Journal of Guangdong University of Technology ›› 2010, Vol. 27 ›› Issue (2): 1-5.

• Comprehensive Studies •     Next Articles

Bilinear Control over the Yaw Control of Small-scale Unmanned Helicopters

  

  1. Faculty of Automation,Guangdong University of Technology,Guangzhou 5 10090,China
  • Online:2010-06-25 Published:2010-06-25

Abstract: Bilinear control strategy based on model bias separation is proposed,and it is applied to the yaw control of small-scale unmanned helicopters.The system model is divided into two parts:linear mode1 and uncertainty. The information of uncertainty is online obtained by the novel structure of model bias separation. The c0ntroller is the integration of a conventional linear controller with a linear compensator. The simulation resuits verify the effectiveness of the proposed bilinear control strategy.

Key words: bilinear control;model bias separation;unmanned helicopter:yaw control

[1]姜哲,何玉庆,赵新刚,等.基于反馈线性化的无人直升机航向控制[J].机器人,2007,29(3):193-199.

[2]Mettler B.Identification Modeling and Characteristics of Miniature Rotorcraft『M].Norwell:Kluwer Academic Publishers,2003:163-200.

[3]Ping Song,Qi Guang—ping,Li Ke-jie.The flight control system based on multivariable PID neural network for smal1.scale unmanned helicopter[C]∥International Conf.information Technology and Computer Science,2009:538-541.

[4]Xin Hou,Ping Li,Zhou Fang,et a1.An application of fuzzy PID algorithm on unmanned helicopter attitude control[c]ff Proc.of the 6th World Congress on Intelligent Control

and Automation,2006:9129-9133.

[5]Sanchez E N,Becerra H M,Velez C M.Combining fuzzy and PID control for an unmanned helicopter[C]∥Annual meeting of the North American Fuzzy Information Processing Society,2005:235-240.

[6]Wang Xiao·dong,Zhao Xiao—guang.A practial survey on the flight control system of small—scale unmanned helicopter [C]∥Proc.of the 7th World Congress on Intelligent Control an Automation,2008:364-369.

[7]Daigo Fjiwara,Kenzo Nonami.H。。hovering and guidance control for autonomous small—scale unmanned helicopter [c]∥Proc.of IEEE/RSJ International Conference on In.telligent Robots and Systems,2004:2463-2468.

[8]Civita M L.Integrated Modeling and Robust Con~ol for Full-Envelope Flight of Robotic Helicopters[C]∥Proc.of IEEE International Conf.Robotics& Automation.2003:552-557.

[9]Shim D H.Hierarchical Flight Control System Synthesis for Rotorcraft based Unmanned Aerial Vehicles[c]∥ AIAA Guidan ce,Navigation an d Control Conf.& Exhibit,2000:1-9.

[10]Johnson E N,Kannan S K.Adaptive Trajectory Control for Autonomous Helicopters[J].AIAA Journal of Guidance,Control,and Dynamics,2005,28(3):524-538.

[11]Pesonen U J,Steck J E,Rokhsaz K,et a1.Adaptive neural network inverse controller for general aviation safety[J].Journal ofGuidance,Control,and Dynamics,2004,27(3):434-443.

[12]赵新刚,姜哲,韩建达,等.模型直升机航向自适应保性能控制[J].系统仿真学报,2007,19(13):3047-3051.

[13]胡寿松.自动控制原理[M].北京:科学出版社,2006:398-510.
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