The research of two-degree freedom small scale helicopters based on kinetic modeling and control analysis

被引:0
|
作者
Lu Changlong [1 ]
Qiu Ping [2 ]
机构
[1] Jingdezhen Ceram Inst, Sch Mech & Elect Engn, Jingdezhen 333403, Peoples R China
[2] Jingdezhen Ceram Inst, Dept Foreign Languages, Jingdezhen 333403, Peoples R China
关键词
small-scale helicopter; modeling; feed-forward control; similarity theory;
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
Two degree of freedom flight test platform was devised to simulate the helicopter by using of the similarity theory. Taking the platform as the researching object and combing the Lagrange-Euler equation with the equivalent moment method, the system dynamic model is derived and the physical parameter is pre-estimated. The relation between the lift force and the change of the rotation speed is acquired by the experiment with the fixed collective angle. According to the kinetic equation, a PID revised feed-forward controlling algorithm with robust characteristic was devised and the MATLAB simulation is applied to verify fast astringency and validity of the controller
引用
收藏
页码:929 / 934
页数:6
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