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A Cooperative Guidance Law with Multi-constraints for Intercepting Maneuvering Target

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Proceedings of 3rd 2023 International Conference on Autonomous Unmanned Systems (3rd ICAUS 2023) (ICAUS 2023)

Part of the book series: Lecture Notes in Electrical Engineering ((LNEE,volume 1174))

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Abstract

Aiming at the problem of cooperative interception of maneuvering target by multiple air-to-surface missiles, a three-dimensional cooperative guidance law with falling angle constraint is proposed. Firstly, by applying Lyapunov theory, guidance commands are designed to ensure that missiles hit the target at desired falling direction and angle. Secondly, the time-to-go of each missile is estimated in the missile’s yaw plane by solving homogeneous differential equations with second-order constant coefficients. Then, based on the finite time consistency theory, a cooperative guidance law with time-varying guidance coefficient is designed, so that each missile hits the maneuvering target at the same time. Finally, the effectiveness and correctness of the multi-constraint cooperative guidance law designed in this paper are verified by simulation.

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Acknowledgements

This work was supported by the Shanghai Aerospace Science and Technology Innovation Foundation under Grant Nos.SAST2021-027 and SAST2021-056, Aeronautical Science Foundation of China under Grant 20220001059001 and 2022Z037059001, and the National Undergraduate Training Program for Innovation and Entrepreneurship under Grant 202210288023.

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Correspondence to Panlong Wu .

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Wang, Y., He, Y., Zhong, J., Wu, P. (2024). A Cooperative Guidance Law with Multi-constraints for Intercepting Maneuvering Target. In: Qu, Y., Gu, M., Niu, Y., Fu, W. (eds) Proceedings of 3rd 2023 International Conference on Autonomous Unmanned Systems (3rd ICAUS 2023). ICAUS 2023. Lecture Notes in Electrical Engineering, vol 1174. Springer, Singapore. https://doi.org/10.1007/978-981-97-1091-1_11

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