Research on ANN Dynamic Inversion Control of UAV

摘要：

　　The paper proposes a method to design AANN dynamic inversion controller through online ANN compensating inversion error.It mainly aims at evident shortage of dynamic inversion controller of UAV.A single hidden layer ANN structure is constructed and the stability of the whole closed loop system is proved.Also the stable adjustment arithmetic of online ANN weight is proposed.The robustness,the adaptability to fault and the response capability to actuator delay time of the scheme are verified by simulation.It is also proved that the online ANN has improved the performance of dynamic inversion controller well.It has important reference value for designing advanced flight control systems of UAV.

关键词： Dynamic inversion controller UnmaANNed aerial vehicle (UAV) Neural network (ANN) Stability Single Hidden Layer (SHL)

作者: CHEN Weilun XIN Gongcai

作者单位: Department of Instrument and Electric Engineering The First Aeronautical Institute of Air Force Xinyang,Henan,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: 1353-1357

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）