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Research Article | Open Access | Just Accepted

Coverage-based optimal cooperative guidance strategy for multiple missiles against maneuverability-superior targets

Jin Tang1,2, Jiaxin Wang1,2, Kebo Li1,2( ), Haojian Li1,2, Yan-gang Liang1,2

1 College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China

2 State Key Laboratory of Space System Operation and Control, Changsha 410073, China

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Abstract

For the problem of exo-atmospheric interception, a coverage-based optimal cooperative guidance strategy is developed for multiple inferior missiles against a maneuverability-superior target. First, the cooperative interception problem is transformed into a coverage problem of the target’s evasion capability. Leveraging the capture region theory of biased proportional navigation, the maneuvering coverage region of the interceptor relative to the target under nonlinear conditions is derived. This coverage region focuses on covering the target’s maneuverability range rather than its lateral position, effectively avoiding errors induced by linearization assumptions. Furthermore, by optimizing the energy consumption of all interceptors, an optimal cooperative guidance problem under coverage constraints is formulated. The Lagrange multiplier method is employed to analytically solve for the real-time guidance commands for each interceptor, ensuring complete coverage of the target’s maneuverability range. Numerical simulation results demonstrate the effectiveness and superiority of the proposed strategy.

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Cite this article:
Tang J, Wang J, Li K, et al. Coverage-based optimal cooperative guidance strategy for multiple missiles against maneuverability-superior targets. Astrodynamics, 2026, https://doi.org/10.1007/s42064-026-0332-6

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Received: 09 April 2026
Accepted: 13 July 2026
Available online: 28 September 2026

© Tsinghua University Press 2026.

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