Impact Time Control Cooperative Guidance Law Design Based on Modified Proportional Navigation

نویسندگان

چکیده

The paper proposes a two-dimensional impact time control cooperative guidance law under constant velocity and three-dimensional time-varying velocity, which can both improve the penetration ability combat effectiveness of multi-missile systems adapt to complex variable future warfare. First, more accurate time-to-go estimation method is proposed, based on modified proportional navigational (MPNG) with constraint designed in this paper, also effective when initial leading angle zero. Second, adopting architecture centralized coordination, using MPNG as local guidance, desired coordination variables, designed. Finally, solving expression derived, analytic function respect given, Numerical simulation results verify feasibility applicability methods.

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ژورنال

عنوان ژورنال: Aerospace

سال: 2021

ISSN: ['2226-4310']

DOI: https://doi.org/10.3390/aerospace8080231