期刊文献+

基于SMDO的滑模控制器设计及其在导弹上的应用 被引量:14

Design of Sliding Mode Controller Based on SMDO and Its Application to Missile Control
原文传递
导出
摘要 提出了一种基于滑模干扰观测器(SMDO)的滑模控制器(SMC)设计方法。针对一类级联多输入多输出(MI-MO)非线性系统,根据奇异摄动原理将其分为内、外回路分别进行控制器设计。以外回路为例,分析了传统基于饱和函数的滑模控制的鲁棒性,针对其在面临干扰时鲁棒性较差的问题,在名义滑模控制律的基础上设计了基于超扭曲算法的SMDO以实现对干扰的估计和补偿。将该方法应用于导弹控制系统的设计中,通过仿真表明,基于SMDO的滑模控制器(SMDO-SMC)有效提高了控制系统的鲁棒性和性能。 A sliding mode controller (SMC) design approach based on the sliding mode disturbance observer (SMDO) is proposed. A class of cascade multiple-input multiple-output (MIMO) nonlinear system is separated into outer and inner loops based on the singular perturbation principle, and the controllers are designed in the two loops respectively. The robustness of the traditional saturation-function-based sliding mode controller is analyzed in the outer loop, and it is found to be weak in the presence of disturbances. To overcome this problem, together with the nominal sliding mode control law, SMDOs based on the super-twisting algorithm are designed to estimate and compensate for disturbances. Finally, the approach is applied to a missile control system design. The simulation results demonstrate that SMDO-based sliding mode controller (SMDO- SMC) effectively improves both the robustness and control performance of the control system.
出处 《航空学报》 EI CAS CSCD 北大核心 2011年第5期873-880,共8页 Acta Aeronautica et Astronautica Sinica
关键词 滑模干扰观测器 滑模控制 超扭曲算法 导弹 鲁棒控制 sliding mode disturbance observer sliding mode control super-twisting algorithm missiles robust contro
  • 相关文献

参考文献13

  • 1Young K D, Utikin V I, Ozgtiner U. A control engineer's guide to sliding mode control[J]. IEEE Transactions on Control System Technology, 1999, 7(3): 328-342.
  • 2Shtessel Y B, Shkolnikov I A, Brown M D J. An asymptotic second-order smooth sliding mode control[J]. Asian Journal of Control, 200a, 5(4), 498-503.
  • 3Xu H J, Mirmirani M D, Ioiannou P A. Adaptive sliding mode control design for a hypersonic flight vehicle[J].Journal of Guidance, Control, and Dynamics, 2004, 27 (5) : 829-838.
  • 4Hess R A, Wells S R. Sliding mode control applied to reconfigurable flight control design[J]. Journal of Guidance, Control, and Dynamics, 2003, 26(3): 452-462.
  • 5丁世宏,李世华.空间飞行器姿态的有限时间跟踪控制方法[J].航空学报,2007,28(3):628-633. 被引量:9
  • 6Shtessel Y B, Burlington J, Banda S. Multiple timescale flight control using reconfigurahle sliding modes[J]. Journal of Guidance, Control, and Dynamics, 1999, 22 (6) .873-883.
  • 7Huang J, Lin C F. Application of sliding mode control to bank-to-turn missile systems [C]// Proceedings of 1st IEEE Regional Conference on Aerospace Control Systems. 1993: 569-573.
  • 8Hall C E, Shtessel Y B. Sliding mode disturbance observer-based control for a reusable launch vehiele[J].Journal of Guidance, Control, and Dynamics, 2006, 29(6) : 1315- 1328.
  • 9Slotine J J E, Coetsee J A. Adaptive controller synthesis for nonlinear systems [J].International Journal of Control, 1986, 43(6): 1631-1651.
  • 10Naidu D S, Calise A J. Singular perturbations and time scales in guidance and control of aerospace systems: a survey[J]. Journal of Guidance, Control, and Dynamics, 2001, 24(6)1057-1070.

二级参考文献21

共引文献66

同被引文献105

引证文献14

二级引证文献78

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