Abstract
A sufficient condition is derived for the existence of the optimal μ controllers by showing the equivalence between the optimal μ problem and the weighted H2-optimization problem. The weighted H2-optimization technique used in linear quadratic Gaussian design with loop transfer recovery is exploited to generate a sequence of H2 controllers converging to the optimal μ controller. The resulting optimal μ controller not only has the inherent robust-performance property resulting from the μ 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 H2-based μ-synthesis approach is comparable to the conventional H∞-based μ-synthesis technique (D-K iteration) but with reduced computational efforts.
Original language | English |
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Pages (from-to) | 886-892 |
Number of pages | 7 |
Journal | Journal of Guidance, Control, and Dynamics |
Volume | 19 |
Issue number | 4 |
DOIs | |
Publication status | Published - 1996 |
All Science Journal Classification (ASJC) codes
- Control and Systems Engineering
- Aerospace Engineering
- Space and Planetary Science
- Electrical and Electronic Engineering
- Applied Mathematics