Modeling and Control System Design of a Small-Scale Unmanned Helicopter
This paper investigates the modeling and control system design of a small-scale unmanned helicopter.We employ a system identification method to get the attitude angular velocity transfer function of a helicopter,and apply a nested PID approach to design the control system,which can be used to control the attitude and position of a helicopter.Experiment results show that the identified model has well accuracy and the control system designed based on the model can control the attitude and position of a helicopter quite well.
unmanned helicopter modeling control.
Wang Jinhua Bai Zhiqiang Liu Peizhi Hu Xiongwen
Intelligence and Integrated Measurement & Control Department Beijing Institute of Computer Application,Beijing,China
国际会议
International Conference on Modelling,Identification and Control(模拟、鉴定、控制国际会议)
上海
英文
2008-06-29(万方平台首次上网日期,不代表论文的发表时间)