A Total Energy Control System strategy for the Quadrotor Helicopter

被引：0
|
作者：
Vasquez-Beltran, M. A. [1 ]
Rodriguez-Cortes, H. [2 ]
机构：
[1] Inst Politecn Nacl, Ctr Invest & Estudios Avanzados, Ave IPN 2508, Mexico City 07360, DF, Mexico
[2] Inst Politecn Nacl, Ctr Desarrollo Aeroespacial, Belisario Dominguez 22,Col Ctr, Mexico City 06010, DF, Mexico
来源：
2015 INTERNATIONAL CONFERENCE ON UNMANNED AIRCRAFT SYSTEMS (ICUAS'15) | 2015年
关键词：
CONTROLLED LAGRANGIANS; NONLINEAR CONTROLLER; INTERCONNECTION; STABILIZATION; NAVIGATION;
D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
This paper proposes a control strategy for the quadrotor helicopter based on the Total Energy Control System (TECS) approach. Assuming that the rotational dynamics control loop is faster than the translational dynamics control loop, a TECS based control strategy is designed for the translational dynamics. The performance of the proposed control strategy is verified experimentally.
引用
收藏
页码：286 / 293
页数：8
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