Abstract
This paper presents a new method for designing H∞ optimal or suboptimal controllers for nonlinear systems. A stability analysis is conducted using simplicial algorithms. In this example gains are used as the H∞ weighting functions. The system is a unstable first order plant, driven by a Bang-Bang actuator. A describing function model of the actuator is used in this analysis.
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More From: Automatic Control in Aerospace 1994 (Aerospace Control '94)
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