APPROXIMATE POLE PLACEMENT APPROACH

被引:4
|
作者
LILJA, M
ASTROM, KJ
机构
[1] Lund Institute of Technology, Department of Automatic Control, Lund
关键词
D O I
10.2514/3.20953
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A recently developed design method is applied to the benchmark problem. The design method may be viewed as a numerical loop-shaping method that also permits approximate assignment of the dominant poles of the closed-loop system. Solutions with different properties are obtained depending on the choice of closed-loop poles. Three different designs are given. The first is a a high-gain solution, the second gives a controller with relative degree 2, and the last one gives a controller with relative degree 1. The controllers satisfy the given design criteria. The chosen design method also makes it possible to tune a controller for structured parameter variations. A special controller, which admits a wide range of variations in the spring constant, is designed. It is also shown that the design method can easily be extended to deal with disturbances with known frequencies.
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页码:1082 / 1086
页数:5
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