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zhi sheng ji xuan ting kong zhi qi de she ji
Author(s): 
Pages: 63-67
Year: Issue:  2
Journal: Aircraft Design

Keyword:  直升机控制器悬停;
Abstract: 直升机在空中定点悬停是飞行任务中的一个重要课题,只靠飞行员操纵来达到精确的悬停是非常困难的。本文利用现代控制理论来设计直升机悬停控制器,文中推导了最优控制算式,并在IBM—PC机上进行了数字仿真,结果表明该系统在悬停时具有较高的位置精度。
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