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oaioai:casi.ntrs.nasa.gov:19830017440

NASA propulsion controls research

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1983
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Abstract

Multivariable control theory is applied to the design of multiple input and output engine controls. Highly-accurate, real-time engine simulations are utilized for control development and checkout. Electro-optical control components are developed for use in electronic control systems having fiber optic data links. Integrated controls are developed for VSTOL and Rotorcraft propulsion systems. Post-stall models of engine systems are developed to aid in understanding and control of post-stall engine behavior

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This paper was published in NASA Technical Reports Server.

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