TIME-SCALE SYNTHESIS OF A CLOSED-LOOP DISCRETE OPTIMAL-CONTROL SYSTEM

被引:19
|
作者
NAIDU, DS [1 ]
PRICE, DB [1 ]
机构
[1] NASA,LANGLEY RES CTR,SPACECRAFT CONTROL BRANCH,DIV GUIDANCE & CONTROL,HAMPTON,VA 23665
关键词
CONTROL SYSTEMS; DIGITAL - CONTROL SYSTEMS; DISCRETE TIME - CONTROL SYSTEMS; OPTIMAL - MATHEMATICAL TECHNIQUES - Matrix Algebra;
D O I
10.2514/3.20235
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A two-time-scale discrete control system is considered. The closed-loop optimal linear quadratic regulator for the system requires the solution of a full-order algebraic matrix Riccati equation. Alternatively, the original system is decomposed into reduced-order slow and fast subsystem. The closed-loop optimal control of the subsystems requires the solution of two algebraic matrix Riccati equations of an order lower than that required for the full-order system. A composite, closed-loop suboptimal control is created from the sum of the slow and fast feedback optimal controls. Numerical results obtained for an aircraft model show a very close agreement between the exact (optimal) solutions and computationally simpler composite (suboptimal) solutions.
引用
收藏
页码:417 / 421
页数:5
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