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NASA NTRS ยท 19750009328

Fault tolerant programmable digital attitude control electronics study

Abstract

The attitude control electronics mechanization study to develop a fault tolerant autonomous concept for a three axis system is reported. Programmable digital electronics are compared to general purpose digital computers. The requirements, constraints, and tradeoffs are discussed. It is concluded that: (1) general fault tolerance can be achieved relatively economically, (2) recovery times of less than one second can be obtained, (3) the number of faulty behavior patterns must be limited, and (4) adjoined processes are the best indicators of faulty operation.

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BibTeXRIS

Sorensen, A. A.. 1974-07-25. Fault tolerant programmable digital attitude control electronics study. https://ntrs.nasa.gov/citations/19750009328

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