期刊文献+

基于鲁棒最优方法的无人机动态投影控制 被引量:4

UAV dynamic projective control method based on robust and optimal theories
下载PDF
导出
摘要 以某型大展弦比无人机为研究对象,设计了基于鲁棒最优理论和动态投影方法的补偿控制器。首先采用鲁棒伺服线性二次型调节器方法,通过全状态反馈构建满足最优性能指标的参考系统,然后采用输出反馈和动态补偿器替代全状态反馈,重构出具备参考系统全部最优特征结构的动态投影控制系统。重点阐述了通过动态投影控制方法进行系统极点配置的具体步骤,并分析了动态补偿器的自由矩阵参数对系统稳定性的影响。仿真结果表明,与常规比例-积分-微分控制方法相比,所设计的动态投影控制系统具有更强的稳定性与更好的瞬态响应特性。 A control method for a unmanned aerial vehicle having large aspect ratio is proposed. A compen- sative controller is designed based on dynamic projective control method and robust optimal theories. Firstly, a closed loop system of robust servomechanism linear quadratic regulator method is obtained by state feedback which is considered as a reference system. Then a method of dynamic projective control is adopted to reconstruct the whole characteristic structure of the reference system by output feedback and a dynamic compensator. The concrete steps of the pole placement by dynamic projective control method are expounded. Also, the influence of var ying the free matrix of dynamic compensator is discussed. The result of simulation shows that the designed control system has remarkable transient performance and stability which is much better than ordinary control method.
出处 《系统工程与电子技术》 EI CSCD 北大核心 2015年第9期2088-2095,共8页 Systems Engineering and Electronics
基金 航空科学基金(20125852057) 江苏省普通高校研究生科研创新计划(CXLX12_0159)资助课题
关键词 无人机控制 动态补偿器 鲁棒最优控制 投影控制 unmanned aerial vehicle (UAV) control dynamic compensator robust-optimal control projective control
  • 相关文献

参考文献12

  • 1罗云林,尹楚雄.基于模糊径向基神经网络的小型无人机控制系统研究[J].中国民航飞行学院学报,2014,25(1):46-49. 被引量:4
  • 2黄开,黄一敏,孙春贞.无人机发动机停车应急着陆纵向控制律研究[J].电子设计工程,2014,22(16):8-10. 被引量:1
  • 3张民,陈欣,陆宇平,臧月进.基于μ综合方法的空空导弹鲁棒驾驶仪设计[J].上海交通大学学报,2011,45(3):418-422. 被引量:4
  • 4Wise A K, Lavretsky E. Robust and adaptive control of X-45A J-UCAS: a design trade study[C]// Proc. of the 18th Interna- tional Federation of Automatic Control ( IFAC) World Con gress, 2011:6555 - 6560.
  • 5Wise A K. Verifiable adaptive flight control: UCAV and aerial refueling[C]//Proc, of the AIAA Guidance, Navigation and Control Conference and Exhibit, 2008 : 1 - 26.
  • 6Wise A K, Nguyen T. Optimal disturbance rejection in missile autopilot design using projective controls[J]. Control Systems, 1992, 12(5): 43-49.
  • 7Wise A K. Comparison of six robustness tests evaluating missile autopilot robustness to uncertain aerodynamics[J]. Journal of Guidance Control and Dynamics, 1992, 15(4): 861-870.
  • 8Nam S W, Veillette R J. Reduced-order controller design using projective controls with output feedback reference [C]//Proc. o f the 32nd IEEE Conference on Decision and Control, 1993: 2925 -2926.
  • 9Medanic J V. Nonlinear output feedback controller design by projective controls[C]//Proc, of the 42nd IEEE Conference on Decision and Control, 2003.- 5185 - 5190.
  • 10吴森堂,费玉华.飞行控制系统[M].2版.北京:北京航空航天大学出版社,2013.

二级参考文献14

  • 1沈明辉,陈磊,吴瑞林,周伯昭.大气层内动能拦截弹的变增益鲁棒姿控系统设计研究[J].宇航学报,2007,28(3):562-565. 被引量:5
  • 2林叶锦,任光.遗传优化的径向基函数船舶模糊控制器[J].控制理论与应用,2004,21(6):1036-1040. 被引量:12
  • 3张明廉.飞行控制系统[M].北京:国防工业出版社,1986..
  • 4Brinkman K,Visser H G. A closed-loop guidance approximation for the turn-back maneuver after engine failure during climb- out, AIAA-2007-233 [R]. Reno, Nevada: AIAA 45th Aerospace Sciences Meeting and Exhibit ,2007:8-1 1.
  • 5ENG P,MEJIAS L. Automating human thought processes for a UAV forced landing[J]. Journal of Intelligent and Robotic Systems, 2010 ( 57 ) :329-349.
  • 6Jett B W. The Feasibility for Turnback from a Low Altitude Engine Failure During The Takeoff Climb-out Phase, AIAA- 82-0406 [R]. Orlando, Florida:AIAA 20th Aerospace Sciences Meeting, 1982:11-14.
  • 7Shapira I,Ben-Asher J. Range maximization for emergency landing after engine cutoff[J]. Journal of Aircraft. September- October, 2005,42 ( 5 ): 1296-1306.
  • 8李欣.小型无人机简化配置控制律设计技术研究[D].南京南京航空航天大学.2011.
  • 9刘建伟,朱敏.一种对RBF网络中聚类算法的改进[J].微计算机信息,2009,25(15):73-74. 被引量:1
  • 10张民,陈欣,陆宇平.基于改进PSO算法的导弹控制参数优化[J].南京航空航天大学学报,2009,41(4):445-449. 被引量:6

共引文献17

同被引文献15

引证文献4

二级引证文献38

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部