A Guidance law for interception of very high-speed targets using a simulator-based learning algorithm

Document Type : Dynamics, Vibrations, and Control

Authors

1 Department of Electrical and Computer Engineering, K. N T University of Technology

2 imam hossein university

Abstract

In this paper, the problem of intercepting very high-speed non-maneuvering ballistic targets is addressed and a novel guidance law to enhance the probability of ‘hit to kill’ is designed. The most important challenges which arise in the interception of high-speed ballistic targets include high closing velocity resulting in the lack of time for the final reaction, low radar cross section and high noise power resulting in the lack of precise detection of target track until the last moments and considerable time constant in the order of final interception phase time. By ignoring some of these important challenges, existing guidance laws show great degradation in practice. In this paper we propose a twofold technique to overcome the challenges: a staggered missile team to share the target detection information and a feedforward static guidance input. The amplitude of static guidance is deduced through a regression model using a simulator software. Simulation of the proposed guidance law on a high precision model shows the efficiency of the method.

Keywords

References

[1] Hayoun, S. Y. and Shima, T. “NecessaryConditions for “Hit-to-Kill” in Missile Interception Engagements”, J. Guid. Control. Dyn. Vol. 41, No. 4, pp. 916-928, 2018.##
[2] Zarchan, P. “Ballistic Missile Defense Guidance and Control Issues”, Sci. Global Secur. Vol. 8, No. 1, pp. 99–124, 1998.##
[3] Zarchan, P. “Tactical and Stratgic Missile Guidance”, American Institute of Aeronautics and Astronautics, United States, 2012.##
[4] Fu, B., Fu, W., Guo, H, Chen, K., and Chang, X. “Partial Integrated Guidance and Control Method for the Interception of Nearspace Hypersonic Target”, 13th IEEE Int. Conf. on Control and Automation (ICCA), Ohrid, Macedonia, 2017.##
[5] Kuroda, T. and Imado, F. “Advanced Missile Guidance System against Very High Speed Target”, Guidance, Navigation and Control Conf., American Institute of Aeronautics and Astronautics, Minnesota, United States, 1988.##
[6] Lin, C., Member, S., Hung, H., Chen, Y., and Chen, B. “Development of an Integrated Fuzzy-Logic-Based Missile Guidance Law against High Speed Target Maneuver”, IEEE Trans. Fuzzy Syst. Vol. 12, No. 12, pp. 157-169, 2004.##
[7] Golan, O. M., Shima, T., and Engineer, C. S. “Head Pursuit Guidance for Hypervelocity Interception”, AIAA Guidance, Navigation, and Control Conference and Exhibit, 2004.##
[8] Prasanna, H. M. and Ghose, D. “Retro-Proportional Navigation: A New Guidance Law for Interception of High-Speed Targets”, J. Guid. Control Dyn. Vol. 10, No. 3, pp. 298-302, 2014.##
[9] Li, Y., Yan. L., Zhao. J., Liu, F. and Wang, T. “Combined Proportional Navigation Law for Interception of High-Speed Targets”, Def. Tech., Vol. 10, No. 3, pp. 298-303, 2014.##
[10] Padhi, R., Chawla, C., and Das, P. G. “Partial Integrated Guidance and Control of Interceptors for High-Speed Ballistic Targets”, J. Guid. Control Dyn. Vol. 37, No. 1, 2014.##
[11] Shaferman, V. and Sima, T. “Cooperative Optimal Guidance Laws for Imposing a Relative Intercept Angle”, J. Guid. Control Dyn. Vol. 38, No. 8, pp. 1395-1408, 2015.##
[12] Su, W., Li. K., and Chen, L. “Coverage-Based Cooperative Guidance Strategy against Highly Maneuvering Target”, Aerosp. Sci. Tech. Vol. 71, pp. 147-155, 2017.##
[13] Zhou, J. and Yang, J., “Distributed Guidance Law Design for Cooperative Simultaneous Attacks with Multiple Missiles”, J. Guid. Control Dyn. Vol. 39, No. 10, pp. 2439-2447, 2016.##
[14] Shaferman, V. and Oshman, Y. “Stochastic Cooperative Interception Using Information Sharing Based on Engagement Staggering”, J. Guid. Control Dyn. Vol. 39, No. 9, pp. 2127-2141, 2016.##
[15] Ljung, L. “System Identification: Theory for the User” Prentice Hall, United States, 1999.##
[16] Yanushevsky, R. “Modern Missile Guidance”, CRC Press, United States, 2007##

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History

  • Receive Date: 29 July 2019
  • Revise Date: 15 November 2019
  • Accept Date: 25 August 2020
  • Publish Date: 22 October 2020

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