1 / 15

IDPU FSW Critical Design Review F. Harvey University of California - Berkeley

IDPU FSW Critical Design Review F. Harvey University of California - Berkeley. Overview. Flight Software Overview Documentation Development Process Requirements Design, Modules Resource Summary Schedule Issues. Documentation. Stored on ftp://apollo.berkeley.edu/pub/Themis:

naasir
Télécharger la présentation

IDPU FSW Critical Design Review F. Harvey University of California - Berkeley

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. IDPU FSW • Critical Design Review • F. Harvey • University of California - Berkeley

  2. Overview • Flight Software Overview • Documentation • Development Process • Requirements • Design, Modules • Resource Summary • Schedule • Issues

  3. Documentation Stored on ftp://apollo.berkeley.edu/pub/Themis: ftp://apollo.berkeley.edu/pub/Themis/Systems/Requirements ftp://apollo.berkeley.edu/pub/Themis/Systems/ICDs ftp://apollo.berkeley.edu/pub/Themis/Instruments/IDPU/FSW/Docs THM_FSW_001D_SRS (Software Requirements Specification) THM_FSW_003_CTM (Command and Telemetry)

  4. Documentation • FSW Primary Documentation FSW Technical Notes

  5. Documentation • FSW Reference Documentation

  6. Development Process • Heritage tools • Assembler, Linker, utilities from earlier satellite efforts • Some specific DCB tests use C tools and debug equipment from Stereo. • Centralized storage • apollo.berkeley.edu/pub/THEMIS/Instruments/FSW/Code • apollo.berkeley.edu/pub/THEMIS/Instruments/FSW/Docs • Reviews • Completed Software Reqs Specification Review 4/1/04 • David King principal reviewer. Dorothy Gordon and investigators, as required.

  7. Development Process • Primary Development Platforms (2) • DCBs 1 & 3(Data Controller Board), follow flight revisions • GSE Interface Board, as BAU Simulator (clocks, commands, HST) • GSE Interface Board, as test pattern generator • Rom Emulator (Tech-Tools ER3) • Toolset 1: C compiler and Rom Monitor program • Toolset 2: Heritage tools for assembly language • GSE PC & s/w for high speed data collection • 1 in Boston (h/w support), 1 in Berkeley (s/w development) • Test Platforms (2) • DCBs 2 & 4 • GSE Interface Board as BAU Simulator • ETU under test (BEB, DAP…) • GSE PC for high speed data collection • One of these becomes the IDPU Simulator for Swales

  8. Deliverables • Deliverables • IDPU Simulator • Phase 1, or better, FSW • Needed at Swales to match with BAU EDU (Summer 2004) • Phase I – Board level • April-May 2004 • Phase II – Box Level • Data acquisition, SSR • PROM image, final. • Summer 2004 • Phase III – instrument level • Control external parts • Boom deployment • ESA covers, SST attenuator • June (as tests allow) • Phase IV – science optimization • Triggers, science modes • Compression • October

  9. Requirements • Changes since PDR • IDPU Simulator (s/w) • When boards turned off, set enables such that _CLK lines are near ground. • For DFB (filter) channels with packet switch rates > 16 seconds, FSW to ‘arm’ the DMA channel before the switch point. • 2 virtual channels (not 1). • 4th mode, Low Power (vs Safe) • No longer need termination modes for ETC DMA channels. • FGPA version #

  10. Data Collection • Data Collection • DMA Channel Controller Assigned to Each Data Source • FSW Hands Packet Addresses to Each DMA Channel Controller • Double-Buffered DMA Address to Eliminate Gaps • DMA Channels Are Sync’d to either Time or Spin-Phase • FSW Initializes Each DMA Channel for type of Synchronization • FSW writes Headers for Each Packet as it is Produced • NEW: FSW ‘arms’ very slow channels to change buffer addresses. • Data Collection Rates • Peak Input Rate of 430 KB • Preferred Length just under 4 KB for raw data packets • Peak Packet Rate of 157 Packets/sec • Performance Calculation: ~300 cycles/header, ~2.4% CPU • NEW: Basic h/w s/w interface tested in March.

  11. Data Compression • Data Compression • Multiple Algorithms Available (ref. thm_fsw_901_Compression) • Huffman4 • Delta Modulation • Combined Delta Mod/Huffman • Run Length not effective on this data • Numerous Studies of Compression Algorithm Performance • Used Cluster Flight Data • Similar Instrumentation, Expected Signal Levels • Similar Data Volumes • Achieved appx 1.5 compression without being Adaptive • Needed Adaptive Behavior to Get to 1.8+ or more • Performance Studies of Non Adaptive Compressors • Huffman4x2 Algorithm 21 KB/sec • Delta Modulation Algorithm 11-14 KB/sec • Entire Memory Compressed in 1-2 hours

  12. Science Telemetry • Science Telemetry • Packets Selected are Handed to DCB High Speed TLM DMA • Address of the 4K Block and Length in Bytes • FSW receives Interrupt when the Address Pointers Swap • FSW has 1 Packet Time to refresh DMA Address Pointer • Packet Rate Determined by Packet Length • If Packets are 2-4KB in length, then at 2Mbps transfer rate, FSW outputs ~50 to 100 packets per sec. • If Packets are Compressed, then FSW may find very short packets. • Packet Mixing • VC2 for quicklook data, VC3 for stored data.

  13. Triggers • Trigger Calculations Using In Situ Data • FSW Continuously Samples Science Data in SSR (e.g. ESA/SST Peak Flux, DFB V1-V6 Voltages, FGM Bx-Bz) • Evaluates Data Quality at 8 Hz • Calculates Quality using 8 Selectable Functions • Result Values 0-255 • Specific Functions are TBD (Phase IV) • Conjunction Prioritization • FOT will uplink Predicted Conjunction Times • FSW increases Quality Value near Conjunction • FSW decreases Quality Value near downlink • Conjunction Duration and Bias are Commandable

  14. Resources • PROM/EEPROM • PROM Functions • EEPROM Load • Uplink Support • L&EO Functions • EEPROM/Uplink • One-Time Events • Test Programs • Initialization Params • Science Upgrades • RESOURCE USAGE • 72% PROM • 33% RAM • 50% EEPROM • 36.5% CPU

  15. Schedule FSW ETU Schedule FSW ETU Phase I Board Lvl Development 4/9/04 FSW ETU Phase I Test 5/11/04 FSW ETU Phase II Box Lvl Development 6/8/04 FSW ETU Phase II Test 6/15/04 FSW ETU Phase III Inst Lvl Development 6/22/04 FSW ETU Phase III Verification w Sims 7/6/04 FSW FLT PROM FINAL 7/6/04 FSW FLIGHT Schedule FSW FLT SPEC MODS FSW FLT Development/Test FSW FLT Phase IV Science Development FSW FLT Phase IV Test 10/12/04

More Related