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oaioai:casi.ntrs.nasa.gov:19830007045

Advanced flight control system study

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1982
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Abstract

The architecture, requirements, and system elements of an ultrareliable, advanced flight control system are described. The basic criteria are functional reliability of 10 to the minus 10 power/hour of flight and only 6 month scheduled maintenance. A distributed system architecture is described, including a multiplexed communication system, reliable bus controller, the use of skewed sensor arrays, and actuator interfaces. Test bed and flight evaluation program are proposed

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This paper was published in NASA Technical Reports Server.

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