On the structure of robust controllers and weight selection in the mixed sensitivity minimization

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Abstract

In this paper we examine the structure of robust controllers obtained from the mixed sensitivity minimization for a class of mechanical systems consisting of rigid body dynamics, weak flexible modes, and small time delays (or non-minimum phase effects due to non-collocated actuator and sensor). In particular, we study the weight selection in the mixed sensitivity design and illustrate that for certain performance and robustness objectives, the resulting H∞ optimal controller is in the form of a classical PID controller cascaded by a filter suppressing the uncertain flexible modes. Furthermore, we provide a link between this H∞ optimal controller and the conventional three-loop controller/autopilot (3LC) scheme frequently used in aerospace applications. More precisely, the 3LC scheme is shown to be equivalent to a two-degree-of freedom (2DoF) control structure where the H∞ controller is used in the feedback loop and the reference signal is filtered outside the loop.

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AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025

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American Institute of Aeronautics and Astronautics Inc.

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Citation

Published Version (Please cite this version)

Language

English