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基于非线性干扰观测器的超机动飞行轨迹线性化控制 被引量：2

Nonlinear Disturbance Observer-Enhanced Trajectory Linearization Control for Super-Maneuverable Flight
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摘要 针对非线性系统存在建模误差和外界干扰等不确定因素问题,提出一种基于非线性干扰观测器(Nonlinear Disturbance Observer,NDO)在线补偿的轨迹线性化控制(Trajectory Linearization Control,TLC)方法。设计非线性干扰观测器,对不确定因素进行估计,NDO的输出用以设计新的补偿控制律,与TLC方法相结合来消除不确定因素的影响。以赫布斯特机动过程为例进行飞行仿真,并与单纯采用TLC方法的控制性能进行对比。仿真表明,系统能较好地跟踪姿态角指令,有良好的鲁棒性。 Considering the uncertainties, such as errors in modeling and external disturbances, existed in nonlinear systems, a nonlinear disturbance observer （NDO） is used to estimate the uncertainties, and then its output is integrated with the output of Trajectory Linearization Control （TLC）, as a new control law to cancel the unknown term. So, nonlinear systems will attain to excellent performance. Herbst maneuver is method, and for comparison, the herbst maneuver is also simulated the method is effective and has better robustness. simulated for an aircraft mathematics model using this using only TLC controller. Simulation＇results show that
作者 王芳 钱承山
机构地区 中国电子科技集团公司第 南京信息工程大学信息与控制学院
出处 《兵工自动化》 2010年第7期59-62,共4页 Ordnance Industry Automation
关键词 轨迹线性化控制 非线性干扰观测器 超机动 trajectory linearization control nonlinear disturbance observer super-maneuverable
分类号 TP273 [自动化与计算机技术—检测技术与自动化装置]
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参考文献8

  • 1Mickle M.C.and Zhu J.J,A Nonlinear Roll-Yaw Missile Autopilot Based on Plant Inversion and PD-Spectral Assignment[A].Proceedings of the 37th IEEE Conference on Decision & Control[C] ,Tampa,Florida,1998:4679-4684.
  • 2Mickle M.C.and Zhu J.J.,Bank-to-turn roll-yaw-pitch autopilot design using dynamic nonlinear inversion and PD-eigenvalue assignment[A].Proceedings of the American Control Conference[C] ,Chicago,Illinois,2000:1359-1364.
  • 3Liu Y,Wu X and Zhu J.J.et al,Omni-Directional mobile robot controller design by Trajectory Linearization[A].Proceedings of the American Control Conference[C] ,Denver,Colorado,2003:3423-3428.
  • 4Zhu J.J.,Banker D.and Hall C.E.,X-33 Ascent Flight Controller Deign by Trajectory Linearization A Singular Perturbation Approach[A].Proceedings of AIAA GN&C Conference[C] ,Denver,Colorado,2000:1-19.
  • 5朱秋芳,姜长生,朱亮,谢祥华.采用TLC方法的超机动飞行控制系统设计[J].南京航空航天大学学报,2007,39(3):379-383. 被引量：6
  • 6Barmish BR and Leimann G,On Ultimate Boundedness Control of Uncertain Systems in the Absence of Matching Assumptions[J].IEEE Trans.on Automatic Control,1982,27(1):153-158.
  • 7Kahlil H.K.,Nonlinear System 2th ed,Prentice-Hall,Upper Saddle River,NJ,1996.
  • 8朱亮,姜长生,方炜.基于非线性干扰观测器的不确定非线性系统鲁棒轨迹线性化控制[J].信息与控制,2006,35(6):705-710. 被引量：8

二级参考文献16

  • 1Mickle M C,Zhu J J.Bank-to-turn roll-yaw-pitch autopilot design using dynamic nonlinear inversion and PD-eigenvalue assignment[A].Proceedings of the American Control Conference[C].Piscataway,NJ,USA:IEEE,2000.1359～1364.
  • 2Liu Y,Wu X F,Zhu J J,et al.Omni-directional mobile robot controller design by trajectory linearization[A].Proceedings of the American Control Conference[C].Piscataway,NJ,USA:IEEE,2003.3423 ～ 3428.
  • 3Zhu J J,Banker B D,Hall C E.X-33 ascent flight control design by trajectory linearization-A singular perturbation approach[A].AIAA Guidance,Navigation,and Control Conference and Exhibit[C].Reston,USA:AIAA,2000.1 ～19.
  • 4Bevacqua T,Best E,Huizenga A,et al.Improved trajectory linearization flight controller for reusable launch vehicles[A].42nd AIAA Aerospace Sciences Meeting and Exhibit[C].Reston,USA:AIAA,2004.1 ～16.
  • 5Zhu J J,Mickle M C.Synthesis of time-varying bandwidth filtersbased on all-pole LTI prototypes[A].Proceedings of the 1998American Control Conference[C].Evanston,IL,USA:American Automatic Control Council,1998.2889～ 2894.
  • 6Chen W H,Balance D J,Gawthrop P J,et al.Nonlinear disturbance observer for robotic manipulators[J].IEEE Transactions on Industrial Electronics,2000,47(4):932 ～938.
  • 7Chen W H.Nonlinear disturbance observer enhanced dynamic inversion control of missiles[J].Journal of Guidance,Control,and Dynamics,2003,26(1):161 ～166.
  • 8Barmish B R,Leimann G.On ultimate boundedness control of uncertain systems in the absence of matching assumption[J].IEEE Transactions on Automatic Control,1982,27 (1):153 ～158.
  • 9Kahlil H K.Nonlinear Systems[M].New Jersey,USA:Prentice-Hall,2002.
  • 10Mickle M C,Zhu J J.A nonlinear roll-yaw missile autopilot based on plant inversion and PD-spectral assignment[C]// Proceedings of the 37th IEEE Conference on Decision & Control.Tampa:IEEE,1998:4679-4684.

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二级引证文献5

兵工自动化
2010年 第7期

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