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- W2065720104 abstract "Microprocessors that meet the typical spacecraft requirements for radiation tolerance, low power dissipation and high reliability normally have relatively low computing throughput. Due to the requirements for fine attitude determination and the need to control and respond to a large number of interfaces, a high throughput processor was needed in the Midcourse Space Experiment (MSX) attitude determination and control system. The needed throughput in the MSX attitude processor was achieved by dividing the tasks of attitude determination and control, interrupt processing and interface control among several lower throughput computers including two Mil-Std-1750A processors and two 8085" @default.
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- W2065720104 date "1993-08-22" @default.
- W2065720104 modified "2023-09-25" @default.
- W2065720104 title "A low power, radiation tolerant spacecraft attitude processor" @default.
- W2065720104 doi "https://doi.org/10.2514/6.1993-4492" @default.
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