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NTTS Concept Design Review Presentation

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Title: NTTS Concept Design Review Presentation


1
EGSE and Mission Control System Space-system
Simulator for EMCS Testing (SSET)
K. G. Skaug and P. van Duijn, Satellite Services
B.V.S. Valera and A. Voordijk,
ESA/ESTECPresentation given at EGOS, June 16th
2004, ESOC/Darmstadt
2
Presentation Overview
  • Background
  • Key Requirements
  • Configurations
  • Implementation Characteristics
  • Example Interactions
  • Phase-2 Development Plan
  • Other Applications
  • Conclusion

3
Background
  • The Space-system Simulator for EMCS Testing
    (SSET) was conceived by ESA/ESTEC in response to
    the complex challenge of testing the SCOS2K-based
    EMCS system. The scope of testing includes
  • Software upgrades of the EMCS itself (regression
    tests)
  • Validation of mission specific database
    preparations
  • Partial simulations of space system with hardware
    in the loop
  • The SSET is configured with the same SCOS
    database information as used by the EMCS itself.
    This achieves several objectives
  • Efficient Simulation set-up (no duplication of
    test data input work).
  • Test Configuration skew is counteracted (same
    data on both sides).
  • Independent validation of the mission database
    information
  • Compliance with the MDD specification
  • Internal coherence / consistency
  • The system observes and enforces compliance with
    the ECSS Packet Utilisation Standard
    (ECSS-E70-41A)

4
SSET Key Requirements (1/2)
  • Simulate multiple Space segment (satellites,
    onboard units) and/or Ground segment (SCOE)
    subsystems
  • Configured by the mission database files,
    including e.g.
  • TMPH table TM packet header structure
  • RPT table Reports (TM Packets) to be simulated.
  • PAR table Raw parameter definitions
  • PLF table Parameter fixed-position instances
  • TCPH table TC packet header structure
  • Thorough checking of database information for
    validity, consistency, PUS compliance etc.
  • Simulate and distribute periodic and single-shot
    reports (TM packets) with parameter contents
  • Simulate the on-board time and emission of Time
    packet

5
SSET Key Requirements (2/2)
  • Allow remote control of parameter values
  • All PUS parameter types to be supported
  • Respond to simulated requests (TC packets)
    according to PUS Service 1 specification
  • Acknowledge Acceptance, Start, Progress (xN),
    Completion
  • Customisation of Service 1 behaviour on a
    per-APID basis
  • Decoding of TC data with feedback to EMCS
  • On-demand corruption of TM packets
  • Controllable using PUS TC packets and/or EGSE
    level messages.
  • Communicates with the EMCS via ESAs EGSErouter
    protocol.

6
SSET Configurations (1/3)
  • Nominal EMCS Configuration S/C and SCOE Simulated

7
SSET Configurations (2/3)
  • Space Configuration All Interactions via TM/TC
    FE
  • In this configuration, SSET Controller acts as
    an on-board application
  • and is controlled purely by TC packets.

8
SSET Configurations (3/3)
  • Mixed Configuration Controller is a SCOE, S/C
    via FE

9
Implementation Characteristics
  • Runs on Windows NT/2000/XP Platform
  • Based on SSBVs proven SpaceLinkNGT software
    libraries for TM/TC processing, network
    interfacing, and GUI components.
  • User friendly GUI with simple controls and
    extensive offering of simulation status
    information.
  • System Log and binary data archive for test
    session tracing
  • Flexible external interfaces through SSET API

10
SSET User Interface
11
Example Interactions (1/4)
  • Generation and Distribution of Onboard Telemetry

12
Example Interactions (2/4)
  • Default Service 1 response interaction

13
Example Interactions (3/4)
  • User-configurable Service 1 response interaction

14
Example Interactions (4/4)
  • Parameter Get/Set Transactions

15
Other Applications (1/2)
  • Driver for Spacecraft Simulator in verification
    of ground station infrastructure

16
Other Applications (2/2)
  • RT Simulator Driver in CDMU/OBDH SCOE

17
Phase 2 Planned Developments
  • The following features are foreseen for the next
    phase of SSET development
  • Dynamic parameter simulation (periodic
    variations)
  • Out-of-Limit range detection / forcing
  • Interfacing with TM/TC FE hardware (currently
    software-only)
  • Enhanced support for SCOE simulation
  • Support for constellations (multiple distinct
    S/C)
  • Expanding packet responding model beyond Service
    1

18
Conclusion
  • SSET designed for EMCS testing
  • Database validation
  • Use of SCOS data saves effort in simulation setup
  • PUS Compliance
  • Wide variety of testing oriented functions
  • TM Packet Simulation
  • Parameter simulation
  • TC Verification
  • Can easily be applied to other contexts of TM/TC
    simulation outside of EMCS

19
Thank you for your attention
Scheepmakerstraat 40 2222 AC Katwijk ZH The
Netherlands Tel 31-(0)71-402-8120 Fax
31-(0)71-402-7934 www.satserv.nl www.SpacelinkNG
T.com Contact P. van Duijn Executive Director
Email P.van.Duijn_at_satserv.nl
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