NASA NTRS · 19800014839
Practical optimal flight control system design for helicopter aircraft. Volume 1: Technical Report
Abstract
A method by which modern and classical theory techniques may be integrated in a synergistic fashion and used in the design of practical flight control systems is presented. A general procedure is developed, and several illustrative examples are included. Emphasis is placed not only on the synthesis of the design, but on the assessment of the results as well.
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Hofmann, L. G., Riedel, S. A., Mcruer, D.. 1980-05-01. Practical optimal flight control system design for helicopter aircraft. Volume 1: Technical Report. https://ntrs.nasa.gov/citations/19800014839
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