Computer Science – Software Engineering
Scientific paper
Mar 1992
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1992stin...9430857s&link_type=abstract
Presented at the 1992 European Simulation Multiconference, York, England, 1-3 Jun. 1992
Computer Science
Software Engineering
Checkout, Computer Systems Simulation, Control Simulation, Program Verification (Computers), Satellite Attitude Control, Space Vehicle Checkout Program, Spacecraft Design, Test Facilities, Architecture (Computers), Channels (Data Transmission), Embedded Computer Systems, Italian Space Program, Real Time Operation, Software Engineering, Systems Integration
Scientific paper
The place of a Modular Attitude and Orbit Control Subsystem Test and Simulation Assembly (MACS-TSA) in the development process of the ISO (Infrared Space Observatory) and SAX (Italian X-ray Astronomy Satellite) spacecrafts is given, with emphasis on the simulation aspects. The MACS-TSA is used as checkout equipment during the integration of Attitude and Orbit Control System (AOCS) hardware and software at subsystem level. The other spacecraft subsystems are simulated, as well as their dynamic behavior in the orbital environment. A description of the components of the TSA is given.
Keppel Henk
Sonnenschein Frans J.
No associations
LandOfFree
The MACS-TSA applied in the ISO and SAX spacecraft projects does not yet have a rating. At this time, there are no reviews or comments for this scientific paper.
If you have personal experience with The MACS-TSA applied in the ISO and SAX spacecraft projects, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and The MACS-TSA applied in the ISO and SAX spacecraft projects will most certainly appreciate the feedback.
Profile ID: LFWR-SCP-O-1491850