Robust Formation Flight Control System Design For Multi-UAVs

摘要：

Based on the wind tunnel test data of actual unmanned aircraft, the dynamics and kinematics nonlinear model is established. Firstly, the robustness control system of a single unmanned aircraft is designed by the stochastic robustness analysis and design method. Secondly, based on the inner loop stability of single aircraft, a formation flight control method based on the Leader-follower model in three dimensions is proposed. Finally, simulations results of some type of unmanned aircraft formation flight trajectory show the effectiveness of the proposed method.

关键词： Stochastic robustness analysis and design Flight control Formation control

作者: QIU Qi WU Sen Tang

作者单位: School of Automation Science and Electrical Engineering, Beihang University, Beijing 100191, P. R. China

会议类型: 国际会议

会议名称: The 31st Chinese Control Conference(第三十一届中国控制会议)

会议地点: 合肥

会议语种:英文

页码: 4617-4621

在线出版日期: 2012-07-01（万方平台首次上网日期，不代表论文的发表时间）