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- W3022617437 abstract "The Modular Attitude Control Subsystem (MACS) was developed as part of the Multimission Modular Spacecraft for NASA Goddard Space Flight Center in the late 1970s. This subsystem has demonstrated performance on multiple low earth orbit scientific missions. Application on T/P is derived from the flight proven LANDSAT-5 design and represents the first Fairchild development of the MACS. Design and development are complete with final ground verification underway to support a July 1992 T/P launch. The philosophy of the ground verification process is described in detail. The discussion will provide the approach of subsystem verification from component level testing through ever increasing levels of subsystem and satellite integration. The role of analyses will be described and some on-orbit subsystem performance issues are presented. This work was performed for the Jet Propulsion Laboratory, California Institute of Technology, sponsored by the National Aeronautics and Space Administration." @default.
- W3022617437 created "2020-05-13" @default.
- W3022617437 creator A5068757828 @default.
- W3022617437 date "1993-01-01" @default.
- W3022617437 modified "2023-09-27" @default.
- W3022617437 title "VALIDATION APPROACH FOR THE MODULAR ATTITUDE DETERMINATION CONTROL SUBSYSTEM IMPLEMENTED ON TOPEX/POSEIDON (T/P)" @default.
- W3022617437 doi "https://doi.org/10.1016/b978-0-08-041715-8.50025-0" @default.
- W3022617437 hasPublicationYear "1993" @default.
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