基于MPSC和CPN制导方法的协同制导律

李新三; 汪立新; 王明建; 闫循良; 刘国辉; 丁邦平

doi:10.13700/j.bh.1001-5965.2015.0592

基于MPSC和CPN制导方法的协同制导律

doi: 10.13700/j.bh.1001-5965.2015.0592

1.
火箭军工程大学控制工程系, 西安 710025
2. 火箭军工程大学士官学院, 青州 262500

基金项目: 国家自然科学基金（61203354）

详细信息

作者简介:
李新三,男,博士,讲师。主要研究方向:导航制导与仿真技术。Tel.:18292855105,E-mail:xinsan_2006@163.com;汪立新,男,博士,教授,博士生导师。主要研究方向:导航制导与仿真。Tel.:029-84741536,E-mail:281167393@qq.com

通讯作者:
汪立新,Tel.:029-84741536,E-mail:281167393@qq.com

中图分类号: V444
计量
- 文章访问数: 1052
- HTML全文浏览量: 76
- PDF下载量: 999
- 被引次数: 0
出版历程
- 收稿日期: 2015-09-10
- 网络出版日期: 2016-09-20

Cooperative guidance law based on MPSC and CPN guidance method

1.
Department of Control Engineering, Rocket Military Engineering University, Xi'an 710025, China
2. Petty Officer Academy, Rocket Military Engineering University, Qingzhou 262500, China

Funds: National Natural Science Foundation of China (61203354)

摘要

摘要: 针对带有末端攻击角度约束的多导弹协同制导问题，运用模型预测扩展控制（MPSC）和协同比例制导（CPN），设计了一种满足末端攻击角度约束的多导弹协同次优制导律。阐述了MPSC制导方法的基本理论，详细给出了控制量表达式以二次形式近似时MPSC制导律的设计过程。采用CPN对MPSC制导方法的初始控制量进行猜测，并确定协同攻击时间。仿真时考虑两枚导弹对地面静止目标进行协同攻击。仿真结果表明，两枚导弹攻击时间偏差和末端攻击角度偏差均可控制在给定范围内，即本文所设计的制导律在实现多导弹协同攻击时，还可以很好地满足末端攻击角度约束。
- 制导 /
- 协同制导 /
- 模型预测扩展控制(MPSC) /
- 攻击角度约束 /
- 攻击时间约束
Abstract: Cooperative guidance of multiple missiles satisfying terminal impact angle constraints is considered. A suboptimal guidance law is presented using the recently proposed model predictive spread control (MPSC) method and cooperative proportional navigation (CPN) guidance law. The basic principle of the MPSC method is given and the MPSC guidance law is designed on the assumption that the control is considered to be a function of quadratic formulation. The MPSC method requires a control history to begin the algorithmic sequence. Guess control history is computed using the CPN technique, subject to constraint on impact time. A stationary target is attacked by two missiles in the simulation. It is observed from the simulation that the impact time error and terminal impact angle error are within the specified convergence tolerance. The terminal impact angle constraint is well satisfied in salvo attack scenario.
- guidance /
- cooperative guidance /
- model predictive spread control (MPSC) /
- impact angle constraint /
- impact time constraint

HTML全文

参考文献(20)

[1]	LEE J I,JEON I S,TAHK M J.Guidance law using augmented trajectory-reshaping command for salvo attack of multiple missiles[C]//UKACC International Control Conference 2006.Glasgow:UKACC,2006:766-771.
[2]	邹丽,孔繁峨,周锐,等.多导弹分布式自适应协同制导方法[J].北京航空航天大学学报,2012,38(1):128-132.ZOU L,KONG F E,ZHOU R,et al.Distributed adaptive cooperative guidance for multi-missile salvo attack[J].Journal of Beijing University of Aeronautics and Astronautics,2012,38(1):128-132(in Chinese).
[3]	孙雪娇,周锐,吴江,等.多导弹分布式协同制导与控制方法[J].北京航空航天大学学报,2014,40(1):120-124.SUN X J,ZHOU R,WU J,et al.Distributed cooperative guidance and control for multiple missiles[J].Journal of Beijing University of Aeronautics and Astronautics,2014,40(1):120-124(in Chinese).
[4]	范作娥,于德海,顾文锦.带落角约束和目标机动补偿的三维制导律[J].系统工程与电子技术,2011,33(8):1856-1859.FAN Z E,YU D H,GU W J.Three-dimensional guidance law with impact angle constraint and maneuvering target compensation[J].Systems Engineering and Electronics,2011,33(8):1856-1859(in Chinese).
[5]	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.
[6]	LEE J I,JEON I S,TAHK M J.Guidance law to control impact time and angle[J].IEEE Transactions on Aerospace and Electronic Systems,2007,43(1):301-310.
[7]	张友安,马培蓓.带有攻击角度和攻击时间控制的三维制导[J].航空学报,2008,29(4):1021-1026.ZHANG Y A,MA P B.Three-dimensional guidance law with impact angle and impact time constraints[J].Acta Aeronautica et Astronautica Sinica,2008,29(4):1021-1026(in Chinese).
[8]	PADHI R,KOTHARI M.Model predictive static programming:A computationally efficient technique for suboptimal control design[J].International Journal of Innovative Computing,Information and Control,2009,5(2):399-411.
[9]	DWIVEDI P N,BHATTACHARYA A,PADHI R.Suboptimal midcourse guidance of interceptors for high speed targets with alignment angle constraint[J].Journal of Guidance,Control,and Dynamics,2011,34(3):860-877.
[10]	OZA H B,PADHI R.Impact-angle-constrained suboptimal model predictive static programming guidance of air-to-ground missiles[J].Journal of Guidance,Control,and Dynamics,2012,35(1):153-164.
[11]	MAITY A,OZA H B,PADHI R.Generalized model predictive static programming and its application to 3D impact angle constrained guidance of air-to-surface missiles[C]//2013 American Control Conference(ACC).Piscataway,NJ:IEEE Press,2013:4999-5004.
[12]	CANNON M.Efficient nonlinear model predictive control algorithms[J].Annual Reviews in Control,2004,28(2):229-237.
[13]	SLEGERS N,COSTELLO M.Model predictive control of a parafoil and payload system[J].Journal of Guidance,Control,and Dynamics,2005,28(4):816-821.
[14]	PADHI R,CHAWLA C,DAS P G.Partial integrated guidance and control of interceptors for high-speed ballistic targets[J].Journal of Guidance,Control,and Dynamics,2014,37(1):149-163.
[15]	赵启伦,陈建,董希旺,等.拦截高超声速目标的异类导弹协同制导律[J].航空学报,2016,37(3):936-948.ZHAO Q L,CHEN J,DONG X W,et al.Cooperative guidance law for heterogeneous missiles intercepting hypersonic weapon [J].Acta Aeronautica et Astronautica Sinica,2016,37(3):936-948(in Chinese).
[16]	张爱梅,江加和.基于相互通信的多导弹协同制导[J].应用科技,2015,42(2):1-6.ZHANG A M,JIANG J H.Cooperative guidance for multi-missiles based on mutual communication [J].Applied Science and Technology,2015,42(2):1-6(in Chinese).
[17]	ZHAO S Y,ZHOU R,WEI C.Design and feasibility analysis of a closed-form guidance law with both impact angle and time constraints[J].Journal of Astronautics,2009,30(3):1064-1085.
[18]	HARL N,BALAKRISHNAN S N.Impact time and angle guidance with sliding mode control[J].IEEE Transactions on Control Systems Technology,2012,20(6):1436-1449.
[19]	JEON I S,LEE J I,TAHK M J.Homing guidance law for cooperative attack of multiple missiles[J].Journal of Guidance,Control,and Dynamics,2010,33(1):275-280.
[20]	方研,马克茂,陈宇青.带有攻击角度和时间约束的协同制导律设计[J].系统仿真学报,2014,26(10):2434-2441.FANG Y,MA K M,CHEN Y Q.Cooerative guidance laws with constraints on impact time and terminal angle[J].Journal of System Simulation,2014,26(10):2434-2441(in Chinese).