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MOPOS Measurements REPORT SVN 183 / 185

C. Deplano, J.J. Savioz, A. Topaloudis. MOPOS Measurements REPORT SVN 183 / 185. Outline. Setup FIFO Capture Injection Trajectory Orbit Diagnostic Global Orbit Continuous Filter For each one: Software menu Measurement & behavior BST and IRQ Conclusion. Setup – MOPOS Lab.

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MOPOS Measurements REPORT SVN 183 / 185

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  1. C. Deplano, J.J. Savioz, A. Topaloudis MOPOS Measurements REPORT SVN 183 / 185

  2. Outline • Setup • FIFO • Capture • Injection Trajectory • Orbit Diagnostic • Global Orbit • Continuous Filter • For each one: • Software menu • Measurement & behavior • BST and IRQ • Conclusion Caterina Deplano

  3. Setup – MOPOS Lab • 1 VME crate cfv-866-bidev1 (32-bit) • 1 VFC v2 board + 1 FMC board • 1 Front-End Board (first prototype – last year) equipped with a LogAmp Board on the H plane • Front End Frame: data from a single batch, 64 bunches each (LogAmp Calibrator – Horizontal Plane) • All acquisition done via the VME/WB trigger register • Where not differently specified: SVN version 183 • Timing constrains MET • SVN 183  BST block NOT CONNECTED  ONLY INTERNAL VFC CLOCK • SVN 185  BST block CONNECTED Caterina Deplano

  4. Setup – MOPOS Lab Ch2 • FMC TOP • CH1 connected to the Front-End Front-End Frame  CH2 not connected VFC Internal Frame Ch1 BST Caterina Deplano

  5. Setup – MOPOS Lab • The measurement can be done with 2 different frames: • Front-End Frame • Operational • Frame from the Front-end board connected to the optical fiber • Internal Frame • Debug • Internally generated on the VFC Application FPGA • Same length • ADC data are different • The internal frame has only one Long Word which change • turn clock counter • Software: • FPGAs Configuration via software on CPU • Data analysis with python routines on cs-ccr-dev3 Caterina Deplano

  6. LogAmp Calibration via Serial Link Caterina Deplano

  7. LogAmp Calibration via Serial Link • Log-Amp calibration  maximum positive displacement  1 batch of 64 bunches Caterina Deplano

  8. Parallel Modes • Possibility to test each mode individually or ALL modes in parallel • FIFO and Filter are asynchronous MODEs Caterina Deplano

  9. FIFO MODE • Debug Mode  Complete Frameavailableoff-line (All Data) Caterina Deplano

  10. FIFO MODE – Front End Frame • Log-Amp calibration  maximum positive displacement Bin: ADC SLOT (100 ns ) Caterina Deplano

  11. FIFO MODE – Internal Frame Caterina Deplano

  12. CAPTURE MODE • Raw ADC Data available off-line • Debug Mode  Data related to one plane only (H or V) • 1 Intensity Signal: SUM • 3 Position Signals: 40MHz H – 40 MHz L – 200 MHz • Operational Mode  Data related to plane H and plane V • 1 Intensity Signal: SUM • 1 Position Signal: Selected Position between the 40MHz H – 40 MHz L – 200 MHz • 1 Intensity Signal: SUM • 1 Position Signal: Selected Position between the 40MHz H – 40 MHz L – 200 MHz H V Caterina Deplano

  13. CAPTURE MODE Caterina Deplano

  14. CAPTURE (Debug Mode) Caterina Deplano

  15. CAPTURE (Debug Mode) Delta signals selected if Sum > validity 40M H if SUM < sensitivity Caterina Deplano

  16. CAPTURE (Operational Mode) Delta signals selected if Sum > validity (10000 Adc bin) 40M H if SUM < sensitivity (12000 Adc bin) Caterina Deplano

  17. CAPTURE (Operational Mode) 40M L 40M H 40M H Caterina Deplano

  18. CAPTURE (Operational Mode) 40M L 40M H 40M H Off-line analysis: ▼  mean position calculated ●  x-coordinate to select the points to calculate the mean position Caterina Deplano

  19. CAPTURE (Operational Mode) Caterina Deplano

  20. Trajectory MODE • Triggered at Injection  Mean Position Value / Batch • Up to 13 batches can be selected Caterina Deplano

  21. Trajectory (Debug Mode) slots 16 ÷ 28 slots 11 ÷ 15 slots 1÷ 10 slots 29÷ 40 slots 41÷ 50 Caterina Deplano

  22. Trajectory (Debug Mode) Caterina Deplano

  23. Trajectory (Debug Mode) • RANDOM BUG: sometime one or more batches show a 0 value • The other turns are fine • Independent from the batch definition Caterina Deplano

  24. Trajectory (Operational Mode) Caterina Deplano

  25. Trajectory (Operational Mode) Validity = 12000 Sensitivity = 12000 Delta H = Delta 200 Caterina Deplano

  26. Orbit Diagnostic MODE • Mean Position Value / ADC Slot • Can be used to define the slots selection for the Global Orbit Mode Caterina Deplano

  27. Orbit Diagnostic MODE Delta H = Delta 40 L Validity = 0 Sensitivity = 0 Validity = 10000 Sensitivity = 12000 Delta H = Mix between Delta 40 L and H Related to Sensitivity Systematic BUG solved  First tour used to reset previous DAQ Caterina Deplano

  28. Orbit Diagnostic MODE Caterina Deplano

  29. Orbit Diagnostic VS Capture Validity = 10000 Sensitivity = 12000 Capture  1 Turn Orbit Diagnostic  254 Turns Caterina Deplano

  30. Global Orbit MODE • Mean Position Value / Turns  Currently one value every t turn • The slots to be considered in the mean calculation can be masked  To be changed? One mean value for each batch (up to 13) ?????? Caterina Deplano

  31. Global Orbit MODE Validity = 0 Sensitivity = 0 Ask for slots 1-50 Delta 40 L Ask for slots 1-235 Systematic BUG solved  reset of enable signals Delta 40 L Caterina Deplano

  32. Global Orbit MODE Validity = 10000 Sensitivity = 12000 Ask for slots 1-235 Delta 40 H or Delta 40 L Ask for slots 20-25 Delta 40 L Caterina Deplano

  33. Filter MODE • Same information as the Global Orbit mode BUT • The slots cannot be masked individually • It is a Continuous Filter (Infinite Impulse Response) • Must be reset before each new cycle Caterina Deplano

  34. Filter MODE since svn 176 • To be done: • τ is constant = 24 • Implement the programmable time constant To be done: More measurements to verify the variance Caterina Deplano

  35. IRQ – BST Test ongoing • BST triggers  OK (tested with the UTC clock from the BST Master) • To be tested: the correct BST Master Hardware Register and the Pre-pulse Signal • Single Interruption • DAQ IRQ ok if the VME asynchronous trigger is used • DAQ IRQ okif the BST synchronous trigger is used (Capture Mode) • Injection Trajectory, Global Orbit and Orbit Diagnostic: change the software procedure • Multiple Interruptions  TO BE TESTED • Test successive Interruption: • Global Orbit: 1 DAQ IRQ every 10 orbits (FIFO almost full) and 16 orbits (FIFO full) Caterina Deplano

  36. IRQ – BST BST Master Frame - SPS  TO BE DONE • Test the Pre-pulse signal • Ejection-signal ? • Fix the hardware bit for each DAQ Mode (one for each DAQ mode is needed?) • Fix the trigger rate of each DAQ MODE: • Global Orbit  IRQ @ 100 Hz (10 orbits acquired at the IRQ) • Orbit Diagnostic  100 Hz ? • Injection Trajectory  Pre-pulse – single DAQ IRQ • Capture  on request – single DAQ IRQ • Provide software procedure to use the pre-pulse to trigger the Capture and the Trajectory modes together • Filter + General BST Information  1kHz? 100 Hz? • Provide the software procedure Caterina Deplano

  37. Conclusion Random bugs • Injection Trajectory: one or more batches get a 0 value for one tour (while before/after are good); it is independent from the batch number and from the batch definition (number of slots) and from the front-end or internal frame • Turn Clock lost on the Front-End Board after few/some hours. Problem in the connection between the FE board and the AFPGA (??).  needed to restart the optical link • Turn Clock on Application FPGA from SVN 185: • Double turn generation  asecond pulse is generated 50 ns after the first • Sometimes it is needed to restart the optical link several times to take the link synchronization Caterina Deplano

  38. Conclusion Still to be tested • Interruptions and BST • Do all the measurement with the FE frame for the FMC ch2 Improvements • Filter: use the programmable time constant set by VME • Global Orbit  Single Batch Selection (currently done) or Orbit per Batch Selection (to be done) ? Remarks • Timing constraints MET • The Front-End frame and the internal frame show the same behavior for all the acquisition modes. Caterina Deplano

  39. Caterina Deplano

  40. FIFO MODE – Internal Frame • BUG (Timing Constraint Met): SOLVED ?! • Svn 176: Plane V for FMC TOP channel bottom (ch2) shows an internal frame always wrong. • Snv 177: Correct; both planes, both FMC channel  not tested FE frame on FMC ch2 • Snv 182: FMC ch1 Correct; FMC ch2  V/H plane wrong • SVN 183 and 185 OK  internal data frame resynchronized (same frequency but random phase) Caterina Deplano

  41. BST Master Frame – new bits/tasks ? Caterina Deplano

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