NASA NTRS · 19740023314
Flight control systems research
Abstract
Theoretical development is reported for the parameter optimization design technique needed for digital flight control system design. The results of an example case study applying the optimization technique for continuous systems to an F-8 aircraft feedback control system are presented. The concept of evolving the simplest system configuration that is capable of meeting a specified set of performance requirements is illustrated in this work.
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Whitaker, H. P., Baram, Y., Cheng, Y.. 1973-11-01. Flight control systems research. https://ntrs.nasa.gov/citations/19740023314
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