Output tracking with nonhyperbolic and near nonhyperbolic internal dynamics: Helicopter hover control

被引:34
|
作者
Devasia, S
机构
[1] Department of Mechanical Engineering, University of Utah, Salt Lake City
关键词
D O I
10.2514/2.4079
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A technique to achieve output tracking for nonminimum phase linear systems with nonhyperbolic and near nonhyperbolic internal dynamics is presented. This approach integrates stable inversion techniques, which achieve exact tracking, with approximation techniques, which modify the internal dynamics, to achieve desirable performance. such modification of the internal dynamics is used 1) to remove nonhyperbolicity, which is an obstruction to applying stable inversion techniques, and 2) to reduce large preactuation times needed to apply stable inversion for near nonhyperbolic cases. The method is applied to an example helicopter hover control problem with near nonhyperbolic internal dynamics for illustrating the tradeoff between exact tracking and reduction of preactuation time.
引用
收藏
页码:573 / 580
页数:8
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