1 / 27

The AGILE Instrument functional performance

The AGILE Instrument functional performance. A. Argan, A. Trois (on behalf of the AGILE Team). SUMMARY. Introduction Overview on the on-board scientific data acquisition Overview on the in-flight functional performance Conclusions. The most compact and low-power Instrument

ely
Télécharger la présentation

The AGILE Instrument functional performance

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript


  1. The AGILE Instrument functional performance A. Argan, A. Trois (on behalf of the AGILE Team) 5th Science AGILE Workshop  – ESRIN, Frascati, 12-13 June 2008

  2. SUMMARY • Introduction • Overview on the on-board scientific data acquisition • Overview on the in-flight functional performance • Conclusions 5th Science AGILE Workshop  – ESRIN, Frascati, 12-13 June 2008

  3. The most compact and low-power Instrument ever developed in High Energy Astrophysics. INTRODUCTION - GLOBAL VIEW • Detector volume: ~ 0.25 m3 • Detector mass: ~ 120 kg • Detector power consumption: ~ 60 W • Complex data acquisition system: • 36.864 Silicon Tracker (gamma-ray imager) channels • 6.144 Super-Agile (hard X-ray imager) channels • 60 Mini-Calorimeter channels • 15 AC channels • 27 FPGA’s • 1 DSP 5th Science AGILE Workshop  – ESRIN, Frascati, 12-13 June 2008

  4. OVERVIEW ON THE ON-BOARD DAQ (I) 5th Science AGILE Workshop  – ESRIN, Frascati, 12-13 June 2008

  5. THE ON-BOARD DAQ (II): GRID 20 independent trigger algorithms 5th Science AGILE Workshop  – ESRIN, Frascati, 12-13 June 2008

  6. SA DATA HANDLING THE ON-BOARD DAQ (III): GRB SEARCH MCAL BURST CYCLIC BUFFER MCAL T BURST E BUS L RATEMETERS E BURST SEARCH ON TIMESCALES 64ms-8s M BURST SEARCH E RATEMETERS ON TIMESCALES <1ms-16ms T R Y FAST LINK IMAGES DECONVOLUTION AND BURST COORDINATESDETERMINATION SA IMAGING IMAGES INTEGRATION HARDWARE SOFTWARE Burst Search on 8+9 channels (SA + MCAL) Burst Search timescales from <1ms to 8s On-board Burst coordinates determination (error ~20 arcmin) 5th Science AGILE Workshop  – ESRIN, Frascati, 12-13 June 2008

  7. OVERVIEW ON THE ON-BOARD DAQ TELECOMMANDS • AC FEE configuration: • 1 TC33S5: AC Obs. configuration (RAM/EEPROM) • 1 TC33S6: AC El. Cal. configuration (RAM/EEPROM) • ST FEE configuration: • 1 TC33S7: ST General Obs. configuration (RAM/EEPROM) • 96 TC33S8: ST Regin configuration (RAM/EEPROM) • 1 TC33S9: ST El. Cal. configuration (RAM/EEPROM) • SA FEE configuration: • 1 TC33S10: SA General Obs. configuration (RAM/EEPROM) • 48 TC33S11: SA Obs. Regin configuration (RAM/EEPROM) • 48 TC33S11: SA Cal. Regin configuration (RAM) • 4 TC33S12: SA El. Cal. configuration (RAM/EEPROM) • MCAL FEE configuration: • 1 TC33S13: MCAL Obs. configuration (RAM/EEPROM) • 1 TC33S14: MCAL El. Cal. configuration (RAM/EEPROM) 5th Science AGILE Workshop  – ESRIN, Frascati, 12-13 June 2008

  8. OVERVIEW ON THE ON-BOARD DAQ TELECOMMANDS • PDHU – GRID logic configuration: • 1 TC33S2: GRID HW configuration (RAM/EEPROM) • 1 TC33S3: GRID SW step-1 configuration (RAM/EEPROM) • 1 TC33S4: GRID SW step-2 configuration (RAM/EEPROM) • 1 TC33S37: GRID SW step-3 configuration (RAM/EEPROM) • PDHU - BURST logic configuration: • 1 TC33S15: Burst Search general configuration (RAM/EEPROM) • 1 TC33S16: Burst Search HW configuration (RAM/EEPROM) • 4 TC33S17: SA Burst Search SW configuration (RAM/EEPROM) • 4 TC33S19: MCAL Burst Search SW configuration (RAM/EEPROM) • 1 TC33S18: SA Imaging configuration (RAM/EEPROM) • PDHU - General scientific configuration (managed by LTP during the Routine phase): • 1 TC33S1: Scientific general configuration (RAM/EEPROM) • 1 TC33S20: Telemetry Partition Table configuration (RAM/EEPROM) 5th Science AGILE Workshop  – ESRIN, Frascati, 12-13 June 2008

  9. OVERVIEW ON THE ON-BOARD DAQ LOOK-UP TABLES • PDHU – GRID logic configuration: • ¾ Trigger: 4 LUTs Obs. + 2 LUTs Cal. • AC Veto: 4 LUTs Obs. + 1 LUT Cal. • R-Trigger: 4x8 LUTs Obs. + 2 LUTs Cal. • 1.5 Trigger: 4 LUTs • CDIS Trigger: 4 LUTs • ST Offsets: 1 LUT • FVC1: 1 LUT • FVC2: 1 LUT • Kalman Filter: 7 LUTs • PDHU – SA Photon-by-Photon configuration: • Address Corr.: 4 LUTs • PDHU - BURST logic configuration: • SA Burst Trigger: 4x4 LUTs • SA Imaging Trig.: 4 LUTs • MCAL Burst Trig.: 4x4 LUTs • MCAL BBFP: 4x4 LUTs • SA Burst Imag.: 7 LUTs 5th Science AGILE Workshop  – ESRIN, Frascati, 12-13 June 2008

  10. OVERVIEW ON THE ON-BOARD DAQ A complete AGILE scientific configuration is composed of: • 220 TCs (~100000 parameters) 126 LUTs 5th Science AGILE Workshop  – ESRIN, Frascati, 12-13 June 2008

  11. THE AGILE ON-GROUND TESTING (I) 5th Science AGILE Workshop  – ESRIN, Frascati, 12-13 June 2008

  12. THE AGILE INTEGRATION AND QUALIFICATION 5th Science AGILE Workshop  – ESRIN, Frascati, 12-13 June 2008

  13. THE AGILE LAUNCH CAMPAIGN (I) AGILE integrated in the PSLV-C8 April 15, 2007 5th Science AGILE Workshop  – ESRIN, Frascati, 12-13 June 2008

  14. THE AGILE LAUNCH CAMPAIGN (II) Fotoni a terra e in volo - I Last gamma-ray detected in India by the AGILE-GRID on top of PSLV-C8 5th Science AGILE Workshop  – ESRIN, Frascati, 12-13 June 2008

  15. THE AGILE LAUNCH The AGILE satellite was successfully launched by the Indian rocket PSLV-C8 on April 23, 2007. 5th Science AGILE Workshop  – ESRIN, Frascati, 12-13 June 2008

  16. OVERVIEW ON THE IN-ORBIT PERFORMANCE 5th Science AGILE Workshop  – ESRIN, Frascati, 12-13 June 2008

  17. SILICON TRACKER FEE CONFIGURATION • Energy Threshold (dig. value=5) => ~95% detection efficiency • - 792 strips disabled (~ 2% total strips) 5th Science AGILE Workshop  – ESRIN, Frascati, 12-13 June 2008

  18. GRID FUNCTIONAL PERFORMANCE (I) Fotoni a terra e in volo - II First gamma-ray detected in orbit with the nominal GRID trigger configuration (May 10, 2007) 5th Science AGILE Workshop  – ESRIN, Frascati, 12-13 June 2008

  19. GRID FUNCTIONAL PERFORMANCE (II) 5th Science AGILE Workshop  – ESRIN, Frascati, 12-13 June 2008

  20. The GRID Trigger background rejection GRID FUNCTIONAL PERFORMANCE (III) Pre-trigger rate Level-1 output rate Level-1.5 output rate Level-2 output rate 5th Science AGILE Workshop  – ESRIN, Frascati, 12-13 June 2008

  21. GRID FUNCTIONAL PERFORMANCE (IV) TM GRID event rate: < 7Hz Max. sustainable (and measured) TM GRID event rate: 30 Hz. 5th Science AGILE Workshop  – ESRIN, Frascati, 12-13 June 2008

  22. SUPER-AGILE FEE CONFIGURATION • Energy Threshold = 18keV • 718 strips disabled (~ 12% total strips) 5th Science AGILE Workshop  – ESRIN, Frascati, 12-13 June 2008

  23. - Energy Upper threshold (>100 keV) cuts ~250 cts/s. - AC Top and Lat cuts ~100 cts/s (~5% deadtime). SUPER-AGILE FUNCTIONAL PERFORMANCE (I) by SA Team – IASF-INAF Roma 5th Science AGILE Workshop  – ESRIN, Frascati, 12-13 June 2008

  24. SUPER-AGILE FUNCTIONAL PERFORMANCE (II) TM SA event rate (with SA max temperature ≤ 26°C): < 100Hz by SA Team – IASF-INAF Roma 5th Science AGILE Workshop  – ESRIN, Frascati, 12-13 June 2008

  25. MCAL_BURST P109="Observation" P110="0" P111="0" P112="0" P113="0" P114="3" P115="3" P116="3" P117="3" P140="StandBy at PDHU Level" P171="Keep Nominal Config" P202="Keep Nominal Config" P233="StandBy at PDHU Level" SA P127="Separate SAIE Setup" P128="Observation" P129="Observation" P130="0" P158="Keep Nominal Config" P159="Keep Nominal Config" P160="Keep Nominal Config" P189="Keep Nominal Config" P190="Keep Nominal Config" P191="Keep Nominal Config" P220="Keep Nominal Config" P221="Keep Nominal Config" P222="Keep Nominal Config" P251="Keep Actual Config" P252="StandBy at FEE Level" P253="StandBy at FEE Level" SA_BURST P119="Observation" P120="2" P121="2" P122="2" P123="2" P125="1" P150="StandBy" P181="Keep Nominal Config" P212="Keep Nominal Config" P243="StandBy" AC_FEE P108="Observation" P139="Keep Nominal Config" P170="Keep Nominal Config" P201="Keep Nominal Config" P232="Keep Actual Config" GRID P100="Observation" P101="0" P102="0" P103="0" P104="0" P105="0" P106="0" P107="0" P131="StandBy at PDHU Level" P162="Keep Normal Config" P193="Keep Normal Config" P224="StandBy at PDHU Level" LTP SCIENTIFIC CONFIGURATION 5th Science AGILE Workshop  – ESRIN, Frascati, 12-13 June 2008

  26. Total telemetry per orbit (MB) Orbit TELEMETRY BUDGET 5th Science AGILE Workshop  – ESRIN, Frascati, 12-13 June 2008

  27. CONCLUSIONS - The Commissioning phase has been carried out with excellent results. - The PL subsystems are in general working in a satisfactory and nominal way. In several cases, during the first year, we could improve the pre-launch performance. - During the second year, we plan to further optimize the g-rays, x-rays and MCAL functional performance. 5th Science AGILE Workshop  – ESRIN, Frascati, 12-13 June 2008

More Related