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A Computational Framework to Control Verification and Robustness AnalysisThis paper presents a methodology for evaluating the robustness of a controller based on its ability to satisfy the design requirements. The framework proposed is generic since it allows for high-fidelity models, arbitrary control structures and arbitrary functional dependencies between the requirements and the uncertain parameters. The cornerstone of this contribution is the ability to bound the region of the uncertain parameter space where the degradation in closed-loop performance remains acceptable. The size of this bounding set, whose geometry can be prescribed according to deterministic or probabilistic uncertainty models, is a measure of robustness. The robustness metrics proposed herein are the parametric safety margin, the reliability index, the failure probability and upper bounds to this probability. The performance observed at the control verification setting, where the assumptions and approximations used for control design may no longer hold, will fully determine the proposed control assessment.
Document ID
20100006918
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Crespo, Luis G.
(National Inst. of Aerospace Hampton, VA, United States)
Kenny, Sean P.
(NASA Langley Research Center Hampton, VA, United States)
Giesy, Daniel P.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 25, 2013
Publication Date
January 1, 2010
Subject Category
Aircraft Stability And Control
Report/Patent Number
L-19786
NASA/TP-2010-216189
LF99-8484
Report Number: L-19786
Report Number: NASA/TP-2010-216189
Report Number: LF99-8484
Funding Number(s)
CONTRACT_GRANT: NNX07AC48A
CONTRACT_GRANT: NNH07ZEA001N
WBS: WBS 457280.02.07.07.06.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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