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zui you diao jie qi she ji de ying yong shi li
Author(s): 
Pages: 6-14
Year: Issue:  4
Journal: Aerospace Control

Keyword:  现代控制理论运动微分方程性能函数离散系统最优控制增广系统超调量稳态误差权阵姿态角;
Abstract: <正> 本文对某飞行器航向通道设计了最优调节器,给出了现代控制理论具体应用的一个实例。1.最优调节器的设计设某飞行器的航向质心运动微分方程如下
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