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假设起始分开很远的两架飞机进行导弹空战。每一飞机在开始的攻击阶段寻求其导弹的优良发射位置,同时避免差的规避位置。在发射瞬间,飞机进入纯规避段,见图1。此问题要求飞机的转弯与速度性能与导弹的射程能力能够匹配。它的最优解指出如何应用参与的飞行器的全部性能。此项研究的特殊目的还有考察远距离战术。机动时,飞行器能自由选择高度、提
It is assumed that two aircrafts, far apart from the beginning, are conducting missile air combat. Each aircraft seeks its missile’s fine launch position during the initial attack phase, while avoiding poor avoidance positions. At the launch moment, the aircraft entered a pure avoidance zone, see Figure 1. This issue requires that the aircraft’s turn and speed performance be matched to the missile’s range capability. Its optimal solution indicates how to apply the full performance of the participating aircraft. The special purpose of this study is to examine long-range tactics. When maneuvering, the aircraft is free to choose the height, mention