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- W83646711 abstract "The testing of Spacecraft Attitude and Orbit Control Subsystems is described from the early design up to in-flight, inclusive. Main topics dealt with are: description of three generic AOCS test classes, model philosophy, standardization, subsystem static test methods, subsystem dynamic test methods, generic test equipment and test facilities.Main conclusions are:1. test scheduling should aim to find problems and errors as early as possible. Consequently system level tests should be descoped in favor of detailed testing of the AOCE (unit level) and in particular subsystem level testing;2. onboard AOCS software poses new testing problems, especially when RAM located;3. there is a shift from airbearing-type dynamic tests to servo-tabletype dynamic tests, mainly due to increasing spacecraft sizes, structural flexibility and multi-body dynamics concepts." @default.
- W83646711 created "2016-06-24" @default.
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- W83646711 date "1984-05-18" @default.
- W83646711 modified "2023-09-27" @default.
- W83646711 title "Testing of spacecraft attitude and orbit control systems" @default.
- W83646711 hasPublicationYear "1984" @default.
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