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F100 Multivariable Control Synthesis Program. Computer Implementation of the F100 Multivariable Control AlgorithmAs 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.
Document ID
19840003103
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Soeder, J. F.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
October 1, 1983
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.60:2231
NASA-TP-2231
E-1496
Report Number: NAS 1.60:2231
Report Number: NASA-TP-2231
Report Number: E-1496
Accession Number
84N11171
Funding Number(s)
PROJECT: RTOP 505-34-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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