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

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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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