| Citation: | WANG Jie, DING Dali, XU Ming, et al. Air-to-air missile launchable area based on target escape maneuver estimation[J]. Journal of Beijing University of Aeronautics and Astronautics, 2019, 45(4): 722-734. doi: 10.13700/j.bh.1001-5965.2018.0462(in Chinese)
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In order to satisfy the special requirement for fire control of air-to-air missiles under unmanned air combat conditions, the problem of launchable area of air-to-air missile based on target maneuver estimation is presented. Based on the missile-target tracking escape countermeasure strategy, the target maneuver estimation model is designed. According to the relative position information of the missile and the target, the estimation of the target escape maneuver mode is realized. Based on a variety of practical constraints, a missile dynamics model is constructed. A launchable area boundary solving strategy based on the golden section search strategy is designed to achieve a fast and accurate search for the boundary value of the launchable area. The simulation results show that the air-to-air missile has a greater probability of hitting the target in the launchable area based on the target maneuver estimation proposed in the paper. The presented launchable area is more suitable for the dramatic change of the target escape maneuver in the close air combat, which is beneficial to the full play of the missile tactical performance.
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