NASA NTRS ยท 19910052968
Control law synthesis and stability robustness improvement using constrained optimization techniques
Abstract
The present generic optimization procedure for a continuous or discrete control law (of arbitrary order), which will be applicable to a multiinput-multioutput system, is upon constraining used to satisfy conflicting design requirements on the mean-square responses and stability robustness at the plant input and output. The synthesis procedure is especially suitable for flexible airframes and large space structures modeled by a high-order state-space system of equations. Analytical expressions are obtained for the gradients of the cost function, together with design constraints on the mean-square response and minimum singular value.
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Mukhopadhyay, Vivekananda. 1990-01-01. Control law synthesis and stability robustness improvement using constrained optimization techniques. https://ntrs.nasa.gov/citations/19910052968
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