北京航空航天大学学报 ›› 2014, Vol. 40 ›› Issue (1): 120-124.

• 论文 • 上一篇    下一篇

多导弹分布式协同制导与控制方法

孙雪娇1, 周锐1, 吴江1, 陈哨东2   

  1. 1. 北京航空航天大学 飞行器控制一体化技术重点实验室, 北京 100191;
    2. 洛阳电光设备研究所 火力控制技术国防科技重点实验室, 洛阳 471009
  • 收稿日期:2013-03-14 出版日期:2014-01-20 发布日期:2014-01-22
  • 基金资助:
    国家自然科学基金资助项目(61273349,61175109);航空科学基金资助项目(2011ZC13001)

Distributed cooperative guidance and control for multiple missiles

Sun Xuejiao1, Zhou Rui1, Wu Jiang1, Chen Shaodong2   

  1. 1. Science and Technology on Aircraft Control Laboratory, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;
    2. Key Laboratory of National Defense on Fire Control Technology, Luoyang Institute of Electro-optical Equipment, Luoyang 471009, China
  • Received:2013-03-14 Online:2014-01-20 Published:2014-01-22

摘要: 针对多枚导弹三维空间协同攻击机动目标要求,提出了一种多导弹分布式协同制导与控制方法.基于网络同步原理设计了一种多导弹三维位置同步算法,将目标视作领弹,与攻击导弹组成“领弹-从弹”的拓扑结构,实现了导弹对目标的协同攻击引导.同步算法给出了惯性坐标系导弹3个方向速度的指令,基于坐标变换将其转化为自动驾驶仪可以跟踪的速度及弹道倾角指令.基于切换控制方法设计了导弹自动驾驶仪,实现了多导弹协同制导与控制的闭环仿真.仿真结果验证了该方法的有效性.

Abstract: A kind of multi-missile distributed cooperative guidance and control method for coordinated attacking maneuvering target in three-dimensional space was proposed based on the principle of network synchronization. A kind of suitable three-dimensional position synchronization algorithm was designed. The target was seen as a leader and made up a "leader-followers" topology with missiles. The synchronization algorithm gave out the speed commands of each missile in three directions. Velocity and trajectory angle commands which can be tracked by autopilot were got based on the coordinate transformation theory. Switching control method was used in designing autopilot, which realized closed loop simulation. The simulation results demonstrate the effectiveness of this method.

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