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Practical optimal flight control system design for helicopter aircraft. Volume 1: Technical ReportA 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.
Document ID
19800014839
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hofmann, L. G. (Systems Technology, Inc. Hawthorne, CA, United States)
Riedel, S. A. (Systems Technology, Inc. Hawthorne, CA, United States)
Mcruer, D. (Systems Technology, Inc. Hawthorne, CA, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1980
Subject Category
Aircraft Stability And Control
Report/Patent Number
TR-1127-1-I
NASA-CR-3275
Report Number: TR-1127-1-I
Report Number: NASA-CR-3275
Accession Number
80N23328
Funding Number(s)
CONTRACT_GRANT: NAS2-9946
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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