NASA NTRS · 19980017310
QFT Multi-Input, Multi-Output Design with Non-Diagonal, Non-Square Compensation Matrices
Abstract
A technique for obtaining a non-diagonal compensator for the control of a multi-input, multi-output plant is presented. The technique, which uses Quantitative Feedback Theory, provides guaranteed stability and performance robustness in the presence of parametric uncertainty. An example is given involving the lateral-directional control of an uncertain model of a high-performance fighter aircraft in which redundant control effectors are in evidence, i.e. more control effectors than output variables are used.
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Hess, R. A., Henderson, D. K.. 1996-01-01. QFT Multi-Input, Multi-Output Design with Non-Diagonal, Non-Square Compensation Matrices. https://ntrs.nasa.gov/citations/19980017310
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