Correction Strategy of Online Midcourse Guidance for High-Speed Gliding Target Interceptor
نویسندگان
چکیده
During the interception of a high-speed gliding vehicle (HGV), predicted intercept point (PIP) is updated many times, so interceptor must continuously adjust its trajectory. In this paper, we propose an online guidance correction algorithm for interceptor, which can effectively meet position constraints and energy management process. Firstly, simplify interceptor’s maneuvering problem to two-body orbital transfer problem. The Lambert orbit method used enable maneuver towards target’s PIP. Secondly, by comparing high probability existence area (THPEA) with interceptor-interceptable (IIA), engine start threshold set in stages avoid frequent redundancy maneuvers caused starting during missile correction. This approach achieves management. Simulation results show that our midcourse strategy effective.
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ژورنال
عنوان ژورنال: Applied sciences
سال: 2023
ISSN: ['2076-3417']
DOI: https://doi.org/10.3390/app13116661