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A Verification-Driven Approach to Control Analysis and TuningThis paper proposes a methodology for the analysis and tuning of controllers using control verification metrics. These metrics, which are introduced in a companion paper, measure the size of the largest uncertainty set of a given class for which the closed-loop specifications are satisfied. This framework integrates deterministic and probabilistic uncertainty models into a setting that enables the deformation of sets in the parameter space, the control design space, and in the union of these two spaces. In regard to control analysis, we propose strategies that enable bounding regions of the design space where the specifications are satisfied by all the closed-loop systems associated with a prescribed uncertainty set. When this is unfeasible, we bound regions where the probability of satisfying the requirements exceeds a prescribed value. In regard to control tuning, we propose strategies for the improvement of the robust characteristics of a baseline controller. Some of these strategies use multi-point approximations to the control verification metrics in order to alleviate the numerical burden of solving a min-max problem. Since this methodology targets non-linear systems having an arbitrary, possibly implicit, functional dependency on the uncertain parameters and for which high-fidelity simulations are available, they are applicable to realistic engineering problems..
Document ID
20080033122
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Crespo, Luis G.
(National Inst. of Aerospace Associates 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 24, 2013
Publication Date
August 18, 2008
Subject Category
Systems Analysis And Operations Research
Meeting Information
Meeting: AIAA Guidance, Navigation and Control Conference and Exhibit
Location: Honolulu, HI
Country: United States
Start Date: August 18, 2008
End Date: August 21, 2008
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 457280
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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