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Stochastic performance robustness of aircraft control systemsStochastic robustness, a simple technique used to estimate the robustness of linear, time-invariant systems, is applied to a twin-jet transport aircraft control system. Concepts behind stochastic stability robustness are extended to stochastic performance robustness. Stochastic performance robustness measures based on classical design specifications and measures specific to aircraft handling qualities are introduced. Confidence intervals for both individual stochastic robustness measures and for comparing two measures are presented. The application of stochastic performance robustness, the use of confidence intervals, and tradeoffs between performance objectives are demonstrated by means of the twin-jet aircraft example.
Document ID
19900060610
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Stengel, Robert F.
(Princeton University NJ, United States)
Ray, Laura Ryan
(Princeton Univ. NJ, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1990
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA PAPER 90-3410
Report Number: AIAA PAPER 90-3410
Meeting Information
Meeting: AIAA Guidance, Navigation and Control Conference
Location: Portland, OR
Country: United States
Start Date: August 20, 1990
End Date: August 22, 1990
Accession Number
90A47665
Funding Number(s)
CONTRACT_GRANT: DAAL03-89-K-0092
CONTRACT_GRANT: NGL-31-001-252
Distribution Limits
Public
Copyright
Other

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