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oaioai:casi.ntrs.nasa.gov:19920013401

Design of an integrated airframe/propulsion control system architecture

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1990
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Abstract

The design of an integrated airframe/propulsion control system architecture is described. The design is based on a prevalidation methodology that uses both reliability and performance. A detailed account is given for the testing associated with a subset of the architecture and concludes with general observations of applying the methodology to the architecture

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This paper was published in NASA Technical Reports Server.

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