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作 者:范凯胤 王学奇[1] 姚鹏[1] FAN Kai -yin;WANG Xue -qi;YAO Peng(College of Information Engineering, Qingdao University, Qingdao Shandong 266071, China)
机构地区:[1]空军工程大学航空航天工程学院,陕西西安710038
出 处:《计算机仿真》2018年第6期28-32,共5页Computer Simulation
摘 要:针对空空导弹主要研究了在风场中的射后动态攻击区,用于得到考虑风场影响下任何飞行时间内的导弹动态攻击区信息。根据空空导弹,飞行目标和风场的数学模型,利用二分法对于在风场中的射后动态攻击区的一些典型情况进行了仿真分析。相比于传统动态攻击区的仿真结果,可以得到射后动态攻击区的相关属性:射后动态攻击区包含在传统最大攻击区里,但不完全包含在传统不可逃逸攻击区里;传统动态攻击区只用于发射时刻,而射后动态攻击区可以用于任何飞行时间内;风场会影响射后动态攻击区。In this paper, we mainly research the simulation of air - to - air missile dynamic lauch envelopes after launching in the wind field, which is used to obtain the information of the missile dynamic launch envelopes at any flight time under the influence of wind field. According to the mathematical model of the air - to - air missile, the flight target and the wind field, the simulation analysis was carried out using the method of dichotomy for some typical cases of the dynamic launch envelopes after launching in the wind field. Compared with the traditional dynamic Launch Envelopes, the simulation results can obtain the related properties of dynamic Launch Envelopes after launching, such as dynamic Launch Envelopes after launching is included in the traditional maximum Envelopes, but not included in the traditional on - escape envelopes ; the traditional dynamic Envelopes can just be used at the launch time, and dynamic Launch Envelopes after launching can be used at any flight time ; the wind field can affect the dynamic Launch Envelopes after launching.
关 键 词:空空导弹 射后动态攻击区 传统动态攻击区 风场 二分法
分 类 号:TJ765.4[兵器科学与技术—武器系统与运用工程]
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