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fei xing qi shang gan rao de ce liang he bu chang
Author(s): 
Pages: 19-26
Year: Issue:  1
Journal: Aerospace Control

Keyword:  观测器增广系统反馈控制全部状态反馈增益线性最优化状态反馈原系统补偿原理状态方程;
Abstract: <正> 1、引言在“具有参数补偿的线性最优化系统设计”中论论了飞行器稳定系统采用观测器获得系统状态的方法,用参数补偿原理消除弹体弹性弯曲振动,及通过反馈增益阵实现全状态最优反馈控制。本文在上述工作基础上,设计增广系统全维或降维观测器,观测包括干扰变量在内的全部状态。这样,观测器不但是状态测量装置,也是干扰的测量装置。在满足一定的条件下,设计干扰补偿通道,用干扰补偿干扰。
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