期刊文献+

一种改进的机动目标拦截算法 被引量:4

An Improved Algorithm for Maneuverable Target Interception
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摘要 机动目标的拦截问题可以用"追逃游戏"模型描述,考虑追击者的惯性、控制量有限等动力学特征时,拦截位置和控制量的确定是非常困难的.针对平面机动目标的拦截问题,以机器人拦截足球为模型,提出了一种改进的拦截算法——改进的"预测-规划-执行"法,通过预测机动目标的运动轨迹,提出了一种快速简便地确定粗略拦截位置的试探方法,在此基础上,再确定机器人的控制速度和精确拦截位置,控制机器人朝拦截位置运动.最后,给出了仿真计算结果,并应用于机器人足球比赛,仿真计算表明,算法可以准确有效地拦截运动目标. Interception of a maneuverable target can be described as a "pursuit-evasion game" model. It is difficult to determine the position of the engagement in respect to the dynamic characters of the pursuer, such as inertia and limited control. Based on the model of a robot intercepting a soccer ball in a robot soccer competition, an improved "prediction, planning and execution" algorithm is proposed for planar maneuverable target interception. Through predicting a moving target's trajectory and probing a possible engagement position, a quick and convenient approach to calculating the interception location is proposed, and then a controlling strategy for the robot and an accurate engagement position are determined to drive the robot to the engaged location in given time. Finally, simulation results are obtained from the application of the algorithm to robot soccer games. They demonstrate that the algorithm can accurately and effectively intercept the maneuverable target.
出处 《中南林业科技大学学报》 CAS CSCD 北大核心 2008年第5期136-139,共4页 Journal of Central South University of Forestry & Technology
基金 中南林业科技大学人才引进基金资助(项目编号:06Y409)
关键词 控制理论与应用 机器人 机动目标 拦截 预测 规划 control theory and applications robot maneuverable target interception prediction planning
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参考文献6

  • 1[1]Vladimir Turetsky,Josef Shinar.Missile guidance laws based on pursuit-evasion game formulations[J].Automatica,2003(39):607-618.
  • 2[2]Mehrandezh M,Sela M N,Fenton R G.Robotic interception of moving objects using ideal proportional navigation guidance technique[J].Robotics and Autonomous Systems.1999 (28):285-310.
  • 3[3]Kimura H,Mukai N,Slotine J E.Adaptive visual tracking and Gaussian network algorithm for robotic catching[J].ASME,Advances in Robust and Nonlinear Control System,1992(43):67-74.
  • 4[4]Zarchan P.Tactical and strategic missile guidance[J].Progress in Astronautics and Aeronautics Reston,Washington DC,AIAA,Inc.,1990(124).
  • 5张友安,胡云安,林涛.导弹制导的鲁棒几何方法[J].控制理论与应用,2003,20(1):13-16. 被引量:14
  • 6王湘中,喻寿益.基于改进进化策略的足球机器人最优控制[J].哈尔滨工业大学学报,2005,37(7):969-970. 被引量:1

二级参考文献13

  • 1马辰威,刘巍,张承,韩光胜.基于遗传算法的足球机器人控制参数优化[J].哈尔滨工业大学学报,2004,36(7):920-922. 被引量:5
  • 2王湘中 喻寿益.适用于高维优化问题的改进进化策略[J].控制理论与应用,2005,22(4):798-792.
  • 3HA I J, HUR J S, KO M S, et al. Performance analysis of PNG laws for randomly maneuvering targets [ J]. IEEE Trans on Aerospace and Electronic System, 1990, 26(5) :713 -721.
  • 4CHO H, RYOO C K. Closed-form optimal guidance law for missiles of time-varying velocity [J]. J of Guidance, Control, and Dynamics, 1996,19(5): 1017 - 1022.
  • 5KIMKB, KIMMJ, KWONWH. Receding horizon guidance laws with no information on the time-to-go [J]. J of Guidance, Control,and Dynamics, 2000, 23(2):193- 199.
  • 6GERARD L. Guidance algorithms design: a nonlinear inverse approach [J]. J of Guidance, Control, and Dynamics, 1998,21(5):742 - 746.
  • 7HA J J, CHONG S. Design of a CLOS guidance law via feedback linearization [ J]. IEEE Trans on Aerospace and Electronic System,1992, 28(1): 51 - 62.
  • 8BEZICK S, RUSNAK I, GRAY W S. Guidance of a homing missile via nonlinear geometric control methods [J]. J of Guidance, Control, and Dynamics, 1995,18(3): 441-448.
  • 9GUO C Y, CHIOU Y C. Geometric analysis of missile guidance command[J]. IEE Proc-Control Theory and Applications, 2000, 147(2): 205-211.
  • 10ZHOU Di, MU Chundi, XU Wenli. Adaptive sliding-mode guidance of a homing missile [J]. J of Guidance, Control, and Dynamics,1999, 22(4): 589 - 594.

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