1) terminal correction projectile
末修弹
1.
The influential factors of the trajectory correction including the pulse motor starting control time,pulse motor quantity were analyzed and the application and limit of trajectory tracking used in terminal correction projectile were studied.
分析了脉冲启控时间、脉冲个数对修正效果的影响,并对弹道追踪导引律在末修弹中应用条件及其局限性进行了详细研究。
2) terminal trajectory correction rocket projectile
末修火箭弹
1.
Characteristics of parabolic and proportional navigation guidance of terminal trajectory correction rocket projectile;
末修火箭弹抛物线比例导引的特性
3) terminal correction submunition
末修子母弹
1.
The assessment criterion for interdiction ability of terminal correction submunition(TCM) to runway was taken as objective function,and the parameters which should be optimized were confirmed.
将末修子母弹对跑道封锁能力的评价指标作为优化设计的目标函数,确定了需要优化的总体参数,并利用改进的粒子群优化算法建立了总体参数的优化模型。
2.
On the basis of the proposed new concept,the assessment criteria for damage ability of terminal correction submunition were presented,which are of important reference value in system design and efficiency optimization of terminal correction submunition.
根据末修子母弹的工作原理及其对机场跑道的毁伤效果,定义了有效毁伤长度的概念,并以此为基础给出了单发末修子母弹对机场跑道毁伤能力的评价指标。
3.
A calculation method of the damage probability of terminal correction submunition to integrated aim was built based on the Monte-Carlo method, and the calculation of the damage probability of terminal correction submunition to integrated aim was achieved based on programming with VC.
建立了末修子母弹对集群目标毁伤概率的计算模型,根据集群目标布阵特点建立坐标系,采用Monte-Carlo试验统计法,随机模拟子母弹抛撒落点,通过判断子弹弹道末端对探测目标的打击弹道修正来得到被打中的目标编号,并用VC++编程实现了末修子母弹对集群目标的毁伤概率的计算。
4) terminal correct projectile
末段修正弹
1.
On the basis of setting up the angle motion mathematic model of the terminal correct projectile forced by impulse corrective force, this paper discusses the dynamic response of the terminal correct projectile and response spectrum.
建立了末段脉冲修正弹在脉冲修正力作用下的角运动数学模型 ,分析了末段修正弹对脉冲修正力的动态响应特性和响应谱 ,给出了对尾翼稳定脉冲修正弹设计有普遍指导意义的结果。
5) terminal trajectory correction projectile
末段弹道修正弹
6) terminal correction mortar projectile
末段修正迫弹
1.
This paper researches the impulse correction technologies of terminal correction mortar projectile, put forward the four quadrant impulse correction scheme and the higher frequency laser flash impulse correction scheme.
文中对末段修正迫弹脉冲修正技术进行了研究,提出了四象限脉冲修正方案和高频照射脉冲修正方案,分别进行了脉冲发动机组布局设计和脉冲修正策略设计,建立了相应的数学模型;四象限脉冲修正方案由于没有准确的目标方位信息,会造成脉冲推力损失和脱靶量增大;通过使用脉冲发动机提前工作角,高频照射脉冲方案能使脉冲作用力的合力作用在正确的修正方向上,有利于减少脱靶量,提高修正精度。
补充资料：半硬壳式弹体(见弹道导弹弹体)
半硬壳式弹体(见弹道导弹弹体)
semi-hard-shelled missile body
bQn yingkeshi dan桩半硬壳式弹体(semi一hard一shelled、ssilebody)见弹道导弹弹体。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条