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Figure 3: LR meter measurements forprototype I.A. Figure 4: Longitudinal scan of the transverse DC magnetic field and corresponding kick strength for 6 GeV electron beam, using a Senis sensor. thez-axis. Thefieldwasthenmeasuredalongthelongitu- dinal axis within a range of ±150mm. Additionally, both the transverse plane...
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edbbbaec-918d-455c-b14a-91a2aa474299
corrector magnet at each longitudinal position of the sensor. Due to the limited number of inputchannels (two channels used by the sensor’s two differential outputs), frequency- dependent measurements were taken for one plane at a time. The AC scans for one plane are shown in [ 4]. AC Characterization with Search Coil ...
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fbc0cd63-49e2-4450-9345-95d4434bc8ce
Figure 5: Transfer function for the integrated field of proto- type I.A using search coil. CONCLUSION A testbench for characterising the actuator chain of the FOFBsystemforPETRAIVhasbeendeveloped,initially fortheprototypeprogramandalsoforlateruseinseriespro- ductionof the magnets. The two-sensorapproachhas been deploye...
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dd2e7173-3586-4a84-bfd0-bc2098682a98
andinparticularJörgLudwig,fortheirsupportduringthe development and measurement phase, as well as the TEMF Institute at TU Darmstadt for the extensive simulations. REFERENCES [1]S.H.Mirza etal.,“RequirementsanddesignforthePETRAIV fastorbitfeedbacksystem”,in Proc.IBIC’22 ,Kraków,Poland, Sep. 2022, pp. 343–347. doi:1/zero...
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dc051be8-c93c-47e7-bd9e-fc3f8a32e079
ISBN: 978-3-95450-252-3 ISSN: 2673-5350 doi: 10.18429/JACoW-IPAC2026-WEP6109 2802 MC6.T05: Beam Feedback SystemsWEP6109 WEP: Poster session Content from this work may be used under the terms of the CC BY 4.0 licence (© 2026). Any distribution of this work must maintain attribution to the author(s), title of the work, p...
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9f91fd4d-ec8b-43d0-9636-d9868aad6a3b
HIGHLIGHTS OF SPILL OPTIMIZA TION SY S TEM US A GE A T GSI AND PR OGRESS OF C ONTR OLS INTEGRA TION P . Nieder ma y er*, H. Bräuning , V . Kamerdzhie v , H. Lieber mann , T . Milosic , D. Ondreka , R. Singh , J. S tadlmann , M. T raxler , M. W iebusc h , B. Zipf el GSI Helmholtzzentr um für Sc hw er ionenf orsc hung, ...
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a5203a84-dfc8-4110-92db-86c16b2fb716
e x p e r i m e n t a l c a m p a i g n s , e n a b l i n g i m p r o v e d s p i l l s t a b i l i t y a n d m o r e e ffi c i e n t b e a m d e l i v e r y t o u s e r s u n d e r v a r i o u s o p e r a t i o n a l c o n d i t i o n s . T h e e x p e r i e n c e g a i n e d d u r i n g t h e s e...
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0bf39a12-b11a-4daf-bae2-36c9a5bc5990
m o n i t o r i n g o f s l o w e x t r a c t e d s p i l l s t h r o u g h t i g h t e r c o u p l i n g w i t h a c c e l e r a t o r c o n t r o l s a n d u n i fi e d h u m a n a n d m a c h i n e i n t e r f a c e s . T h i s c o n t r i b u t i o n s u m m a r i z e s t h e o p e r a t i o n ...
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320de23c-be8c-4d5f-8967-27d81880b420
u p t o u r a n i u m t o a b r o a d e x p e r i m e n t a l p r o g r a m [ 1 ] . T h e r e b y , r e s o n a n t s l o w e x t r a c t i o n i s u s e d t o d r i v e p a r t i c l e s i n t o t h e e x t r a c t i o n b e a m l i n e s , e i t h e r c o n t r o l l e d b y a q u a d r u p...
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a641619f-7b63-446f-9b4b-84898b30e648
t y p i c a l l y o b s e r v e d s p i l l i n t e n s i t y fl u c t u a t i o n s a n d d r i f t s a r e detr imental to the efficient beam usag e. T h e S p i l l O p t i m i z a t i o n S y s t e m ( S O S ) [ 2 – 4 ] w a s d e v e l - o p e d t o o p t i m i z e t h e e x t r a c t i o n p r ...
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89e8b32d-285c-4271-a9bf-f7fb3f784cef
s i g n a l f o r t h e k n o c k - o u t e x c i t a t i o n s y s t e m [ 5 ] . I n t h e c a s e o f a q u a d r u p o l e - d r i v e n e x t r a c t i o n , i t p r o d u c e s a t u n e r a m p w i t h a m o d u l a t i o n [ 6 ] f o r t h e q u a d r u p o l e p o w e r s u p p l y . ...
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1a41ae57-2174-43c2-8e3d-bcb6d366034f
Optimization Sy s tem can be f ound in [ 2 ] . * p.nieder ma y er@gsi.deOPERA TION AL HIGHLIGHTS D u r i n g t h e 2 0 2 5 b e a m t i m e s t h e S p i l l O p t i m i z a t i o n S y s t e m w a s u s e d a s a s t a n d a l o n e s y s t e m f o r R F - K O e x t r a c - t i o n . A s t h e c o n...
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e4820c69-1865-4f7d-9606-a7402f80199a
t h e N U S T A R , R ³ B a n d H A D E S c o l l a b o r a t i o n s , b i o p h y s i c s g roups and detector researc h prog rams [ 7 – 11 ] . HADES F AIR Phase 0 Gold Run F r o m 2 6 . A p r i l t h r o u g h 5 . M a y 2 0 2 5 t h e H A D E S c o l l a b - o r a t i o n [ 1 2 ] c o n t i n u e d ...
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052db894-bafe-4576-8edd-f542dc7e3e1c
t o r o f u p t o 1 2 kHz a t t h e e n e r g y o f 6 0 0 MeV / nucleon . A m o n g o t h e r f a c t o r s , t h e i n c r e a s e c o m p a r e d t o p r e v i o u s b e a m t i m e s w i t h o n l y 8 kHz [ 1 3 ] i s p o s s i b l e b e c a u s e o f t h e s p i l l q u a l i t y o ...
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e36873ee-5c49-4240-a1a2-3f63f4b88aec
t o t a l o f 6 b i l l i o n e v e n t s a n d 2 6 0 TB o f d a t a w e r e r e c o r d e d d u r i n g t h e 2 1 6 h o u r s o f t h e b e a m t i m e ( F i g .   1 ) . T h e c o l l a b - o r a t i o n r e p o r t s t h a t t h i s i s a l m o s t t h e n u m b e r o f a n t i c i p a ...
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276abe1b-0d67-488c-938a-3872036f3ca0
e n e r g i e s d u r i n g t h e 2 0 2 5 g o l d b e a m t i m e . T h e h a t c h e d a r e a m a r k s t h e e a r l y s t a r t o n t h e w e e k e n d b e f o r e t h e s c h e d u l e d b e a m t i m e . T h e g r e e n w e d g e m a r k s t h e e v e n t r a t e a s s u m e d i n t...
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28cfefa9-42d3-4427-8039-a3443195c69b
Dual Ion Beam Ther apy S tudy I n M a y 2 0 2 5 s t u d i e s o n t h e s p i l l p r o p e r t i e s o f a b e a m c o n s i s t i n g o f t h e t w o i o n s p e c i e s C1 2 3+ a n d He4 + w e r e c o n d u c t e d a t S I S 1 8 [ 1 1 ] . S u c h b e a m s h a v e a p p l i c a t i o n s i...
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1
51ec257a-6222-44ab-a298-bcf751fe999f
S y s t e m b a s e d o n t h e m e a s u r e d c a r b o n s i g n a l ( F i g .   2 ) . K e e p i n g t h e c a r b o n i n t e n s i t y i n t h e s p i l l a t a c o n s t a n t v a l u e e n a b l e d s t u d i e s o n t h e t i m e c u r v e o f t h e h e l i u m f r a c t i o n o v e...
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b55b571c-08f7-41a5-8c31-07d9f1665c6b
Extraction time / s0 . 00 . 20 . 40 . 60 . 81 . 01 . 21 . 4Intensity / arb. unit F i g u r e 2 : I n t e n s i t y o f c a r b o n a n d h e l i u m c o n t r i b u t i o n s i n t h e e x t r a c t e d s p i l l . T h e i n t e n s i t y f e e d b a c k c o n t r o l u s e s t h e c a r b o n s i g...
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58c52199-5fdf-4387-9977-5a2bed0c0c28
t i o n S y s t e m o n a r e g u l a r b a s i s w i t h o u t t h e n e e d f o r e x p e r t i n t e r v e n t i o n s f o r s e t u p , a f u l l c o n t r o l s y s t e m i n t e g r a t i o n o f t h e s y s t e m w a s r e q u i r e d . T h i s i n c l u d e s i m p l e m e n t i n g e...
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7e69e427-24fa-4a10-8b38-9a76ed5c3ecf
p a r a m e t e r s a n d d e t e c t o r c a l i b r a t i o n f a c t o r s . I n a d d i t i o n , a n i n t e g r a t e d u s e r i n t e r f a c e ( G U I ) f o r t h e o p e r a t i n g p e r s o n n e l a n d p e r s i s t e n t s t o r a g e o f a l l r e l e v a n t p a r a m e t e r s i...
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f8d1054c-756b-4ddb-9f49-a874ab29e5ba
d y n a m i c i n t e n s i t y c o n t r o l a n d s p i l l p a u s e f o r b i o p h y s i c a l a p p l i c a t i o n s , s p i l l a b o r t f o r m a c h i n e a n d d e t e c t o r s a f e t y , a n d a p a r a m e t r i z e d c o n t r o l c u r v e t o e n a b l e o p e r a t i o n w h ...
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1
318c490c-04d5-4839-8193-963670ffac2b
m u l t i p l e x e r w a s b u i l d t o d y n a m i c a l l y r o u t e s i g n a l s f r o m v a r i o u s b e a m - l i n e a n d e x p e r i m e n t d e t e c t o r s t o t h e f e e d b a c k s y s t e m . I n c o m b i n a t i o n w i t h t h e F E S A i m p l e m e n t a t i o n , t h i s...
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09de3c31-8a5e-4ae3-89a4-b30d9edcf6a7
t h e d e v e l o p m e n t o f a d e d i c a t e d G U I ( F i g .   3 ) w i t h b u i l t - i n e x p e r t - k n o w l e d g e ( p r e s e t s , s a n i t y c h e c k s ) t o g e t h e r w i t h c o m p r e h e n s i v e d o c u m e n t a t i o n e n a b l e s r o u t i n e o p e r a t i o n b y ...
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560bdffb-87c5-4e71-b69d-70ac4f941cd2
personnel will f ollo w . F igure 3: Screenshot of the GUI f or operating the SOS OUTLOOK F o l l o w i n g t h e s u c c e s s f u l u t i l i z a t i o n o f t h e S p i l l O p t i - m i z a t i o n S y s t e m f o r R F - K O e x t r a c t i o n f r o m S I S 1 8 d u r i n g t h e 2 0 2 5 b e a m...
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ad9a6ba8-7368-46f9-87f9-3da3ec9cd62e
REFEREN CES [1] J . S t a d l m a n n e t a l . , “ N e w c a p a b i l i t i e s o f S I S 1 8 a f t e r u p g r a d e p r o g r a m a s F A I R i n j e c t o r ” , p r e s e n t e d a t I P A C ’ 2 6 , D e a u v i l l e , France, Ma y 2026, paper THP4002, this conf erence. [2] P . N i e d e r m a y...
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41dc8e03-40a2-43ce-9a6b-0636c866c4af
ISBN: 978-3-95450-252-3 ISSN: 2673-5350 doi: 10.18429/JACoW-IPAC2026-WEP6111 2804 MC6.T05: Beam Feedback SystemsWEP6111 WEP: Poster session Content from this work may be used under the terms of the CC BY 4.0 licence (© 2026). Any distribution of this work must maintain attribution to the author(s), title of the work, p...
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2df8a358-4697-43a1-8d21-a2dc86f0ab17
[3] P . N i e d e r m a y e r , “ T r a n s v e r s e e x c i t a t i o n f o r b e a m d i a g n o s t i c s a n d s l o w e x t r a c t i o n f r o m s y n c h r o t r o n s ” , D o c t o r a l d i s s e r - tation, Goethe-U niv ersität Frankfur t, 2025. [4] P . N i e d e r m a y e r , “ S o f t w a r ...
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39b57a52-e404-4260-be8e-6e45122adb18
s l o w - e x t r a c t i o n b e a m s p i l l u s i n g t r a n s i t - t i m e - d e p e n d e n t t u n e m o d u l a t i o n ” , P h y s . R e v . A p p l . , v o l .   1 3 , n o .   4 , p .   4 4 0 7 6 , 2 0 2 0 . doi:10.1103/PhysRevApplied.13.044076 [7] P . R u s s o t t o e t a l . , “ S t u ...
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612d3bd8-b70f-4c15-b2ff-3edcbd1e945b
H A D E S ” , i n P r o c e e d i n g s o f S c i e n c e , F A I R n e x t G e n e r a t i o n Scientis ts – 8th Edition W orkshop, 2026, v ol.  475, p.  17. doi:10.22323/1.475.0017[9] A . H e r l e r t , “ T h e N U S T A R p r o g r a m a t F A I R : O v e r v i e w a n d p r e s e n t s t a t u s...
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c61bd516-781f-43f1-8755-0552c9af1e46
d e n c e w i t h h i g h - m o m e n t u m p r o t o n s ” , P h ys i c a l R e v i e w Le tt er s , v ol.  136, no.  14, p.  142501, 2026. doi:10.1103/6vsl-ng7x [11] A . P a s t u s h e n k o e t a l . , “ F l a t C / H e s p i l l s f o r o n l i n e r a n g e m o n - i t o r i n g i n p a r t i c...
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2
9d61811a-7f88-4e52-9ae1-01c930219bc3
f e a t u r i n g t h e n e w H A D E S A u + A u d a t a ” , N u c l e a r P h y s i c s A , v o l .   9 3 1 , Q U A R K M A T T E R 2 0 1 4 , p p .   7 8 5 – 7 8 9 , 2 0 1 4 . https://doi.org/10.1016/j.nuclphysa.2014.09.035 [14] E . R e n n e r e t a l . , “ F i r s t m i x e d H e / C i o n b ...
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b8d31e4a-f2c2-49c2-af6f-0731f580f25f
ISBN: 978-3-95450-252-3 ISSN: 2673-5350 doi: 10.18429/JACoW-IPAC2026-WEP6111 MC6.T05: Beam Feedback Systems 2805WEP: Poster session WEP6111 Content from this work may be used under the terms of the CC BY 4.0 licence (© 2026). Any distribution of this work must maintain attribution to the author(s), title of the work, p...
D:\Daily_ihep\Conferences\IPAC2026\WEP\WEP6111.pdf
2
ebc73e24-a686-419d-8638-5c35c4d5f34e
SYNCHRONIZED DEMULTIPLEXING OF A BEAM CURRENT SIGNAL FOR A BUNCH-BY-BUNCH LONGITUDINAL FEEDBACK SYSTEM C. Reinwald, H. Klingbeil1, Technical University of Darmstadt, Darmstadt, Germany 1also at GSI Helmholtzzentrum für Schwerionenforschung GmbH, Darmstadt, Germany K. Groß, M. Hardieck, D. Lens, GSI Helmholtzzentrum für...
D:\Daily_ihep\Conferences\IPAC2026\WEP\WEP6113.pdf
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93a673b8-481c-4f85-ad49-0de23d1dc62c
cessing of a beam current signal provided by a Fast Current Transformer. This signal is utilized as main input for the feedbacksystemin order to detect longitudinal beam oscil- lations of individual bunches. Therefore, it is demultiplexed into a sequence of segments, each containing the beam cur- rentsignalofasinglebuc...
D:\Daily_ihep\Conferences\IPAC2026\WEP\WEP6113.pdf
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eeb84c89-eb55-4c6d-8ebc-8a304fc456c7
forheavy-ionresearchinGermany,aBunch-By-BunchLon- gitudinal Feedback System is in development. A schematic showing the basic topology of the system is provided in Fig.1. FCT DEMUXuFCTSignal Processing Bunch 1 Signal Processing Bunch 2 ... Signal Processing Bunch 10MUXKickerCavity Beam Figure 1: Schematic visualizing th...
D:\Daily_ihep\Conferences\IPAC2026\WEP\WEP6113.pdf
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ae68fee2-37d9-4d92-9d2c-dfc8002dcfb6
one specific bunch resulting in signals like 𝑢FCT,b1shownon the right-hand side of Fig. 2. This separation enables anindividualmonitoringofthesinglebunchesinthering by their dedicated signal processing units which, in case longitudinal bunch oscillations are detected, generate corre- sponding feedback signals to damp ...
D:\Daily_ihep\Conferences\IPAC2026\WEP\WEP6113.pdf
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cfe6a276-964f-4391-a8af-02b08a126bd2
Longitudinal Feedback System can be found in [ 2–4]. 0.0 0.5 1.0 1.5 2.0 2.5 3.0 3.5 4.0 Time in s 1.00 0.75 0.50 0.25 0.000.250.500.751.00Voltage in VuLFDDSA uLFDDSB uFCT 0.0 0.5 1.0 1.5 2.0 2.5 3.0 3.5 4.0 Time in s 1.00 0.75 0.50 0.25 0.000.250.500.751.00Voltage in VuLFDDSA uLFDDSB uFCT,b1 Figure 2: The diagram on t...
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81d76c2a-b591-44b2-bec6-8d3718bbe086
(LFDDSA) and Longitudinal Feedback DDS B (LFDDSB) forthegenerationoftheharmonicreferencesignals 𝑢LFDDSA and𝑢LFDDSBvisualizedinFig. 2usingDirectDigitalSynthe- sis(DDS).Additionally,thesystemincludestwoCalibration ElectronicsModules(CEL)toadjustthephaseoftherefer- ence signals, a demultiplexer module (DEMUX) to forward...
D:\Daily_ihep\Conferences\IPAC2026\WEP\WEP6113.pdf
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e0a0c34f-d861-4050-80bc-1d52bda6e724
ISBN: 978-3-95450-252-3 ISSN: 2673-5350 doi: 10.18429/JACoW-IPAC2026-WEP6113 2806 MC6.T05: Beam Feedback SystemsWEP6113 WEP: Poster session Content from this work may be used under the terms of the CC BY 4.0 licence (© 2026). Any distribution of this work must maintain attribution to the author(s), title of the work, p...
D:\Daily_ihep\Conferences\IPAC2026\WEP\WEP6113.pdf
0
3f937b2c-1f3b-4c2a-8195-72c365ba50e6
Thedemultiplexingprocessiscontrolledbythetwohar- monic RF reference signals 𝑢LFDDSAand𝑢LFDDSB. Such signals are utilized as references for various purposes all over the facility, e.g. to generate synchronized gap voltages in all cavities. Their correct timing is ensured bythe Bunch- phaseTimingSystemBuTiS[ 5,6]andthe...
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f700726a-4326-459d-ae1a-cd235e6496a0
𝑢LFDDSBtosendonlyonepulseofasinglebunchintheFCT signaltoeachsignalprocessingunit. Thisisalsovalidfor 𝜑R≠ 0as the negative zero crossing of 𝑢LFDDSBrepresents theboundarybetweentwoRFbuckets. Aftereachrevolution, the number of the active output port of the demultiplexer is resetusingthepositivezerocrossingof 𝑢LFDDSA,e...
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438623a9-dd34-4d4c-b63d-022630bd4f48
The FCT is located at the synchrotronring while all other componentsare located in theRF supplyarea. The lengths ofthetransmissionlinesarevalidforthesynchrotronSIS18 wherethesetup iscurrentlytested. ThelengthsforSIS100 may vary. In order to ensure that the phase relations at the green line in Fig. 3do not depend on the...
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9fe4bfda-9991-4e5c-856e-6392d00fd23b
processingdelayintroducedbytheTriggerUnitwithinthe Longitudinal Feedback System, but those are compensated locally through the insertion of transmission lines in the parallel signal paths.PHASE CORRECTIONS FOR THE RF REFERENCE SIGNALS Since fixed, frequency-independent phase differences be- tween𝑢LFDDSA,𝑢LFDDSBand𝑢F...
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e8bf9f7e-c91c-4758-88c3-b81a60bd23c3
measurement, they have to refer to the same position in the ring,inthiscasethepositionoftheFCT 𝜃FCT. Thus,con- sideringabeamcirculatinginclockwisedirectionandthe basic description 𝑢DDS(𝑡) =̂𝑉sin(ℎ𝜔R𝑡 −𝜑∗) for the harmonic reference signals with an optional phase offset𝜑∗, they have to be shifted according to 𝑢...
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thenewsynchrotronSIS100thebeamwillcirculatecounter- clockwise but the main principles do not change. θFCT ωRtθref Figure 4: Diagram indicating the reference position 𝜃reffor RF reference signals in the ring, the FCT position 𝜃FCTand a beam circulating in clockwise direction with a revolution frequency of 𝜔R.17th Int...
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EXPERIMENTAL VERIFICATION OF THE DEMULTIPLEXING The functionality of the demultiplexing of the beam cur- rent signal independent of the current RF frequency has been confirmed in a machine experiment with beam in July 2025. Inthisexperiment,theLongitudinalFeedbackSystem wasusedtodamplongitudinaldipoleoscillationsofindi...
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tionsfortheexperiment,demonstratesthefunctionalityof thisprocessbyprovidingawaterfalldiagramofademulti- plexed beam current signal over a whole acceleration cycle. Inthisplot,regionsofthedemultiplexedsignalcontaining the beam pulses of a single bunch can easily be separated from the light blue regions indicating 𝑢FCT=...
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as it distributes corresponding signal parts to dedicated pro- cessing units. In order to operate the system independent of the RF frequency, the influence of signal delays had to be takenintoaccountbyinsertingadditionaltransmissionlines fordelaycompensation. Furthermore,aphasecorrectionfor thereferencesignalscontrolli...
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uFCT,b2 Figure5: Measurementresultsshowingthesuccessfulde- multiplexingof a beam current signal during operation with a harmonic number of ℎ = 2and a synchronous phase of 𝜑R≈ 2.5°. 2 1 0 1 2 t in s 0100200300400500600Segment time t in ms 0.025 0.0000.0250.050 uFCT,b1Figure6: Waterfalldiagramofademultiplexedbeamcurre...
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doi:1/zero.alt4.18429/JACoW-IPAC2/zero.alt415-MOPHA/zero.alt421 [3]D.Lens,H.Klingbeil,“StabilityofLongitudinalBunchLength FeedbackforHeavy-IonSynchrotrons”, Phys.Rev.STAccel. Beams, vol. 16, no. 3, March, 2013. [4]H.Klingbeil, D. Lens,M. Mehler,B. Zipfel,“ModelingLon- gitudinal Oscillations of Bunched Beams in Synchrot...
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ICALEPCS’09 , Kobe, Japan, Oct. 2009, paper TUC004, pp. 93–95. [8]M.Lipiński, T.Włostowski,J.SerranoandP.Alvarez,“White rabbit: APTPApplicationforRobustSub-NanosecondSyn- chronization”, in Proc. IEEE ISPCS , Munich, Germany, 2011, doi:1/zero.alt4.11/zero.alt49/ISPCS.2/zero.alt411.6/zero.alt47/zero.alt414817th Internati...
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TOWARDS FAST ORBIT CORRECTION: A MODULAR AND EXTENSIBLE GLOBAL ORBIT FEEDBACK SYSTEM A. Aljadaa∗, A. Ahmad, A. Abbadi, H. Al-Mohammad, M. Attal, S. Kasaei SESAME Synchrotron, Allan, Jordan Abstract AtSESAME, orbit correction was previouslyperformed every 5 seconds (0.2 Hz) using MATLAB. However, due to thelimitedcorrec...
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system, implemented in C, achieves sampling rates up to 10Hz,enablingcorrectionofhigher-frequencydisturbances that were previously unaddressable. The system architecture was designed with modularity asacoreprinciple,facilitatingeasymodificationandinte- grationofdifferentcontrolandestimationalgorithms. The completeecosy...
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rection: aC-basedcorecorrectionengine,anEPICSIOC, and a Qt-based graphical user interface. Thecorecorrectionengine,implementedinC,executes the orbit feedback algorithm at a 10 Hz sampling rate. This componentreads slowacquisition(SA)beam position data from the Beam Position Monitors (BPMs) electronics (Lib- era Brillia...
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setpoints, controller gains, and diagnostic signals. ∗amro.aljadaa@sesame.org.joThe Qt-based graphical user interface provides operators withcomprehensivesystemvisualizationand controlcapa- bilities. TheGUIdisplaysliveorbitdatainmultiplerepre- sentations: time-domainwaveformsfortrackingtransientbe- havior, frequency-do...
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proachdecomposestheorbitresponsematrixintoorthogonal eigenmodes, enabling decoupled correction of individual orbit modes while providing inherent numerical stability. The fundamental correction equation relates the required corrector current changes to the measured orbit deviations: Δ𝐼 = 𝑉 ⋅𝑆inv⋅𝐶𝑧⋅𝑈𝑇⋅Δ𝑥, where...
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primarycorrectionmechanism. ChangesinRFfrequency modulate beam energyto matchthe design energy. RF cor- rection is applied first to stabilize beam energy, followed by correctormagnetsforfineorbitadjustment. Thisapproach reduces the correction load on the magnets and prevents corrector saturation. Figure1illustrates the...
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lectable stateestimationalgorithms, each offering different tradeoffs between noise rejection and response time.17th International Particle Accelerator Conference, Deauville, France JACoW Publishing ISBN: 978-3-95450-252-3 ISSN: 2673-5350 doi: 10.18429/JACoW-IPAC2026-WEP6114 MC6.T05: Beam Feedback Systems 2809WEP: Post...
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BPMs EstimatorΔI, Δf Feedback ControllerMachineFeedforward Controller Golden Orbit Correctors + RF +-Figure 1: Orbit correction systemarchitecture. TheMovingAverage(MA)filtercomputesasimplearith- metic mean over a sliding window of N samples: ̂ 𝑥[𝑘] =1 𝑁𝑁−1 ∑ 𝑖=0𝑥[𝑘 −𝑖]. This approach provides straightforward n...
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characteristics through adjustment of the weighting parame- ter. Forapplicationsrequiringoptimalnoise rejection,a dis- creteKalmanfiltercanbeused,whichprovidestheoretically optimal estimates when noise statistics are properly charac- terized. Themodularsoftwarearchitectureenablesconfigurable selectionbetweenestimationa...
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beneficial. Feedback Controller The feedback controller implements a Proportional- Integral (PI) control law in discrete time. The PI controller provides both immediate response to orbit errors throughthe proportional term and elimination of steady-state errors through the integral term. The discrete-time PI controller...
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and noise sensitivity of derivative action is unnecessary. The gain structure implements a two-level hierarchy to provide both global and local control authority. Global pro- portionalandintegralgainsareconfiguredthroughthegraph- icaluserinterface,providingconvenientadjustmentofthe overall loop response. Additionally, ...
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02d3d501-9c36-4226-9bcc-e6018ba0d40e
mentsfeedforwardcompensationtopreemptivelycounteract known disturbance sources. The primary application targets orbit disturbances induced by insertion devices. Insertiondevicessuchaswigglersandundulatorsproduce strong magnetic fields that vary with gap and shift changes. As users adjust these parameters during experim...
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Ratherthanrelyingsolelyonfeedbacktocorrectthesedis- turbances after they occur, feedforwardtable compensation applies precalculated corrector adjustmentssimultaneously with the parameter changes, significantly reducing transient orbit excursions. The feedforward implementation employs Python scripts thatmonitorinsertio...
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plifies measurement noise into large corrector demands that may exceed physical limits or cause instability. Two approaches are implemented to address this ill- conditionedinverseproblem. ThefirstemploysSVDtrunca- tion,wheresingularvaluesbelowaspecifiedthresholdare entirely excluded from the correction, effectively dis...
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ofregularization,enablingustoadaptthecorrectionstrategy to changing operational conditions without recompiling the core correction engine. FUTURE WORK The current implementation operating at 10 Hz sampling rate represents an intermediate step toward achieving true FastOrbitFeedback(FOFB)capabilities. Severalenhance- me...
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parameter optimization for future FOFB implementations.PreparatoryworktowardsFOFBhasalreadybeencom- pleted,includingfastBPMdataacquisitionsoftware. The modulararchitecturesupportsintegrationofFPGAsolutions for hardware-accelerated computation at higher rates. The ultimate goal is transition to FOFB operation [ 5] atsig...
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toaddressthelimitationsofthepreviousMATLAB-based implementation. The migration to C-based implementation enabled a 50-foldincrease in sampling rate, from 0.2 Hz to 10Hz,significantlyimprovingthesystem’sabilitytocorrect higher-frequency orbit disturbances. Themodularsoftwarearchitectureprovidesplug-and-play capability f...
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prehensive approach addresses all aspects of orbit feedback systemoperationfromimplementationthroughcommission- ing to long-term performance assessment. The system has been successfully deployed in produc- tion, demonstrating improved orbit quality. As indicated by the title, this implementation establishes the foundat...
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studies during ALBA commissioning”, in Proc. IPAC’11 , San Sebastián, Spain, Sep. 2011, paper THPC056, pp. 3020–3022. [4]M.T.Heron etal.,“Diamondlightsourceelectronbeampo- sition feedback”, in Proc. ICALEPCS’09 , Kobe, Japan, Oct. 2009, paper THB003, pp. 650–652. [5]J. Chenet al., “Status of SSRF fast orbit feedback sy...
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190717b4-26a4-4bd8-848c-1bd80ca14ea5
AUTOMATED SOFTWARE WORKFLOW FOR ACCELERATOR CONTROL SYSTEMS USING CONTAINERIZATION A. Aljadaa∗1, A. Ahmad1, A. Abbadi1, M. Alzubi1,2, R. Khrais1 1SESAME Synchrotron, Allan, Jordan 2Princess Sumaya University for Technology, Amman, Jordan Abstract A new software workflow has been developed and de- ployed at SESAME that ...
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f40f3c03-70a5-4b58-ab12-21ccb661b81d
facilityischallengingduetovarioussourcesoffailure: hard- warefailuresinserversandnetworks,operatingsystemis- sues like high CPU and memory usage, and application issues suchas crashes and memory leaks. Traditionalman- ual deployment workflows compound these challenges by introducing human error. This paper presents an ...
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d8e57c41-add2-49c4-8842-80e4678f9fe2
containerization, orchestration with Kubernetes, release management with Helm, and continuous deployment au- tomation. Figure1illustrates the workflow, which is discussed in detail in the following sections. This workflow has been deployed in production for all machine IOCs at SESAME Synchrotron Light. CONTAINERIZATION...
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9aa5c284-557b-442b-9612-b59c4f157763
development machineIOC Source + Dockerfile + Helm chartFigure 1: Complete workflow from development to produc- tion deployment. ofdeploymentissues. Tooptimizetheseimages,amultilayer approach is followed when building Docker images. This modularizesthedevelopmentprocessbycreatingimagesfor common dependencies, thereby re...
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e14a7baf-11d6-45b7-96bc-fa15bee074a8
centralized management of these containers requires orches- tration. ORCHESTRATION TomanageDockerIOCsfromacentralnode,Kubernetes [3] was selected as the container orchestration tool. Kubernetes plays a vital role in IOC management, act- ing as a central manager that provides a global view of the entire system and aggre...
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a1056fd3-5e54-4b0f-af0e-d099f25275be
ISBN: 978-3-95450-252-3 ISSN: 2673-5350 doi: 10.18429/JACoW-IPAC2026-WEP6115 2812 MC6.T33: Online Modelling and Software ToolsWEP6115 WEP: Poster session Content from this work may be used under the terms of the CC BY 4.0 licence (© 2026). Any distribution of this work must maintain attribution to the author(s), title ...
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e6c01579-70ab-4dee-8fb7-7eb2d4c795e3
rockylinux:8.10 stream-device-ioc caen-ioc s7nodave-ioc alpineFigure 2: MultilayerDockerimagebuild process. remotemanagementoverlow-bandwidthconnections,faster keyboard-driven navigation, real-time cluster monitoring, and native Helm release management capabilities. Both tools enable manual IOC control and shell access...
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d1f68eed-589c-428b-ac5d-de4ccefe4ea2
Kubernetesalsoimprovesserviceavailabilitybyautomat- ically redeploying the IOCs from failed servers to healthy ones. IfanIOCfailsduetoanapplicationissue,Kubernetes automatically restarts the IOC. Finally, Kubernetes enables resource management by ap- plying CPU and memory constraints to pods. The Ku- bernetes scheduler...
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da457b63-f9fe-4523-af89-0df99a394489
dates and rollbacks through version management, allowing deployment of IOC instances to the cluster and manage- mentofmultipleIOCversions. Helm’stemplatingsystem provides consistency across deployments while allowing fine-grained customization for individual IOC requirements. EachHelmreleasemaintainsacompleteversionhis...
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d4594b29-95ae-4714-ab71-8cc044e5ddf5
tem provides a clear audit trail of all deployment changes, enabling easy identification of the currently running IOC version. AllKubernetesresourcesrequiredtodeployanIOCare packaged in a Helm chart according to Figure 3. A typi- cal chart contains severalcomponents organized in a stan- dardizeddirectorystructure. TheC...
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9327fc6d-c9f9-47f9-bae9-1bf5cb8f2b59
allowsasinglecharttemplatetobereused acrossdifferent IOCs by simply modifying the values file, promoting con- sistency while enabling customization. The deployment template utilizes Helm’s templating syn- tax to reference values dynamically. It defines the Kuber- netes deployment resource with specifications for pod me...
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d520399b-8cfe-4cde-8701-64cab9bc1949
tentVolumeClaimtemplaterequestsstorageresourcesand bindstothevolume. Thesearemountedintothecontainerat theautosavedirectory,ensuringIOCstatepersistenceacross pod restarts and node failures. CONTINUOUS DEPLOYMENT With containerization, orchestration, and package man- agement established, the final component automates th...
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dfcd307f-8521-478e-a51e-3ee6f32d246e
ISBN: 978-3-95450-252-3 ISSN: 2673-5350 doi: 10.18429/JACoW-IPAC2026-WEP6115 MC6.T33: Online Modelling and Software Tools 2813WEP: Poster session WEP6115 Content from this work may be used under the terms of the CC BY 4.0 licence (© 2026). Any distribution of this work must maintain attribution to the author(s), title ...
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d19936d0-cbcc-4dad-ba07-283bfa1d99f8
Cleanup artifacts from previous builds NO YESCheck git tag Build new image Helm package + Update Helm repo Helm install / upgradeStopFigure 4: Continuous deploymentpipeline. detected on the latest commit; regular commits without tags bypassthedeploymentprocess,ensuringcontrolledreleases to production. Thedeploymentproc...
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for new IOCs or an upgrade for existing deployments.This automated pipeline significantly improved deploy- ment speed across all target machines while eliminating human errors such as incomplete deployments and inconsis- tent configurations. Build failures are immediately reported via email with detailed logs, enabling...
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associatedwithmanualworkflows. Thisapproachdemon- strates the benefits of adopting modern industry-standard tools in large scientific facilities. REFERENCES [1]G. Knap, T. M. Cobb, Y. Moazzam, U. K. Pedersen, and C. J. Reynolds, “Kubernetes for EPICS IOCs”, in Proc. 18th Int. Conf. on Accelerator and Large Experimental...
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netes”, https://helm.sh [6]JenkinsCommunity,“Jenkins”, https://www.jenkins.io17th International Particle Accelerator Conference, Deauville, France JACoW Publishing ISBN: 978-3-95450-252-3 ISSN: 2673-5350 doi: 10.18429/JACoW-IPAC2026-WEP6115 2814 MC6.T33: Online Modelling and Software ToolsWEP6115 WEP: Poster session Co...
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TUNE COMPENSATION FOR INSERTION DEVICES MOTION AT THE SOLARIS STORAGE RING M. Ünal†, R. Panas, A.I. Wawrzyniak, W. Wiatrowska SOLARIS National Synchrotron Radiation Centre, Krakow, Poland Abstract Precise control of betatron tune is essential for maintaining beam stability in modern synchrotron light sources. ...
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parameters (gap, phase) and the corresponding tune shifts. Prior to table generat ion, the magnets' response matrices for both tune planes were independently obtained. INTRODUCTION The SOLARIS synchrotron operates at 1.5 GeV and provides light to seven independent beamlines. Three of them are using APPLE II typ...
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f51e8f8e-6151-4481-926f-c20b13caa980
APPLE II type undulator with the strongest influence on tune [2]. The method includes the betatron tune measurements by exciting coherent transverse oscillations with dipole kicker (hori zontal) and pinger (vertical) magnets . Tune s are calculated from turn -by-turn BPM signals using the FFT analysis . N...
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across all undulator gap and phase settings. Finally, using the SVD method, a look- up table was constructed, containing undulators settings and corresponding correcting magnets currents. _____________________________________ †corresponding author: maria.unal@uj.edu.pl The table was tested in standard operati...
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tune response . The measurement was performed with the undulator in the open- gap configuration. Quadrupole currents were varied in steps of 0.05 A for focusing quadrupoles and 0.03 A for defocusing magnets, with ±10 steps around the nominal operational value. For each current setting, three tune measurement...
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058c7061-95e9-460d-8a5d-a63554700568
𝜈𝜈=𝑎𝑎⋅𝐼𝐼+𝑏𝑏 . (1) Where ν denotes fractional tune value and I the quadrupole current. The obtained coefficients are summarized in Table 1. Each m easurement w as repeated three times per magnet to estimat e statistical uncertainty . 17th International Particle Accelerator Conference, Deauvi...
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Table 1: Tune Response Matrix with Standard Errors Magnet type 𝒅𝒅𝝂𝝂𝒚𝒚 𝒅𝒅𝒅𝒅±SE [10-3 A⁻¹] 𝒅𝒅𝝂𝝂𝒙𝒙 𝒅𝒅𝒅𝒅±SE [10-3 A⁻¹] PFS loc. 2.60 ± 0.04 0.9 ± 0.4 SQFO loc. -2.21 ± 0.01 2.50 ± 0.05 PFS 29.3 ± 0.2 -1.5 ± 0.1 SQFO -22.4 ± 0.1 29.5 ± 0.2 Furthermore, disturbance map of vertical and horiz...
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observed [ 2]. Three repeated measurements were performed for each gap–phase combination. The mean value and standard error were calculated , with the relative uncertainty remaining below 0.4%. In Fig. 2 , the data points are shown with semi -transparent markers around the mean values, separately for horizontal...
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Small singular values below a chosen threshold , equal to 10-3, were removed to improve numerical stability and reduce noise amplification. The final correction vector is given by: Δ𝐼𝐼=𝑉𝑉Σ−1𝑈𝑈𝑇𝑇Δ𝜈𝜈. (3) This expression was applied to the response matrix at each undulator gap and phase configurat...
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open -gap configuration is ν x = 0.245 and νy ≈ 0.14, which was used as the baseline for calculating relative tune variations reported in this study. The measurement was performed to validate the applied correction and to visualize the results with (Fig. 3) and without (Fig. 4) applied correction . The undulator...
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peak -to-peak measures. For this reason, standard deviation is not used as a stability metric in this analysis. In the horizontal plane, the mean tune shifts from 0.209 (before correction) to 0.2 19 (after correction). This corresponds to a reduction of the effective tune shift between operating states by 28%. I...
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correction could be improved by increasing the limits of magnets currents, but it leads to a significant reduction in beam lifetime, reaching up to approximately 2.3 hours. Solution is a compromise between long -lasting beam and good tune correction. Additionally, orbit stability was monitored during correction. ...
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