Trajectory Tracking Control for a Rotary Wing Vehicle Powered by Four Rotors

被引:0
作者
José J. Corona-Sánchez
Hugo Rodríguez-Cortés
机构
[1] CINVESTAV-IPN,Departamento de Ingeniería Eléctrica
来源
Journal of Intelligent & Robotic Systems | 2013年 / 70卷
关键词
Nonlinear control; Aerial vehicles; Trajectory tracking;
D O I
暂无
中图分类号
学科分类号
摘要
The present paper presents a trajectory tracking control scheme for an underactuated rotary wing vehicle. The translational controller is designed based on feedback linearization and saturated control. The rotational controller is designed based on the passivity properties of the rotational dynamics. The interconnection between the translational and the rotational controllers is inspired by the backstepping control technique. The final control structure allows to include an integral action that is able to compensate constant disturbances on the rotational dynamics. It is shown that the resulting closed–loop dynamics has a local asymptotic stability property. Numerical simulations show the performance of the proposed controller.
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页码:39 / 50
页数:11
相关论文
共 25 条
[1]  
Davis WR(1998)Micro air vehicles for optical surveillance Linc. Lab. J. 9 197-214
[2]  
Kosicki BB(2009)Nonlinear notion control of a rotary wing vehicle powered by four rotors Revista Ingeniería, Investigación y Tecnología X 1405-7743
[3]  
Boroson DM(2008)A practical visual servo control for an unmanned aerial vehicle IEEE Trans. Robot. 24 331-340
[4]  
Kostishack DF(2005)Stabilization of a mini rotorcraft with four rotors Control Syst. Mag. 25 45-55
[5]  
Araujo-Estrada SA(2010)An integral predictive/nonlinear Automatica 46 29-39
[6]  
Liceaga-Castro E(2004) control structure for a quadrotor helicopter IEEE Trans. Automat. Contr. 49 1975-1990
[7]  
Rodríguez-Cortés H(1996)Nonlinear control of feedforward systems with bounded signals IEEE Trans. Automat. Contr. 41 468-472
[8]  
Guenard N(2011)Attitude control without angular velocity measurement: a passivity approach Control Eng. Pract. 19 790-797
[9]  
Hamel T(undefined)Bounded attitude control of rigid bodies: real-time experimentation to a quadrotor mini-helicopter undefined undefined undefined-undefined
[10]  
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