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一种基于变结构控制的鲁棒制导算法设计 被引量:8

A Robust Guidance Algorithm Design Using Variable Structure Control
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摘要 针对平面拦截问题 ,选择导弹和目标之间的相对速度矢量与导弹 -目标视线之间的夹角 (称为相对航向误差角 )作为将要被控制到零的输出。将与目标运动的加速度和速度方位信息有关的量视为干扰量 ,基于变结构控制理论设计了一种鲁棒制导算法。该制导算法不需要得到目标精确的加速度和速度方位信息 ,因而更便于工程实现。仿真结果表明 。 For the case of planar interception, the so called relative heading error angle between the relative velocity vector and the LoS (Line of Sight) is chosen as the output to be controlled to zero. The terms related to the acceleration and velocity heading angle of target are regarded as disturbances, a robust guidance algorithm design is given by using the theory of variable structure control. The proposed guidance algorithm needs no accurate information on the acceleration and velocity heading angle of the target, and hence is more convenient for practical implementation. The simulation results show that the algorithm has strong robustness to the maneuvering of the target.
出处 《系统工程与电子技术》 EI CSCD 北大核心 2001年第4期61-63,共3页 Systems Engineering and Electronics
基金 航空科学基金资助课题 !(99D12 0 0 1)
关键词 制导 鲁棒控制 算法 变结构控制 Guidance\ \ Robase control\ \ Algorithm
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参考文献4

  • 1[1]Ha J J, Chong S. Design of a CLOS Guidance Law via Feedback Linearization. IEEE Trans. on Aerospace and Electronic System, 1992, 28(1).
  • 2[2]Bezick S, Rusnak I, Gray W S. Guidance of a Homing Missile via Nonlinear Geometric Control Methods. Journal of Guidance, Control, and Dynamics, 1995, 18(3).
  • 3[3]Gerard L. Guidance Algorithms Design: A Nonlinear Inverse Approach. Journal of Guidance, Control, and Dynamics, 1998, 21(5).
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同被引文献33

  • 1李静,左斌,胡云安.基于变结构控制理论的导弹平滑导引律研究[J].海军航空工程学院学报,2007,22(3):313-316. 被引量:7
  • 2赵永涛,胡云安,王瑛.超视距舰空导弹爬升段弹道设计[J].海军航空工程学院学报,2007,22(5):522-526. 被引量:1
  • 3周荻,胡恒章,胡国辉.一种自适应变结构制导律[J].宇航学报,1996,17(4):9-13. 被引量:19
  • 4高为炳.变结构控制的理论及设计方法.北京:科学出版社,1998.
  • 5BABU K R, SARMAH J G. SWAMY K N. Switched bias proportional navigation for homing guidance against highly maneuvering target[J]. Journal of Guidance, Control and Dynamics, 1994,17(6):!357- 1363.
  • 6BABU K R, SARMAH J G, SWAMY K N. Two variable structure homing guidance schemes with and without target maneuver estimation[R]. AIAA-94-3566, 1994.
  • 7[1]ZHOU D.Adaptive Sliding-Mode Guidance of a Homing Missile[J].Journal of Guidance,Control and Dynamics,1999,22(4):589-594.
  • 8[5]FU-KUANG YEH,HSIUAN-HAU CHIEN,LI-CHEN FU.Design of optimal midcourse guidance sliding-mode control for missiles with TVC[J].IEEE transactions on aerospace and electronic systems,2003,39(3):824-837.
  • 9[8]韩京清.拦截问题中的导引律[M].北京:国防工业出版社,1997.
  • 10[1]Bezick S, Rusnak I, and Gray W S. Guidance of a Homing Missile via Nonlinear Geometric Control Methods[J]. oumal of Guidance, Control, and Dynamics, 1995,18(3): 441-448

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