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NASA NTRS ยท 19840003103

F100 Multivariable Control Synthesis Program. Computer Implementation of the F100 Multivariable Control Algorithm

Abstract

As turbofan engines become more complex, the development of controls necessitate the use of multivariable control techniques. A control developed for the F100-PW-100(3) turbofan engine by using linear quadratic regulator theory and other modern multivariable control synthesis techniques is described. The assembly language implementation of this control on an SEL 810B minicomputer is described. This implementation was then evaluated by using a real-time hybrid simulation of the engine. The control software was modified to run with a real engine. These modifications, in the form of sensor and actuator failure checks and control executive sequencing, are discussed. Finally recommendations for control software implementations are presented.

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BibTeXRIS

Soeder, J. F.. 1983-10-01. F100 Multivariable Control Synthesis Program. Computer Implementation of the F100 Multivariable Control Algorithm. https://ntrs.nasa.gov/citations/19840003103

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