Design of Non-linear Dynamic Inversion UAV with QFT

摘要：

　　Flight control system of UAV (Unmanned Aerial Vehicle) has limitations with non-linear dynamic inversion method.This paper introduces QFT based on non-linear dynamic inversion method,for avoiding model errors during existing non-linear function offset,QFT theory is presented firstly,then UAV model is established using non-linear dynamic inversion method,definituding the range of errors and system performance requirements,flight control system of UAV is designed with QFT,the simulating curves show that system has robustness stability.

关键词： unmanned aerial vehicle(UAV) non-linear dynamic inversion quantitative feedback theory (QFT) robust

作者: LI Jie ZHANG Jie XU zhihui

作者单位: The First Aeronautical Institute of Air Force,Xinyang,Henan,China Training office Weinan Teacher University,Weinan,Shanxi,China The 95168 unit of PLA,Guangzhou,Guangdong,China

会议类型: 国际会议

会议名称: 2012 International Conference on Intelligent System and Applied Material(2012智能系统与应用材料国际会议)(GSAM2012)

会议地点: 太原

会议语种:英文

页码: 676-679

在线出版日期: 2012-01-13（万方平台首次上网日期，不代表论文的发表时间）