无人直升机自动起飞控制技术研究
Computer Measurement & Control(2007)
Abstract
以无人直升机起飞段非线性模型为对象,研究了自动起飞控制技术方案,以空中定点控制方案为起点根据控制仿真结果对系统进行改进控制,分别加入线加速度反馈和直接力反馈,达到较好的无人直升机自动起飞控制要求。
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Key words
linear acceleration,fixed point control,direct force,unmanned helicopter,automatic takeoff
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