Robust Dynamic Inversion Control for Near Space Vehicle

摘要：

To the highly nonlinear, significant input-output coupling and remarkable external disturbance of near space vehicle (NSV), a dynamic inversion control method based on H∞ optimal control is proposed. This method combines the robustness of H∞ optimal control theory and nonlinear decoupled control ability of the dynamic inversion control well, so it is possible to achieve highly nonlinear decoupled control for NSV, restrain the effects of external disturbance and realize finite time stability in complicated flight conditions. Therefore, the proposed can provide the longitudinal stability and improves longitudinal flight quality for NSV. Simulation studies demonstrate that the proposed control method is efficient.

作者: Dou Liqian Zong Qun Ji Yuehui

作者单位: College of Electric and Automation Engineering,Tianjin University,Tianjin 300072,China.

会议类型: 国际会议

会议名称: The 3rd International Symposium on Systems and Control in Aeronautics and Astronautics(第三届航空航天系统与控制国际会议 ISSCAA 2010)

会议地点: 哈尔滨

会议语种:英文

页码: 721-726

在线出版日期: 2010-01-08（万方平台首次上网日期，不代表论文的发表时间）