导弹飞行安全区确定  

Determination of Flight Safety Zone of Missile

作　　者：王明海[1] 刘新学[1] 康建斌[1] 

机构地区：[1]第二炮兵工程学院

出　　处：《飞行力学》1999年第1期77-80,共4页Flight Dynamics

摘　　要：对导弹飞行安全区进行了确切定义，分别对正常飞行弹安全区和故障飞行弹安全区进行了定量研究。在研究故障弹安全区时，从对导弹飞行安全区产生的最终效果出发，对各种故障进行了科学分类，并建立了各类故障的故障方程，进而给出了导弹飞行安全区的计算模型和方法，这些模型和方法不仅符合故障飞行的物理背景，而且工程计算简单可靠。通过仿真，给出了导弹发射场、航迹区和靶场的安全区散布规律和量值大小。In this paper, not only the exact definition of missile flight safety zone has been given, but also the quantitative research on normal and abnormal flight safety zone have been done respectively. In studying the abnormal flight safety zone, all of malfunctions have been classified according to their influence on the missile flight safety zone, and the relevant malfunction equations have been developed, and then the calculation model and method of the missile flight safety zone have also been given. These calculation model and method not only accord with the objective reality but also are simple and reliable. By means of simulation calculation, the dispersion law and range have been obtained concerning the safety zone of launch area, track area and target area.

关 键 词：导弹 飞行 安全区 航迹 弹道导弹 

分 类 号：TJ761.3[兵器科学与技术—武器系统与运用工程] TJ760.12