Design of Multi-mode Flight Control System for Unmanned Helicopter

被引:0
|
作者
Xu Hongzhe [1 ]
Huang Jun [1 ]
Zhou Yaoming [1 ]
机构
[1] Beijing Univ Aeronaut & Astronaut, Dept Aeronaut Sci & Engn, Beijing 100191, Peoples R China
关键词
Flight Control; FCC; Stability Augmentation; Autonomous Control; Semi-physical Simulation;
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
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.
引用
收藏
页码:3660 / 3663
页数:4
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