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Integrated flight/propulsion control - Subsystem specifications for performanceA procedure is presented for calculating multiple subsystem specifications given a number of performance requirements on the integrated system. This procedure applies to problems where the control design must be performed in a partitioned manner. It is based on a structured singular value analysis, and generates specifications as magnitude bounds on subsystem uncertainties. The performance requirements should be provided in the form of bounds on transfer functions of the integrated system. This form allows the expression of model following, command tracking, and disturbance rejection requirements. The procedure is demonstrated on a STOVL aircraft design.
Document ID
19930067403
Document Type
Conference Paper
Authors
Neighbors, W. K. (NASA Lewis Research Center Cleveland, OH, United States)
Rock, Stephen M. (Stanford Univ. CA, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Publication Information
Publication: In: AIAA Guidance, Navigation and Control Conference, Monterey, CA, Aug. 9-11, 1993, Technical Papers. Pt. 2 (A93-51301 22-63)
Subject Category
AIRCRAFT STABILITY AND CONTROL
Report/Patent Number
AIAA PAPER 93-3808
Funding Number(s)
CONTRACT_GRANT: NAG3-1177
Distribution Limits
Public
Copyright
Other