带有引诱角色的多飞行器协同最优制导方法

doi:10.7527/S1000-6893.2019.23402

Abstract

Abstract: This paper considers the situation that our high-value aircraft launches two defender to intercept the interceptor when it is faced with interception by the other interceptor. Based on the optimal control theory, an explicit cooperative guidance law with relative interception angle at the end of interception is designed under the assumption that all four aircraft have first-order linear dynamic characteristics. The explicit cooperative guidance law takes into account the cooperation of high-value aircraft and two defenders, and gives the analytical solution of the optimal control input of the three objects. The simulation results show that the designed guidance law can make the two defenders intercept the interceptor successfully, and impose a relative interception angle at the end of the interception. By comparing with the implicit cooperative guidance law which only considers two defenders, the explicit cooperative guidance law is superior to the implicit cooperative guidance law in control requirements and energy consumption. In addition, the stability of the cooperative guidance law under different launching conditions is verified.

Key words: multi-aircraft, cooperative guidance, luring role, optimal control, interception angle, explicit

CLC Number:

WANG Shaobo, GUO Yang, WANG Shicheng, LIU Zhiguo, ZHANG Shuai. Cooperative optimal guidance method for multi-aircraft with luring role[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(2): 323402-323402.

References 23

[1]	姚郁, 郑天宇, 贺风华, 等. 飞行器末制导中的几个热点问题与挑战[J]. 航空学报, 2015, 36(8):2696-2716. YAO Y, ZHENG T Y, HE F H, et al. Several hot issues and challenges in terminal guidance of flight vehicles[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(8):2696-2716(in Chinese).
[2]	SHAFERMAN V, SHIMA T. Cooperative optimal guidance laws for imposing a relative intercept angle[J]. Journal of Guidance, Control, and Dynamics, 2015, 38(8):1395-1408.
[3]	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.
[4]	BOYELL L R. Defending a moving target against missile or torpedo attack[J]. IEEE Transactions on Aerospace and Electronic Systems, 1976, 12(4):522-526.
[5]	BOYELL L R. Counterweapon aiming for defense of a moving target[J]. IEEE Transactions on Aerospace and Electronic Systems, 1980, 16(3):402-408.
[6]	RATNOO A, SHIMA T. Line-of-sight interceptor guidance for defending an aircraft[J]. Journal of Guidance, Control, and Dynamics, 2011, 34(2):522-532.
[7]	RATNOO A, SHIMA T. Guidance strategies against defended aerial targets[J]. Journal of Guidance, Control, and Dynamics, 2012, 35(4):1059-1068.
[8]	YAMASAKI T, BALAKRISHNAN S N, TAKANO H. Modified command to line-of-sight intercept guidance for aircraft defense[J]. Journal of Guidance, Control, and Dynamics, 2013, 36(3):898-902.
[9]	YAMASAKI T, BALAKRISHNAN S N. Intercept guidance for cooperative aircraft defense against a guided missile[J]. IFAC Proceedings Volumes, 2010, 43(15):118-123.
[10]	SHAFERMAN V, SHIMA T. Cooperative multiple model adaptive guidance for an aircraft defending missile[J]. Journal of Guidance, Control, and Dynamics, 2010, 6(33):1801-1813.
[11]	GUO Y, XIAO X H, HE F H, et al. Triangle interception scenario:A finite-time guidance approach[J]. International Journal of Aerospace Engineering, 2016,2016(1):1-12.
[12]	张帅, 郭杨, 王仕成. 带有引诱角色的有限时间协同制导方法[J]. 宇航学报, 2018,39(3):308-317. ZHANG S, GUO Y, WANG S C. Finite time cooperative guidance method with a lure role[J]. Journal of Astronautics, 2018,39(3):308-317(in Chinese).
[13]	ZHANG S, GUO Y, WANG S C. Cooperative intercept guidance of multiple aircraft with a lure role included[J]. International Journal of Aerospace Engineering,2018,2018:1-15.
[14]	SHIMA T. Optimal cooperative pursuit and evasion strategies against a homing missile[J]. Journal of Guidance, Control, and Dynamics, 2011, 34(2):414-425.
[15]	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.
[16]	PERELMAN A, SHIMA T, RUSNAK I. Cooperative differential game strategies for active aircraft protection from a homing missile[J]. Journal of Guidance, Control, and Dynamics, 2011, 34(3):761-773.
[17]	KUMAR S R, SHIMA T. Cooperative nonlinear guidance strategies for aircraft defense[J]. Journal of Guidance, Control, and Dynamics, 2016, 40(1):1-15.
[18]	WEISS M, SHIMA T, CASTANEDA D, et al. Combined and cooperative minimum-effort guidance algorithms in an active aircraft defense scenario[J]. Journal of Guidance, Control, and Dynamics, 2017:1-14.
[19]	赵建博, 杨树兴, 熊芬芬. 无导引头也无惯导导弹的协同制导[J]. 航空学报, 2019, 40(10):323191. ZHAO J B, YANG S X, XIONG F F. Cooperative guidance for seeker less missile without inertial navigation system[J]. Acta Aeronautica et Astronautica Sinica, 2019, 40(10):323191(in Chinese).
[20]	SHAFERMAN V, OSHMAN Y. Cooperative interception in a multi-missile engagement[C]//AIAA Guidance, Navigation, & Control Conference. Reston,VA:AIAA,2009.
[21]	LIU Y F, QI N M, SHAN J J. Cooperative interception with double-line-of sight-measuring[C]//AIAA Guidance, Navigation, & Control Conference.Reston,VA:AIAA, 2013.
[22]	CHEN T, XU S. Approach guidance with double-line-of-sight measuring navigation constraint for autonomous rendezvous[J]. Journal of Guidance, Control, and Dynamics, 2011, 34(3):678-687.
[23]	FONOD R, SHIMA T. Estimation enhancement by cooperatively imposing relative intercept angles[J]. Journal of Guidance, Control, and Dynamics, 2017,40(7):1711-1725.

Cooperative optimal guidance method for multi-aircraft with luring role

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