Synthesis of optimal H∞ controllers is formulated as a loop-shaping problem where the desired closed-loop shape to be pursued is a flat frequency response of the largest singular value. The weighted H2 optimization technique used in LQG/LTR is exploited in the loop shaping procedures to generate a sequence of H2 controllers converging to the optimal H∞ controller. The resulting optimal H∞ controller not only has the inherent robust property due to H∞ criterion but also possesses the nice H2 control structure, being easy to compute and implement. A flight control example is demonstrated to show that the numerical accuracy of the present LQG-based H∞ synthesis is comparable to the conventional H∞ approach, i.e. γ-iteration
Published in:
Decision and Control, 1996., Proceedings of the 35th IEEE Conference on
(Volume:1
)
Date of Conference: 11-13 Dec 1996