An Adaptive Collaborative Guidance Strategy in Three-Body Engagement

doi:10.7652/xjtuxb201704011

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An Adaptive Collaborative Guidance Strategy in Three-Body Engagement

更新时间：2025-07-09

- An Adaptive Collaborative Guidance Strategy in Three-Body Engagement
- Vol. 51, Issue 4, Pages: 72-78+90(2017)
- 作者机构：
  
  西安交通大学电子与信息工程学院,西安,710049
- 作者简介：
- 基金信息：
- DOI：10.7652/xjtuxb201704011
  CLC： TP273.1
- Online First：10 April 2017，
  
  Published：2017
- 稿件说明：
移动端阅览
An Adaptive Collaborative Guidance Strategy in Three-Body Engagement[J]. 2017, 51(4): 72-78+90.
DOI：

An Adaptive Collaborative Guidance Strategy in Three-Body Engagement[J]. 2017, 51(4): 72-78+90. DOI： 10.7652/xjtuxb201704011.

摘要

针对三体对抗中由目标飞行器释放的弱机动防御弹难以精确打击高机动来袭拦截弹的问题

提出了一种目标-防御弹的自适应协同突防制导策略。首先

根据已知的拦截弹的制导策略和运动信息

以最小化脱靶量和控制代价为目标

通过系统降阶

利用最优控制理论设计了目标-防御弹的最优协同制导律。接着

考虑实际攻防对抗中拦截弹制导策略未知的情况

采用基于平方根容积卡尔曼滤波的多模型自适应滤波器估计拦截弹的制导策略和运动信息

利用模型概率对各模型的最优协同制导律进行混合输出

得到自适应协同突防制导律。仿真结果表明:最优协同制导律能让目标飞行器协助防御弹在不具备机动能力优势的情况下成功打击拦截弹

且脱靶量小于0.1 m; 自适应协同制导律能够准确地估计拦截弹的运动状态

并使得防御弹在目标飞行器配合下以较小的控制代价精确地打击拦截弹

脱靶量有97%的概率落入小于0.765 m范围内。

Abstract

The three-body engagement consists of three vehicles

which are an evading target

a defending missile launched by the target

and a homing missile. An adaptive collaborative guidance strategy for the target and the defender is proposed to protect the target from the homing missile. Firstly

it is assumed that the perfect information of the homing missile is known. The optimal collaborative guidance laws for the target and defender are derived by using optimal control theory to minimize the missile-defender miss distance and control effort of the target and defender. Then

the real engagement condition with unknown missile's guidance strategy and measurement noise is considered. Adaptive collaborative guidance laws are proposed based on the multiple-model adaptive estimator with square-root cubature Kalman filter(MMAE-SRCKF)and the optimal collaborative guidance laws. MMAE-SRCKF is used to estimate the guidance law and state information of the homing missile. The adaptive collaborative guidance laws are derived by combining each model's optimal collaborative guidance laws. Simulation results show that the defender hits the homing missile with less control effort in the aid of the target by using the proposed optimal collaborative guidance laws

and the miss distance is smaller than 0.1 m. The proposed adaptive collaborative guidance laws estimate the state information of the missile accurately and make the target and defender act as a team to hit the homing missile.

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references

刘燕斌, 南英, 陆宇平. 导弹突防策略进展 [J]. 导弹与航天运载技术, 2010(2): 18-23.

LIU Yanbin, NAN Ying, LU Yuping. Evolvement of penetration strategies for ballistic missiles [J]. Missiles and Space Vehicles, 2010(2): 18-13.

ASHER R, MATUSZEWSKI J. Optimal guidance with maneuvering targets [J]. Journal of Spacecraft and Rockets, 1974, 11(3): 204-206.

BOYELL R L. Defending a moving target against missile or torpedo attack [J]. IEEE Transaction on Aerospace and Electronic Systems, 1976, 12(4): 522-526.

BOYELL R L. Counterweapon aiming for defense of a moving target [J]. IEEE Transaction on Aerospace and Electronic Systems, 1980, 16(3): 402-408.

SHINAR J, SILBERMAN G. A discrete dynamic game modelling anti-missile defense scenarios [J]. Dynamics and Control, 1995, 5(1): 55-67.

PERELMAN A, SHIMA T, RUSNAK I. Cooperative differential games strategies for active aircraft Protection from a Homing Missile [J]. Journal of Guidance, Control, and Dynamics, 2011, 34(3): 761-773.

RUBINSKY S, GUTMAN S. Three player pursuit and evasion conflict [J]. Journal of Guidance, Control, and Dynamics, 2014, 37(1): 98-110.

RUBINSKY S, GUTMAN S. Vector guidance approach to three-player conflict in exoatmospheric interception [J]. Journal of Guidance, Control, and Dynamics, 2015, 38(12): 2270-2286.

SHIMA T. Optimal cooperative pursuit and evasion strategies against a homing missile [J]. Journal of Guidance, Control, and Dynamics, 2011, 34(2): 424-425.

PROKOPOV O, SHIMA T. Linear quadratic optimal cooperative strategies for active aircraft protection [J]. Journal of Guidance, Control, and Dynamics, 2013, 36(3): 753-764.

GARCIA E, CASBEER D W, PACHTER M. Cooperative strategies for optimal aircraft defense from an attacking missile [J]. Journal of Guidance, Control, and Dynamics, 2015, 38(8): 1510-1520.

SHAFERMAN V, SHIMA T. Cooperative multiple-model adaptive guidance for an aircraft defending missile [J]. Journal of Guidance, Control, and Dynamics, 2010, 33(6): 1801-1813.

邹昕光, 周荻, 杜润乐, 等. 大气层外主动防御三维自适应滑模制导律 [J]. 系统工程与电子技术, 2015, 37(2): 365-371.

ZOU Xinguang, ZHOU Di, DU Runle, et al. Active defense exo-atomospheric adaptive sliding mode guidance law in three dimensions [J]. System Engineering and Electronics, 2015, 37(2): 365-371.

邹昕光, 周荻, 杜润乐, 等. 主动防御非奇异终端滑模协同制导律 [J]. 兵工学报, 2015, 36(3): 476-483.

ZOU Xinguang, ZHOU Di, DU Runle, et al. Active defense nonsingular terminal sliding mode cooperative guidance law [J]. Acta Armamentarii, 2015, 36(3): 476-483.

ZARCHAN P. Tactical and strategic missile guidance [M]. 3rd ed. Reston, VA, USA: American Institute of Aeronautics and Astronautics, 1997: 143-205.

BRYSON A, HO Y C. Applied optimal control [M]. Waltham, MA, USA: Blaisdell Publishing Company, 1969: 148-176.

ARASARATNAM I, HAYKIN S. Cubature Kalman filters [J]. IEEE Transaction on Automatic Control, 2009, 54(6): 1254-1269.

BAR-SHALOM Y, LI X R, KIRUBARAJAN T. Estimation with application to tracking and navigation [M]. New York, USA: Wiley, 2001: 742-746

OSHMAN Y, ARAD D. Differential-game-based guidance law using target orientation observations [J]. IEEE Transaction on Aerospace and Electronic Systems, 2006, 42(1): 316-326.

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