Nonlinear Flight Control Design of a Combat Flying Wing with High Aspect-ratio

摘要：

　　Without horizontal and vertical stabilizers,a combat flying wing with high aspect-ratio has strong nonlinear dynamic feature,and use multiple control surfaces to realize multi-axis controls.Its flight control system must be able to handle nonlinearity and control redundancy problems.The six-degree-of-freedom (6-DOF) nonlinear dynamics model of the flying wing is developed.Utilizing nonlinear dynamic inversion theory and control allocation technique,an advanced flight control system for the tracking of trajectory is designed.Numerical simulation results show that this flight control system could comparatively better solve the nonlinear contral problem of such aircraft types.

关键词： Flying wing Aircraft Dynamic inversion Control allocation Trajectory Flight control Nonlinear modeling Simulation

作者: Wang Lei Wang Lixin

作者单位: School of Aeronautic Science and Engineering Beihang University Beijing, China

会议类型: 国际会议

会议名称: 2012 2nd International Conference on Computer Application and System Modeling(2012第二届计算机应用与系统建模国际会议)(ICCASM-2012)

会议地点: 沈阳

会议语种:英文

页码: 825-827

在线出版日期: 2012-07-27（万方平台首次上网日期，不代表论文的发表时间）