V;IRR;SG;3 rdi nguddana V;PL;1;PST ni thardi V;SG;2;PST rri tjirri V;SG;2;PST ma thamam V;SG;1+INCL;non{FUT} me ngume V;IRR;PC;1 mu pumuni V;PL;3;PST e nerrene V;PC;2;PST rdi nguddana V;PC;1;PST na kinna V;IRR;PL;3 rdu nguddi V;IRR;PL;1;PST la killa V;IRR;PC;3 bi kubi V;IRR;PL;3 ni narnam V;PL;2;non{FUT} nu nguna V;SG;1;PST la pulle V;IRR;PL;3;PST bu nubuy V;IRR;PL;2;PST ntji thantji V;SG;2;PST ngi thungana V;IRR;SG;1+INCL;PST ni narne V;IRR;PC;2 ntha ninthangi V;IRR;PL;2;PST ngu ngungi V;IRR;SG;1;PST ma pumi V;IRR;PL;3;PST buy nubuy V;IRR;PC;2 ya ngurni V;PL;1;PST buy ngubana V;IRR;PC;1;PST li ngillingi V;IRR;PC;1;PST bi pubina V;PC;3;PST bi dim V;SG;2;non{FUT} li tjilim V;SG;2;non{FUT} na ngina V;IRR;SG;1 a pa V;IRR;SG;1+INCL bi nubi V;IRR;PC;2 ntji tje V;IRR;SG;1+INCL;PST i nuyu V;IRR;PL;2 ba ngube V;PC;1;PST be ngubena V;IRR;PC;1;PST mu kumuy V;IRR;PL;3;PST bu kubu V;IRR;PC;3 nu na V;SG;3;PST nu thuni V;IRR;SG;1+INCL;PST rra nira V;IRR;PL;2 na pinnangi V;IRR;PC;3;PST ba nube V;PL;2;PST ma nume V;PC;2;PST e tjena V;SG;1+INCL;PST la pulle V;PL;3;PST rra pe V;PC;3;PST rru ngurrini V;SG;1;PST nu punnungam V;PL;3;non{FUT} ngi nungana V;IRR;PC;2;PST be ngubem V;PL;1;non{FUT} nga pinga V;IRR;PC;3;PST rdu nuddi V;IRR;PL;2;PST ngu ngungan V;SG;1;non{FUT} a na V;IRR;PL;2 bi bina V;SG;1;PST a ngarrani V;PL;1;PST nu nunna V;IRR;PC;2 e tjem V;SG;1+INCL;non{FUT} a narrane V;PC;2;PST la tjilangi V;IRR;SG;1+INCL;PST i pirrine V;PC;3;PST ma ngama V;IRR;SG;1 mi nim V;SG;2;non{FUT} ba bam V;SG;1;non{FUT} ma numi V;IRR;PC;2;PST mi ngumi V;IRR;PC;1 rri niri V;IRR;PC;2 bi bim V;SG;3;non{FUT} rru numpan V;PL;2;non{FUT} be dena V;SG;2;PST buy thubam V;SG;1+INCL;non{FUT} ye nguy V;IRR;SG;1 ngu thunguni V;SG;2;PST ngu thungu V;IRR;SG;2 ntha nintha V;IRR;PL;2 e ngena V;SG;1;PST bi pubina V;PL;3;PST ntha nginthanyi V;PL;1;PST ngu ngungu V;IRR;SG;1 e ngerrem V;PL;1;non{FUT} ba be V;IRR;SG;1;PST rru thurran V;SG;1+INCL;non{FUT} rru thurri V;IRR;SG;1+INCL;PST rdu nuddene V;PC;2;PST rri ngirrini V;IRR;SG;1;PST ngi pungana V;IRR;PC;3;PST rdi nuddana V;PL;2;PST rra nira V;IRR;PC;2 la kila V;IRR;SG;3 li tjilingi V;IRR;SG;2;PST i nirrini V;PL;2;PST la nilla V;IRR;PL;2 ba de V;IRR;SG;2;PST buy nubana V;PL;2;PST mi mi V;IRR;SG;3 ye kuy V;IRR;SG;3 e ke V;IRR;PL;3 la pulle V;IRR;PC;3;PST e dem V;SG;3;non{FUT} be nube V;IRR;PL;2 ntha tjinthangi V;IRR;SG;2;PST na nginnangi V;IRR;PC;1;PST rra pirangi V;IRR;PL;3;PST ntha kintha V;IRR;SG;3 i yungi V;IRR;SG;3;PST be bem V;SG;3;non{FUT} na tjinanga V;SG;1+INCL;PST la ngulam V;SG;1;non{FUT} ntha ngantjim V;SG;1;non{FUT} ya ngan V;SG;1;non{FUT} ngu ngungan V;PL;1;non{FUT} e nerrena V;PL;2;PST nga pingam V;PL;3;non{FUT} ni nganam V;SG;1;non{FUT} li nilli V;IRR;PC;2 a ka V;IRR;SG;3 ngi ngungana V;IRR;PC;1;PST rru thurrini V;SG;2;PST la ngula V;IRR;SG;1 rdi nudde V;IRR;PC;2 ntji nga V;IRR;PC;1 be ngubena V;IRR;PL;1;PST ba pube V;PC;3;PST rra ngarrim V;SG;1;non{FUT} rra tjirrangi V;IRR;SG;1+INCL;PST ngi nungana V;IRR;PL;2;PST ngu punge V;IRR;PC;3;PST rdi puddana V;PC;3;PST nga pinga V;PL;3;PST i nirrine V;IRR;PC;2;PST e tjena V;IRR;SG;1+INCL;PST ngu nungu V;IRR;PL;2;PST ye nuyem V;PL;2;non{FUT} ma numi V;IRR;PL;2;PST bu thubuni V;SG;1+INCL;PST be pubena V;IRR;PL;3;PST bi pubina V;IRR;PC;3;PST rru puyi V;IRR;PL;3;PST na kinna V;IRR;PC;3 rdu nudda V;IRR;PC;2 buy nubana V;IRR;PL;2;PST la nilla V;IRR;PC;2 rdi puddam V;PL;3;non{FUT} ngu nungan V;PL;2;non{FUT} la pila V;IRR;SG;1+INCL la nulla V;IRR;PC;2 rdu nguddini V;PL;1;PST bu nubu V;IRR;PL;2 ye ngana V;IRR;SG;1;PST nga nge V;IRR;PC;1 la thule V;IRR;SG;1+INCL;PST nu ngunni V;PL;1;PST ntji ngantji V;SG;1;PST nu nunna V;PC;2;PST li kili V;IRR;SG;3 rdi nuddana V;PC;2;PST ngi thungana V;SG;1+INCL;PST i yibim V;SG;3;non{FUT} ba nubam V;PL;2;non{FUT}
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IsentropicVortex16_P1.tst
<?xml version="1.0" encoding="utf-8"?> <test> <description>Euler Isentropic Vortex P=1</description> <executable>CompressibleFlowSolver</executable> <parameters>IsentropicVortex16_P1.xml</parameters> <files> <file description="Session File">IsentropicVortex16_P1.xml</file> </files> <metrics> <metric type="L2" id="1"> <value variable="rho" tolerance="1e-12">0.0844975</value> <value variable="rhou" tolerance="1e-12">0.168375</value> <value variable="rhov" tolerance="1e-12">0.160536</value> <value variable="E" tolerance="1e-12">0.4432</value> </metric> <metric type="Linf" id="2"> <value variable="rho" tolerance="1e-12">0.0814545</value> <value variable="rhou" tolerance="1e-12">0.105266</value> <value variable="rhov" tolerance="1e-12">0.127603</value> <value variable="E" tolerance="1e-12">0.379398</value> </metric> </metrics> </test>
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/Screens/Arms File Dialog Screen.tst
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Arms File Dialog Screen.tst
ScreenName String 'Arms File Dialog Screen' ImplName String 'Dialog Screen' ElementChunkArray Int 10 ScreenElementType Int 0 ImplName String 'Front End Dialog Screen Backdrop' TabIndex Int 8 Selectable Bool False Enabled Bool True ReferenceArea Rect( 69, 169, 603, 420 ) # left,top,right,bottom ScreenElementType Int 5 ImplName String 'Arms Profiles file list' TabIndex Int 2 Selectable Bool False Enabled Bool True ReferenceArea Rect( 189, 248, 486, 338 ) # left,top,right,bottom Font String 'Univers10' ScreenElementType Int 1 ImplName String 'Load Or Save Arms Profile Button' TabIndex Int 3 Selectable Bool False Enabled Bool True ReferenceArea Rect( 505, 284, 627, 328 ) # left,top,right,bottom Font String 'BlackChancery16' Text String 'IDGS_TPFRONTENDTEXT_SCREENS_SAVE' Color Colour( 1.000000, 1.000000, 1.000000, 1.000000 ) HotKey Int -1 ScreenElementType Int 1 ImplName String 'Open Dialog Previous Button' TabIndex Int 6 Selectable Bool False Enabled Bool True ReferenceArea Rect( 505, 337, 627, 381 ) # left,top,right,bottom Font String 'BlackChancery16' Text String 'IDGS_TPFRONTENDTEXT_SCREENS_CANCEL' Color Colour( 1.000000, 1.000000, 1.000000, 1.000000 ) HotKey Int -1 ScreenElementType Int 3 ImplName String 'Profile File Name Text Entry' TabIndex Int 4 Selectable Bool True Enabled Bool True ReferenceArea Rect( 279, 341, 439, 382 ) # left,top,right,bottom Font String 'Univers10' Text String 'IDGS_TPFRONTENDTEXT_SCREENS_NULL' Color Colour( 1.000000, 1.000000, 1.000000, 1.000000 ) ScreenElementType Int 2 ImplName String 'Arms Profile Info Label' TabIndex Int 7 Selectable Bool False Enabled Bool True ReferenceArea Rect( 497, 248, 631, 274 ) # left,top,right,bottom Font String 'UniversLightBold14' Color Colour( 1.000000, 1.000000, 1.000000, 1.000000 ) ScreenElementType Int 1 ImplName String 'Center Justify Label' TabIndex Int 12 Selectable Bool False Enabled Bool True ReferenceArea Rect( 455, 216, 677, 249 ) # left,top,right,bottom Font String 'UniversLightBold14' Text String 'IDGS_TPFRONTENDTEXT_SCREENS_VICTORYPOINTS' Color Colour( 0.000000, 0.000000, 0.000000, 1.000000 ) HotKey Int -1 ScreenElementType Int 1 ImplName String 'Center Justify Label' TabIndex Int 13 Selectable Bool True Enabled Bool True ReferenceArea Rect( 466, 213, 666, 248 ) # left,top,right,bottom Font String 'UniversLightBold14' Text String 'IDGS_TPFRONTENDTEXT_SCREENS_VICTORYPOINTS' Color Colour( 1.000000, 1.000000, 1.000000, 1.000000 ) HotKey Int -1 ScreenElementType Int 1 ImplName String 'Right Justify Label' TabIndex Int 14 Selectable Bool False Enabled Bool True ReferenceArea Rect( 40, 352, 264, 371 ) # left,top,right,bottom Font String 'Univers12' Text String 'IDGS_TPFRONTENDTEXT_SCREENS_FILENAME' Color Colour( 0.000000, 0.000000, 0.000000, 1.000000 ) HotKey Int -1 ScreenElementType Int 1 ImplName String 'Right Justify Label' TabIndex Int 15 Selectable Bool False Enabled Bool True ReferenceArea Rect( 128, 350, 263, 369 ) # left,top,right,bottom Font String 'Univers12' Text String 'IDGS_TPFRONTENDTEXT_SCREENS_FILENAME' Color Colour( 1.000000, 1.000000, 1.000000, 1.000000 ) HotKey Int -1
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Assignment-3-Sagnik-Mitra-2027.sce
//Q1. Addition Of Matrix row = input("Enter Number Of Rows: "); col = input("Enter Number Of Column: "); disp("Please Enter First Mtrix:- ") for i=1:row for j=1:col first_mat(i,j) = input("/"); end end disp("Please Enter Second Mtrix:- "); for i=1:row for j=1:col second_mat(i,j) = input("/"); end end for i=1:row for j=1:col Add_matrix(i,j) = first_mat(i,j) + second_mat(i,j); end end disp("The Addition Of Two Matrix Is:- ") disp(Add_matrix) //Q2. Multiplication Of Matrix first_mat_row = input("Enter number of rows of the first Matrix: "); first_mat_col = input("Enter number of columns of the first Matrix: "); second_mat_row = input("Enter number of rows of the second Matrix: "); second_mat_col = input("Enter number of columns of the second Matrix: "); if first_mat_col ~= second_mat_row then disp('First Matrix Column Does Not Match With Second Matrix Row ') break; end disp('Enter first Matrix') for i=1:first_mat_row for j=1:first_mat_col first_matrix(i,j)=input('\'); end end disp('Enter second Matrix') for i=1:second_mat_row for j=1:second_mat_col second_matrix(i,j)=input('\'); end end matrix_mult=zeros(first_mat_row,second_mat_col); for i=1:first_mat_row for j=1:second_mat_col for k=1:first_mat_col matrix_mult(i,j)= matrix_mult(i,j)+ first_matrix(i,k)*second_matrix(k,j); end end end disp('Multiplication of the two matrices is') disp( matrix_mult) //Q3. Transpose Of Matrix rows =input("Please Enter Rows of the Matrix: "); cols =input("Please Enter Columns of the Matrix: "); disp('Enter the Matrix') for i=1:rows for j=1:cols matrixs(i,j)=input('\'); end end tran_matrix=zeros(rows,cols); for i=1:cols for j=1:rows tran_matrix(i,j)=matrixs(j,i) end end disp('Matrix Is') disp(matrixs) disp('Transposed Matrix') disp(tran_matrix)
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scilab.sci
tox = 150E-8 Na = 5E16 Nd = 5E16 es = 1E-12 eox = es/3 q = 1.6E-19 Ut = 26E-3 ni = 1.6E10 printf('\n\t I.1') Cox=eox/tox G = sqrt(2*q*es*Na)/Cox Phi_T = 2*Ut*log(Na/ni) V_T0 = Phi_T+G*sqrt(Phi_T) printf('\nPhi_T = %.2e\n',Phi_T) printf('V_T0 = %.2e\n',V_T0) printf('Gamma = %.2e\n',G) printf('\n\t I.2') Phi_mi = -0.56 Phi_ms = Phi_mi-Ut*log(Na/ni) printf('\nPhi_ms = %.2e\n',Phi_ms) Nss = 1E10 D_V0 = q*Nss*tox/eox printf('\nD_V0 = %.2e\n',D_V0) Vtp = V_T0-abs(Phi_ms)-abs(D_V0) Vtn = V_T0+abs(Phi_ms)+abs(D_V0) printf('\nVtp = %.2e\n',Vtp) printf('Vtn = %.2e\n',Vtn) printf('\n\t I.3') D_Vtp = 0.7-Vtp D_Vtn = Vtn-0.7 Nad_p = eox*D_Vtp/(tox*q) Nad_n = eox*D_Vtn/(tox*q) printf('\nNad_p = %.2e\n',Nad_p) printf('Nad_n = %.2e\n',Nad_n) printf('\n\t III.1') Vcc=5 Vout=2 mu_0 = 875*0.4 W = 1E-4 L = 1E-4 Vg = 5 V_th=0.7 R = (5-2)/(mu_0*Cox*W/L*(Vg-V_th-Vout/2)*Vout) printf('\nR = %.2e\n',R) printf('\n\t III.2') function [y]=fct(Vout) , y=Vcc-2*R*mu_0*Cox*W/L*(Vg-V_th-Vout/2)*Vout-Vout, endfunction Vout=fsolve(0,fct) printf('\nVout = %.2e\n',Vout) printf('\n\t III.3') Vg=1 Vout=Vcc-R*mu_0*Cox*W/L*(Vg-V_th)^2 printf('\nVout = %.2e\n',Vout) exit
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Ex1_9.sce
//Book Name:Fundamentals of Electrical Engineering //Author:Rajendra Prasad //Publisher: PHI Learning Private Limited //Edition:Third ,2014 //Ex1_9.sce. clc; clear; C1=100; //capacitance value in microfarad C2=150; //capacitance value in microfarad C3=200; //capacitance value in microfarad //CASE1 printf("\n (a)") Cs=(C1*C2*C3)/((C2*C3)+(C1*C2)+(C3*C1)); printf("\n The equivalent capacitance in series connection=%2.3f microfarad",Cs) //CASE2 printf("\n (b)") Cp=C1+C2+C3; printf("\n The equivalent capacitance in parallel connection=%3.0f microfarad",Cp)
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Ex8_4.sce
clear // //given s=1 //case a //the rotor circuit impedance=6+j12 obtained from (0.75+5.25)+j(5+7) as rotor resistance and reactance are 0.5 and 0.75 //rotor current=e2/z2=3.23 at angle -63.43 printf("\n At stand still the rotor current is=3.23A at angle -63.43") //case b s=0.04 //z2=(0.75+j*0.04*5)ohm //again e2=s*e2/z2=0.81 at angle -69.44A printf("\n the rotor current running at a slip of 4 with the rotor short circuited is=0.81 at angle -69.44A")
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lq.sci
function P=lq(m,x,y,s) [mx,nx]=size(x) [my,ny]=size(y) if((nx~=ny)|(mx~=1)|(my~=1)), disp('data dimension error') abort end u=zeros(m+1,nx) for i=1:m+1 do for j=1:nx do u(i,j)=x(j)^(i-1) end end coef=(u*u')^(-1)*u*y' X=poly(0,s) P=poly(coef(m+1),s,'coeff') for i=1:m do P=P*X+coef(m+1-i) end endfunction
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Ex_1_15.sce
// Exa 1.15 clc; clear; close; // Given data Rf=470;// in kohm R1=4.3;// in kohm R2=33;// in kohm R3=33;// in kohm Vi= 80;// in µV Vi=Vi*10^-6;// in volt A1= 1+Rf/R1; A2=-Rf/R2; A3= -Rf/R3; A=A1*A2*A3; Vo= A*Vi;// in volt disp(Vo,"Output voltage in volts is : ")
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8_20.sce
P=50000 lr=0.9 P0=P*1*0.9 effi=0.974 Pl=(1-effi)/effi*P0 Pi=Pl/2 Pcfl=Pi/lr/lr pf=0.8 P0=P*pf Pl=Pi+Pcfl effi=P0/(P0+Pl)*100 disp(effi) P0=P/2*lr Pl=Pi+Pcfl/2/2 effi=P0/(P0+Pl)*100 disp(effi) /////////calculation mistakes in the book
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Ex19_3.sce
//Example19.3// //The current indicates a flow rate of electrons a=10*10^-3;//C/s // coulomb per second b=1;//electron c=0.16*10^-18;//C //1 Coulomb of charge I=a*b/c mprintf("I = %e electrons/s",I) //As the oxidation of each iron atom generates two electrons d=1;//reaction e=2;//electrons r=I*d/e mprintf("\nr = %e reaction/s",r)
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Ex4_7.sce
//Ex4_7 clc IDSS=5*10^(-3) disp("IDSS = "+string(IDSS)+" ampere") // maximum drain current JFET RL=910 disp("RL= "+string(RL)+ " ohm") //Load resistance RF=2.29*10^(3) disp("RF= "+string(RF)+ " ohm") // feedback resistance R1=12*10^(6) disp("R1= "+string(R1)+ " ohm") // first resistance R1 at input side R2=8.57*10^(6) disp("R2= "+string(R2)+ " ohm") // second resistance R2 at input side VDD=(24) disp("VDD= "+string(VDD)+" volts") // Drain voltage supply VP=(-2) disp("VP= "+string(VP)+" volts") // pinch off voltage for JFET VGG=(VDD*R2)/(R1+R2) disp("VGG= VDD*R2/(R1+R2)="+string(VGG)+" volts") // Gate voltage for JFET disp("Quadratic equation =5.244*ID^(2)-55.76*ID+144=0")// Forming Quadratic equation using VGS = VGG-ID*RF and ID = IDSS(1-VGS/VP)^2 where ID in mA p = [5.244 -55.76 144] ID=roots(p)*10^(-3)// values of ID converted into Ampere by multiplying by 10^(-3) disp("ID = "+string(ID)+" ampere") // drain current JFET disp("Since ID <=IDSS, hence ID=6.214 mA cannot be chosen, so we chose ID=4.42 mA") IDQ=4.42*10^(-3) disp("IDQ ="+string(IDQ)+" A")//Since ID <=IDSS, hence ID=6.214 mA cannot be chosen, so we chose ID=4.42 mA VGSQ=VGG-IDQ*RF disp("VGSQ = VGG-IDQ*RF = "+string(VGSQ)+" volts") // Gate operating point voltage VDSQ=VDD-IDQ*(RL+RF) disp("VDSQ= VDD-IDQ*(RL+RF)= "+string(VDSQ)+" volts") // Drain voltage for JFET VDGQ=VDSQ-VGSQ disp("VDGQ = VDSQ-VGSQ ="+string(VDGQ)+" volts") // Drain-Gate voltage for JFET disp("VDGQ >magnitude_VP,Hence FET is in pinch off region")
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2019-10-10T23:36:54
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Add.tst
load Add.asm, output-file Add.out, compare-to Add.cmp, output-list RAM[0]%D2.6.2 RAM[1]%D2.6.2 RAM[2]%D2.6.2; set RAM[0] 0, set RAM[1] 0; repeat 20 { ticktock; } output; set PC 0, set RAM[0] 1, set RAM[1] 0; repeat 20 { ticktock; } output; set PC 0, set RAM[0] 0, set RAM[1] 1; repeat 20 { ticktock; } output; set PC 0, set RAM[0] -1, set RAM[1] 0; repeat 20 { ticktock; } output; set PC 0, set RAM[0] 0, set RAM[1] -1; repeat 20 { ticktock; } output; set PC 0, set RAM[0] -1, set RAM[1] 1; repeat 20 { ticktock; } output; set PC 0, set RAM[0] 1, set RAM[1] -1; repeat 20 { ticktock; } output; set PC 0, set RAM[0] -1024, set RAM[1] 1024; repeat 20 { ticktock; } output; set PC 0, set RAM[0] 555, set RAM[1] 555; repeat 20 { ticktock; } output; set PC 0, set RAM[0] -555, set RAM[1] -555; repeat 20 { ticktock; } output; set PC 0, set RAM[0] 555, set RAM[1] -100; repeat 20 { ticktock; } output; set PC 0, set RAM[0] -100, set RAM[1] 555; repeat 20 { ticktock; } output;