Discussed in this paper are some of the problems associated with implementing microcomputer-based power system autonomy on spacecraft flight projects, as well as limitations derived from prior development programs. A new approach is given for developing the autonomy architecture, and an architecture concept, based on that approach, is described.
A new approach to implementing spacecraft power system autonomy
1983-01-01
Conference paper
No indication
English
Implementing spacecraft autonomy using discrete control theory
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