An framework for robust flight control design using constrained optimizationAn analytical framework is described for the design of feedback control systems to meet specified performance criteria in the presence of structured and unstructured uncertainty. Attention is focused upon the linear time invariant, single-input, single-output problem for the purposes of exposition. The framework provides for control of the degree of the stabilizing compensator or controller.
Document ID
19920072658
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Palazoglu, A. (NASA Ames Research Center Moffett Field, CA, United States)
Yousefpor, M. (NASA Ames Research Center Moffett Field, CA, United States)
Hess, R. A. (California, University Davis, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Subject Category
Cybernetics
Report/Patent Number
AIAA PAPER 92-4603
Meeting Information
Meeting: AIAA Guidance, Navigation and Control Conference