A COMPUTER-AIDED SIMULATION PROGRAM DESIGN FOR TESTING THE FLIGHT CONTROLLER OF A THREE AXIS STABILIZED SPACECRAFT
International Telemetering Conference Proceedings / October 13-15, 1981 / Bahia Hotel, San Diego, California === To insure a reliable performance of any spacecraft over its long mission life, a thorough and coordinated attitude control subsystem testing must be conducted. The three axis motion Sim...
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| Language: | en_US |
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International Foundation for Telemetering
1981
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| Online Access: | http://hdl.handle.net/10150/615313 http://arizona.openrepository.com/arizona/handle/10150/615313 |