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Modeling and parameter uncertainties for aircraft flight control system designValues of plant dynamic uncertainties for some recent aircraft design and development programs are given. Histories of pertinent aerodynamic, inertial, and structural parameter variations are given for a period of time from program initiation to aircraft certification. These data can be used as typical of future vehicles so that control system design concepts are evaluated with due consideration to their sensitivity to uncertainties in plant dynamics.
Document ID
19770026205
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mcdonnell, J. D. (Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Berg, R. A. (Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Heimbaugh, R. M. (Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Felton, C. A. (Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1977
Publication Information
Publisher: NASA
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-2887
MDC-J4555
Report Number: NASA-CR-2887
Report Number: MDC-J4555
Accession Number
77N33149
Funding Number(s)
CONTRACT_GRANT: NAS1-14151
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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