A methodology for autonomous spacecraft design blends autonomy requirements with traditional mission requirements and assesses the impact of autonomy upon the total system resources available to support fault-tolerance and automation. A baseline functional design can be examined for autonomy implementation impacts, and the costs, risk, and benefits of various options can be assessed. The result of the process is a baseline design that includes autonomous control functions.
Autonomous spacecraft design methodology
IECEC ''84: Advanced energy systems - Their role in our future ; 1984 ; San Francisco, CA
1984-01-01
Conference paper
No indication
English
Fault tolerant design and autonomous spacecraft
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