Research on Intelligent PID Controller for Attitude Control of Small UAV
The attitude control is the base of autonomic flight control for unmanned aerial vehicle (UAV), its flight quality mostly depends on flight control law. The paper presents an intelligent control algorithm for longitudinal attitude control of a small UAV, which is based on building characteristic models in (e-t) information space. A type of intelligent PID controller based on time-domain performance characteristic model is designed. Simulation results illustrate this intelligent PID controller has better performance than general PID controller and the method is suitable for attitude control of UAV.
unmanned aerial vehicle (UAV) attitude control intelligent PID control characteristic model
Xu Hang Song Zong-quan Liu Hui-ming
Department of Aerial Instrument and Electric Engineering, First Aeronautical Institute of Air Force, Xinyang 464000, China
国际会议
第八届国际测试技术研讨会(8th International Symposium on Test and Measurement)
重庆
英文
2373-2376
2009-08-01（万方平台首次上网日期，不代表论文的发表时间）