CALCULUS OF VARIATIONS DERIVATION OF THE MINIMAX LINEAR-QUADRATIC (H-INFINITY) CONTROLLER

被引:0
|
作者
MILLS, RA [1 ]
BRYSON, AE [1 ]
机构
[1] STANFORD UNIV,DEPT AERONAUT & ASTRONAUT,STANFORD,CA 94305
关键词
D O I
10.2514/3.21172
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The linear-quadratic best controller for the worst bounded disturbances (LQW controller), or so-called H-infinity controller, is derived as a differential game between the controller and disturber using the calculus. of variations. This derivation explicitly shows that for the full-order LQW controller the worst measurement disturbance is zero (!) and the controller initial conditions must be set equal to the plant initial conditions for a well-posed differential game. As in previous derivations, the worst process disturbance is shown to be a feedback on the plant States. The derivation yields necessary conditions for reduced-order and higher older LQW controllers, useful in multiple-plant optimization for robustness. A helicopter near hover is used to illustrate differences between LQW and linear-quadratic-Gaussian (LQG) control. This comparison suggests the relative merits of LQG and LQW control design and shows that a special case of LQW control called infinite-disturbance LQW (''optimal'' H-infinity) control is not practical.
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页码:153 / 160
页数:8
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