Cooperative Guidance Law for High-Speed and High-Maneuverability Air Targets

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2023-2-01
Cevher, Firat Yilmaz
Leblebicioğlu, Mehmet Kemal
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In this paper, a novel cooperative and predictive guidance law is proposed to intercept high-speed and high-maneuverability targets with inferior interceptors. The purpose of guidance is cooperatively covering the most-probable locations where the target may be in the future. To fulfill this purpose, predicted target states in the form of a probability density function were obtained using limited target information, i.e., noisy position data for one case and maneuverability limits for the second case, at first. Next, the likelihood of the reachable set of interceptors was computed over the predicted target state. Then, to increase the probability of interception in a finite time, the interceptors' trajectories were adjusted collaboratively depending on the likelihood values. An extensive Monte Carlo study, with practically applicable simulation parameters, was used to demonstrate the effectiveness of the proposed methods against targets in challenging maneuvering modes.
cooperative guidance, multiple missiles, maneuvering target, inferior interceptor, probability of interception, IMPACT-TIME, MULTIPLE MISSILES, PREDICTIVE GUIDANCE, MANEUVERING TARGETS, STRATEGY, DESIGN, STATIONARY, ATTACK
https://hdl.handle.net/11511/102748
Department of Electrical and Electronics Engineering, Article

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Citation Formats
F. Y. Cevher and M. K. Leblebicioğlu, “Cooperative Guidance Law for High-Speed and High-Maneuverability Air Targets,” AEROSPACE, vol. 10, no. 2, pp. 0–0, 2023, Accessed: 00, 2023. [Online]. Available: https://hdl.handle.net/11511/102748.
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