Design of Multi-mode Flight Control System for Unmanned Helicopter

摘要：

Based on the special requirements of flight control and navigation system of unmanned helicopter,this paper present the main framework of flight control system in a certain type of unmanned helicopter,proposed three flight control modes based on different design stages,gave the autonomous control algorithm and the smoothing method while switching between remote control mode and stability augmentation mode,ultimately proved the feasibility of flight control and navigation program through the semi-physical simulation test and flight test.

作者: XU Hongzhe HUANG Jun ZHOU Yaoming

作者单位: Department of Aeronautics Science and Engineering,Beijing University of Aeronautics and Astronautics,Beijing 100191,P.R.China

会议类型: 国际会议

会议名称: The 30th Chinese Control Conference(第三十届中国控制会议)

会议地点: 烟台

会议语种:英文

页码: 1-4

在线出版日期: 2011-07-01（万方平台首次上网日期，不代表论文的发表时间）