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NASA NTRS ยท 19850063779

Stability robustness improvement using constrained optimization techniques

Abstract

In a multiloop feedback control system, stability margin improvement by singular value shaping can be achieved by a noise adjustment procedure. A direct method for shaping singular value spectrum using constrained optimization technique is described. The design algorithm minimizes a standard LQG performance index while trying to satisfy minimum singular value constraints at the plant input, or output, or at both. Selected parameters of a stabilizing control law are used as the design variables. The capabilities of this method are demonstrated using a two input two output system representing a drone aircraft and its lateral attitude control system.

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BibTeXRIS

Mukhopadhyay, V.. 1985-01-01. Stability robustness improvement using constrained optimization techniques. https://ntrs.nasa.gov/citations/19850063779

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