Abstract
In this paper, an attack-time cooperative guidance scheme is proposed to improve the penetration ability of the guided missiles, which aim at realizing the saturated attack on a single target and it has a specified angle of attack. The guidance scheme consists of three stages. In the first stage, a time coordination method based on paranoid proportional navigation method for tracking guided missile is designed. In the second stage, the missiles are adjusted to achieve the coordination of attack angle. In the third stage, Bessel curve is used to design the trajectory with large climb and dive to improve the penetration ability during the attacking. Finally, the feasibility of the guidance law is verified by simulation.
Keywords
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He, S., Lee, C.H.: Optimal proportional-integral guidance with reduced sensitivity to target maneuvers. IEEE Trans. Aerosp. Electron. Syst. 54(5), 2568–2579 (2018)
Farooq, A., Limebeer, D.J.N.: Trajectory optimization for air-to-surface missiles with imaging radars. J. Guidance Control Dyn. 25(5), 876–887 (2002)
Yanushevsky, R., Boord, W.: Lyapunov approach to guidance laws design. Nonlinear Anal. Theory Methods Appl. 63(5–7), 743–749 (2005)
Song, E.J., Tahk, M.J.: Real-time neural-network midcourse guidance. Control Eng. Pract. 9(10), 1145–1154 (2001)
Chwa, D., Choi, J.Y.: Adaptive nonlinear guidance law considering control loop dynamics. IEEE Trans. Aero. Electr. Syst. 39(4), 1134–1143 (2003)
Shen, G., et al.: Adaptive sliding-mode control for mars entry trajectory tracking with finite-time convergence. Int. J. Robust Nonlinear Control 29(5), 1249–1264 (2019)
Zong, Q., et al.: Robust adaptive dynamic surface control design for a flexible air-breathing hypersonic vehicle with input constraints and uncertainty. Nonlinear Dyn. 78(1), 289–315 (2014)
Chen, T., Zhu, M., Zheng, Z.: Asymmetric error-constrained path-following control of a stratospheric airship with disturbances and actuator saturation. Mech. Syst. Sig. Process. 119, 501–522 (2019)
Kumar, S.R., Rao, S., Ghose, D.: Nonsingular terminal sliding mode guidance with impact angle constraints. J. Guidance Control Dyn. 37(4), 1114–1130 (2014)
Weiss, M., Shima, T.: Linear quadratic optimal control-based missile guidance law with obstacle avoidance. IEEE Trans. Aerosp. Electron. Syst. 55(1), 205–214 (2019)
Esmaelzadeh, R., Naghash, A., Mortazavi, M.: Near optimal re-entry guidance law using inverse problem approach. Inverse Probl. Sci. Eng. 16(2), 187–198 (2008)
Qin, Z., Qi, X., Yongling, F.: Terminal guidance based on bézier curve for climb-and-dive maneuvering trajectory with impact angle constraint. IEEE Access 7, 2969–2977 (2019)
Shaferman, V., Shima, T.: Cooperative multiple model adaptive guidance for an aircraft defending missile. In: AIAA Guidance, Navigation, and Control Conference, vol. 33, issue 6, pp. 1801–1813 (2010)
Yang, B., Liu, H.H.T., Yao, Y.: Cooperative interception guidance for multiple vehicles: a receding horizon optimization approach. In: Guidance Navigation Control Conference, pp. 827–831 (2014)
Xingling, S., Honglun, W.: Back-stepping active disturbance rejection control design for integrated missile guidance and control system via reduced-order ESO. ISA Trans. 57, 10–22 (2015)
Zhao, J., Zhou, R.: Obstacle avoidance for multi-missile network via distributed coordination algorithm. Chin. J. Aeronaut. 29(2), 441–447 (2016)
Zhao, Q., et al.: Distributed group cooperative guidance for multiple missiles with fixed and switching directed communication topologies. Nonlinear Dyn. 90(4), 2507–2523 (2017)
Han, T., Hu, Q.: Robust autopilot design for STT missiles with multiple disturbances using twisting control. Aerosp. Sci. Technol. 70, 428–434 (2017)
Kim, T.H., Park, B.G., Tahk, M.J.: Bias-shaping method for biased proportional navigation with terminal-angle constraint. J. Guidance Control Dyn. 36(6), 1810–1816 (2013)
Acknowledgements
This work was supported by National Natural Science Foundation of China (Grant No. 61803111), and Scientific Research Projects of Guangzhou Education Bureau (Grant No. 201831805).
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Liu, Y., Lan, X., Xu, W. (2020). Attack-Time Cooperative Guidance of Multi-missile System Based on Bessel Curve. In: Wang, R., Chen, Z., Zhang, W., Zhu, Q. (eds) Proceedings of the 11th International Conference on Modelling, Identification and Control (ICMIC2019). Lecture Notes in Electrical Engineering, vol 582. Springer, Singapore. https://doi.org/10.1007/978-981-15-0474-7_111
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DOI: https://doi.org/10.1007/978-981-15-0474-7_111
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