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Tradeoff methods in multiobjective insensitive design of airplane control systemsThe latest results of an ongoing study of computer-aided design of airplane control systems are given. Constrained minimization algorithms are used, with the design objectives in the constraint vector. The concept of Pareto optimiality is briefly reviewed. It is shown how an experienced designer can use it to find designs which are well-balanced in all objectives. Then the problem of finding designs which are insensitive to uncertainty in system parameters are discussed, introducing a probabilistic vector definition of sensitivity which is consistent with the deterministic Pareto optimal problem. Insensitivity is important in any practical design, but it is particularly important in the design of feedback control systems, since it is considered to be the most important distinctive property of feedback control. Methods of tradeoff between deterministic and stochastic-insensitive (SI) design are described, and tradeoff design results are presented for the example of the a Shuttle lateral stability augmentation system. This example is used because careful studies have been made of the uncertainty in Shuttle aerodynamics. Finally, since accurate statistics of uncertain parameters are usually not available, the effects of crude statistical models on SI designs are examined.
Document ID
19870002297
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Schy, A. A.
(Kentron International, Inc. Hampton, VA, United States)
Giesy, D. P.
(Kentron International, Inc. Hampton, Va., United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1984
Publication Information
Publication: NASA. Langley Research Center Recent Experiences in Multidisciplinary Analysis and Optimization, Part 1
Subject Category
Aircraft Stability And Control
Accession Number
87N11730
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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