多导弹分布式协同制导与控制方法

孙雪娇; 周锐; 吴江; 陈哨东

多导弹分布式协同制导与控制方法

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

基金项目: 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）

详细信息

中图分类号: TJ765.3
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出版历程
- 收稿日期: 2013-03-14
- 网络出版日期: 2014-01-20

Distributed cooperative guidance and control for multiple missiles

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

摘要

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.
- 协同制导 /
- 网络同步 /
- 切换控制 /
- 自动驾驶仪
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.
- coordinated attack /
- network synchronization principle /
- switching control /
- autopilot

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参考文献(9)

[1]	王建青, 李帆, 赵建辉, 等.多导弹协同制导律综述[J].飞行力学, 2011, 29(4):6-10 Wang Jianqing, Li Fan, Zhao Jianhui, et al.Summary of guidance law based cooperative attack of multi-missile method[J].Flight Dynamics, 2011, 29(4):6-10(in Chinese)
[2]	Jeon I S, Lee J I, Tahk M J.Impact-time-control guidance law for anti-ship missiles[J].IEEE Transactions on Control Systems Technology, 2006, 14(2):260-266
[3]	赵世钰.多飞行器协同制导方法研究[D].北京:北京航空航天大学, 2009 Zhao Shiyu.Multi-vehicle cooperative guidance law study[D].Beijing:Beijing University of Aeronautics and Astronautics, 2009(in Chinese)
[4]	Zhao Shiyu, Zhou Rui.Cooperative guidance for multimissile salvo attack[J].Chinese Journal of Aeronautics, 2008, 21(6): 533-539
[5]	彭琛, 刘星, 吴森堂, 等.多弹分布式协同末制导时间一致性研究[J].控制与决策, 2007, 25(10):1557-1562 Peng Chen, Liu Xing, Wu Sentang, et al.Consensus problems in distributed cooperative terminal guidance time of multi-missiles[J].Control and Decision, 2007, 25(10):1557-1562(in Chinese)
[6]	邹丽, 丁全心, 周锐.异构多导弹网络化分布式协同制导方法[J].北京航空航天大学学报, 2010, 36(12):1432-1435 Zou Li, Ding Quanxin, Zhou Rui.Distributed cooperative guidance for multiple heterogeneous networked missiles[J].Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(12) :1432-1435(in Chinese)
[7]	张友安, 马国欣, 王兴平.多导弹时间协同制导:一种领弹-被领弹策略[J].航空学报, 2009, 30(6):1109-1118 Zhang Youan, Ma Guoxin, Wang Xingping.Time-cooperative guidance for multi-missiles:a leader-follower strategy[J].Acta Aeronautica et Astronautica Sinica, 2009, 30(6):1109-1118(in Chinese)
[8]	Lawrence D A, Kelly J H, Evers J H.Gain scheduled missile autopilot design using a control signal interpolation technique[R].AIAA-98-4418, 1998
[9]	迟学谦, 王青, 侯砚泽.倾斜转弯导弹的鲁棒跟踪切换控制[J].上海交通大学学报, 2011, 45(2):284-289 Chi Xueqian, Wang Qing, Hou Yanze.Robust model following switching control of BTT missile[J].Journal of Shanghai Jiaotong University, 2011, 45(2):284-289(in Chinese)