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Balloon Flight Planning

Balloon Flight Planning. Roger Williamson June 8, 2000. SCOPE. DAQ subsystem Detector Interfaces Balloon Command, Data, and Electrical Instrument Power Supplies Onboard Software Ground Support Equipment. Requirements.

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Balloon Flight Planning

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  1. Balloon Flight Planning Roger Williamson June 8, 2000

  2. SCOPE • DAQ subsystem • Detector Interfaces • Balloon Command, Data, and Electrical • Instrument Power Supplies • Onboard Software • Ground Support Equipment

  3. Requirements • There is a Balloon Flight Objectives document in preparation that will serve as a source document. • Derived Requirements • L1T Trigger at the environmental rate • Event deadtime of less than 100 microsec • Save data from all events • Send subsample of events to ground realtime

  4. Assumptions • Balloon flight 1st week of Sept, 2001 • Use modified BTEM tower • Downlink not sufficient for full bandwidth data • Power from +28V batteries • Command uplink and primary +28 V power supplied by gondola

  5. Overview • Onboard data storage requirement • 1 kHz L1T average rate • 1 kbyte/event(TBR) average event • 10 hour total record time • 1e3*1e3*36e3 = 36 Gbytes (need more) • CPU processing load risk mitigation • FIFO buffers permit full rate bursts if CPU readout/processing cannot keep up • TKR FIFO ~ 200 events 200 ms burst

  6. Existing Hardware • Tracker Interface • No modification required • Calorimeter Interface • No change to readout interface • Dead time hold off input to L1T --- or --- • Use 100 microsecond hold off timer in CAL readout FPGA • ACD Interface • No modification required • Front end noise fix required - Modification • HSK readout software - Modification • Additional joint testing

  7. Existing Hardware • Global Level 1 Trigger • OR FPGA in ACD TEM • Requires added functionality for balloon flight • Dead time hold off - New • Global live time counter - New • Global L1T counter reset scheme - New • Possibly other science requirements for trigger logic

  8. Existing Hardware • GPS Receiver • Battery powered • Provide RS-232 Interface • Revise Software to include timestamp and position • IDB --- Ethernet CISCO switch • Cable Harness • L1T cables • Ethernet IDB cables

  9. Existing Hardware • SIU TEM • GPS sync with L1TCNT • Ethernet to BIU for command and downlink TM • Fiberoptic link via CISCO switch for GSE

  10. New Hardware • Merge Detector TEMS into 1 VME chassis • Use 21 slot VME chassis • One Master CPU for data acquisition and control • VME backplane BLT to speed up data acquisition to higher L1T rate • Omit Ethernet packet building for most data packets • Send 1(TBD) event per second to downlink (depends on bandwidth and event size) • Accepts change to modified data flow hardware on daughter card or VME • Add HSK and LRS (rate counter) readouts • Add Onboard Storage using VME chassis

  11. New Hardware • Balloon Interface Unit (BIU) simulates SC • TEM type VME Chassis • Ethernet to TEM (instead of 1553B) • New interface to balloon system for commands • BIU provides downlink telemetry subsystem • Provided by NRL with downlink telemetry system

  12. New Hardware • Power switching/control • Controls power to each TEM from +28VDC • Balloon Discrete Commands • 21 Slot VME chassis • Power Supplies • 110VAC changed to +28VDC • Detector power supplies mounted and controlled via VME boards • On/off control via commands • Detector bias voltage setting via commands • Monitor currents and voltages, in/out

  13. New Hardware • Packaging • Cable Harness – Existing + New • Mechanical - New

  14. Housekeeping • Temperature monitors • ACD - 16 (TBR) places • CAL - 16 (TBR) places • TKR (Existing) 16 places • BIU – 16 (TBR) places • Power Supply Voltages - 14 (TBR) places • Power Supply Currents - 14 (TBR) places • Strain gauges (TBR)

  15. Ground Support Equipment • Record and display variable length packets • Displays – • Existing event real-time display • Housekeeping monitors • Status and software monitors • Additional histograms • Science displays • Command web page - Modified • Balloon interface simulator - • +28 V power • Command • Data • Ethernet fiber optic link to CISCO switch

  16. Software • Post Beam Test Cleanroom Software • Ran at rates above 1 kHz for FIFO readouts with direct read from FIFO • Detector control and test suites from Beam Test (TBR) • Modify for BLT readout of FIFOs to provide higher speeds and more CPU margin for other tasks • Variable length event packets

  17. Options • Hardware Data Transfer (to 128 Mbyte DRAM) • New data push technique to move event data to DRAM • CAL Zero Suppression • FPGA hardware version • TKR FPGA Zero Suppression • Hardware suppression of no-hit headers • TKR Rate Counters • TREQ rates for each layer (TBR) • Poisson Rate Generator for L1T (commandable rate)

  18. Schedule (June 2001 Flight) • July, 2000 Balloon Flight Requirements Review • July, 2000 ACD Testing at GSFC • July, 2000 PDR Hardware & Software • July, 2000 TKR TEM at Stanford, 2 weeks test/devel • Sept, 2000 CDR • Oct, 2000 Power System Fab, pkg, HSK,... • Oct, 2000 GSE Release 1 • Oct, 2000 All TEMS at Stanford for software development • Nov, 2000 ACD I/F Test at GSFC • Dec, 2000 TKR I/F Test at UCSC • Jan, 2000 CAL I/F Test at NRL • Mar, 2001 Gondola I/F Test • Mar, 2001 GSE Release 2 • Apr 1-15, 2001 Hardware Integration at SLAC • Apr 16-May 16, 2001 4 weeks Software Integration at SLAC • May 17 Ship to GSFC • May 19 2 week Gondola Integration at GSFC • June 1 4 week software test at GSFC • Aug 1 Ship to launch site

  19. ISSUES • L1T maximum trigger rate • MC data simulation • Data Flow Requirement • Onboard Storage • Trigger design • Downlink bandwidth • Schedule & staffing • Plan for modified data flow and trigger system

  20. ISSUES • ACD HSK readout debug • ACD noise • Power supply plan • Onboard software plan

  21. WBS

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