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thesis
oaioai:casi.ntrs.nasa.gov:19820024503

Cost and benefits design optimization model for fault tolerant flight control systems

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1982
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Abstract

Requirements and specifications for a method of optimizing the design of fault-tolerant flight control systems are provided. Algorithms that could be used for developing new and modifying existing computer programs are also provided, with recommendations for follow-on work

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This paper was published in NASA Technical Reports Server.

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