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机构地区:[1]北京航空航天大学航空科学与工程学院,北京100191
出 处:《飞行力学》2013年第3期285-288,共4页Flight Dynamics
摘 要:在对传统多步裁定法进行研究借鉴的基础上,对其提出了补充完善方法。将飞机性能参数直接引入到计算模型中,提出了依据统计学原理进行飞机、导弹数量分配以解决多机种、多弹种空战体系仿真问题的方法,增加了对电子战、空中优势情况进行的考虑,补充了对导弹消耗情况的详细统计方法,使整套算法具有更高的可信度。通过算例,证明了该算法能够有效地从宏观层面对超视距空战体系进行效能分析。In this paper, an improved multi-step adjudication method is proposed based on the traditional one. Several improvements are conducted in the calculation model: aircraft performances were introduced into calculation model directly; multi-aircraft, multi-missile air combat system simulation was performed by distributing aircraft and missiles based on statistical principles; electronic warfare and air superiority were taken into consideration ; the statistical method of missile loss was supplemented in detail. At last, it is proven via the calculation example that the method can effectively analyze the effectiveness of the be- yond visual range air combat system from macroscopic view.
分 类 号:V271.4[航空宇航科学与技术—飞行器设计]
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