On New UAV Formation Flight Control System

摘要：

Combining Kalman filter with PID controller is applied to design UAV (Unmanned Air Vehicles)formation flight control system.It contains Kalman&PID controllers of speed and pitch angle for UAV.According to characteristic of UAV formation flight ,the PID parameters were adjusted to realize control stability of UAV in formation flight.The simulation results verify the validity and feasibility of the proposed method.And Kalman&PID controller is better than traditional PID controller.

作者: ZHANG Peng LIU Zhendong

作者单位: The Key Auto-control Laboratory,Heilongjiang University,Harbin 150080,P.R.China

会议类型: 国际会议

会议名称: The 30th Chinese Control Conference(第三十届中国控制会议)

会议地点: 烟台

会议语种:英文

页码: 1-4

在线出版日期: 2011-07-01（万方平台首次上网日期，不代表论文的发表时间）