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A Real-Time Dynamic Spacecraft Simulator for the LANDSAT-D MissionA real time dynamic simulator for LANDSAT D was developed and has played an integral role in the development and validation of both the ground control system and of the on-board flight software. The simulator utilized an electronic replica of the spacecraft on-board computer and data handling hardware interfaced to a VAX 11/780 computer and simulation software. Key features of the simulator design are a modular software architecture tailored to the VAX/VMS real time capabilities, a microprocessor controlled interface between the VAX and the flight hardware replica, complete simulation of the spacecraft and NASA network communication links, and a flexible and powerful scenario structuring and operator control capability. The design goals and trade-offs, software, and hardware design are summarized. The application of the simulator to the validation of both the ground systems and on-board software is reviewed in detail.
Document ID
19820017423
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Allen R Coffin
(General Electric Co. Falls Church, VA, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1982
Publication Information
Publication: Twelfth Space Simulation Conference: Shuttle Plus One. A New View of Space
Publisher: National Aeronautics and Space Administration
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
REPT-82B0455
NASA-CP-2229
NAS 1.55:2229
Meeting Information
Meeting: Twelfth Space Simulation Conference
Location: Pasadena, CA
Country: US
Start Date: May 17, 1982
End Date: May 19, 1982
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
82N25299
Funding Number(s)
CONTRACT_GRANT: NAS5-2300
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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