摘要
采用基于模型逆的显模型跟踪控制方法，借鉴ADS-33要求设计了舰载无人直升机俯仰姿态控制律，并进行了仿真验证，较好地解决了舰载无人直升机姿态控制的难题。
The pitch attitude control law was designed using explicit model-following control method based on contrary model according to the demand of ADS-33. It was validated feasibility by simulation, and the problem of attitude control for unmanned shipboard helicopter was solved better.
出处
《海军航空工程学院学报》
2009年第5期543-546,共4页
Journal of Naval Aeronautical and Astronautical University
关键词
显模型跟踪控制
无人舰载直升机
姿态控制
explicit model-following control
unmanned shipboard helicopter
attitude control system
