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Electrical Ground Support Equipment Overview

Electrical Ground Support Equipment Overview. Scott Williams Stanford University scott.williams@stanford.edu. EGSE Functions. EGSE Mission Provide common ground based operations infrastructure Support subsystem I&T including realtime software development Support T&DF development

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Electrical Ground Support Equipment Overview

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  1. Electrical Ground Support Equipment Overview Scott Williams Stanford University scott.williams@stanford.edu

  2. EGSE Functions • EGSE Mission • Provide common ground based operations infrastructure • Support subsystem I&T including realtime software development • Support T&DF development • Support requirements verification testing • Support LAT integration and test operations • Provide environment for prototyping IOC functions, procedures, and processes.

  3. EGSE Functions • Provide common infrastructure • Command and control, including test procedures • Telemetry acquisition, archive, and distribution • Health, status, and data quality monitoring • Support data visualization tools • Support subsystem engineering displays and EGSE • Support subsystem development • Trigger & dataflow system • Flight software environment, FSW Testbed • ACD, CAL, and TKR subsystems I&T • Support integration and test • Verification Testing • Qualification/Calibration Unit I&T • Subsystem receiving inspections • LAT I&T including environmental testing • Mission Systems Integration & Test

  4. Evolutionary EGSE Development

  5. EGSE Requirements Sources EGSE requirements are traceable to several sources • LAT Performance Specification LAT Trigger & Dataflow Specification • LAT Power System Specification • LAT Flight Software Performance Specification • LAT IOC Performance Specification • LAT Verification Plan • LAT Integration & Test Plan • Subsystem Integration & Test Plans • LAT IOC Verification Plan • SI-SC Interface Requirements Document, 433-IRD-0001 • GLAST Mission Assurance Requirements, 433-MAR-0001

  6. Electronics Organization NRL SU-HEPL SU-SLAC NRL SU-HEPL SU-SLAC NRL SU-HEPL SU-SLAC NRL SU-HEPL SU-SLAC NRL SU-SLAC NRL SU-HEPL SU-SLAC CEA-DAPNIA INFN SU-SLAC NRL

  7. EGSE WBS Organization

  8. EGSE Products • 4.1.7.A.2 EGSE • Realtime System and RTOS, application S/W • Network • Workstation/Software • Realtime S/W development environment • Test executive software • Data acqusition, archive, and distribution • Data visualization • 4.1.7.A.3 Spacecraft Interface Simulator • Realtime System and RTOS, application S/W • 4.1.7.A.4 Instrument Power Supply • Power supplies • Configuration control and monitoring

  9. Work Breakdown Structure

  10. Balloon, telemetry, disk read Single command console for flight Archive, dataHub Outbound internet access via firewall router Gse clients, private net Balloon Flight EGSE

  11. Electronics Development Cycles • EGSE must support electronics development • Engineering Model 1 (EM1) • Tower Electronics Module or ACD Electronics Module • Engineering Model 2 (EM2) • Complete T&DF electronics using commercial parts • Qualification • Thermal Vacuum • Vibration • EMI/EMC • Power • Flight • Fully qualified

  12. CAL TKR-CAL TEM TKR Event Processor Units T&DF Architecture Tower Front-End Event Data Distribution & GLT Assembly Control & Processed Event Data Control, HSK Data Interconnection Module Control, Trigger, Event & HSK Data Space-craft Interface Unit Front-End Monitoring Module Global Trigger Module Control & Processed Event Data ACD ACD EM to/from SC EM1 interface EM2/FST/QU/FU interface

  13. EM1 EGSE • Functions • Support development of Tower Electronics Module (TEM) • Support subsystem development, integration and test • Support initial flight software development • Support LAT integration and test of subsystems during LAT assembly • Concept Description • Custom TEM interface board • COTS cPCI chassis with PowerPC CPU and ethernet interface • EGSE Workstation (Linux or Solaris) dual home ethernet with VxWorks environment

  14. EM2 EGSE Functions • Support development of Trigger and Dataflow System • Support Flight Software Testbed • Support Qual/Cal Unit I&T • Support Flight LAT I&T Concept Description • Spacecraft Interface Simulator with COTS cPCI chassis, PowerPC CPU, ethernet interface, MIL-STD-1553 interface, Serial data interface, Analog and Discrete I/O • EGSE Workstation (Linux or Solaris) dual home ethernet with VxWorks environment • Instrument Power Supply under computer control • Ethernet Router/Firewall

  15. EGSE Functions

  16. Subsystem Support • EGSE Support - 4.1.7.A • EGSE systems for integration and test • Common command/configuration environment - TBD • Common data visualization and analysis tools - e.g. ROOT • Realtime s/w development environment - e.g. Tornado • Other Hardware Support - 4.1.7.4/5/6 • Hardware simulators • Memory based front end detector simulators • Provide subsystems with firmware support. • Flight software group is committed to providing subsystem test support for the detector development - 4.1.7.7 • The emphasis is on RTOS support • Provide low-level utilities to access the hardware. • Provide a framework to construct a test environment. • FSG does not write acceptance test code.

  17. EGSE Deliverables Total Systems • Engineering Model 1 - 10 • Engineering Model 2/Qual Unit/Flight Unit - 4

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