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1)  initial trajectory
初始弹道
1.
The initial trajectory numerical simulation of air launched missile;
空射导弹发射初始弹道数值仿真
2.
Influence on initial trajectory of large electric power torpedo caused by battery activated outside tube;
大型电动力鱼雷动力电池管外激活发射对初始弹道的影响
3.
Analysis of effects of torpedo′s weighing property on initial trajectory
鱼雷衡重特性对初始弹道的影响分析
2)  initial ballistic
初始弹道
1.
Aerodynamic characteristics and initial ballistic interference on a missile by a helicopter s rotor down-wash in hovering;
悬停旋翼下洗流对导弹的气动特性和初始弹道的干扰研究
3)  initial phase ballistic
初始段弹道
1.
On the basis of ballistics and missile flight mechanics, initial velocity, angle of fire and stability of initial phase ballistic curve of anti tank missile are analyzed and calculated.
以弹道学和导弹飞行力学为依据 ,对反坦克导弹初始段弹道的初速、射角及稳定性进行分析计算 ,提出了提高反坦克导弹初始段弹道稳定性及如何改进初始段的弹道散布的方
4)  initial rocket position
初始弹姿
5)  initial orbit
初始轨道
1.
An optimal selection algorithm based on grey relational analysis is proposed to select the optimal group from multiple groups of satellite initial orbits,which are determined via various data sources by Space TT&C(Tracking,Telemetry and Command) Center.
针对航天测控中心利用各种数据源确定的多组初始轨道如何选优问题,提出了一种基于灰色关联分析的卫星初始轨道选优算法。
2.
Theoretical analysis was proposed in the optimal selection of spacecraft initial orbits during the orbit injection phase,and an algorithm based on grey relational analysis was proposed to select the optimal initial orbit.
针对航天器入轨段,如何从多组初始轨道中选择一组最优轨道问题,进行了深入地理论分析,提出了一种基于灰色关联分析法的航天器初始轨道选优算法。
6)  incipient trajectory
初期弹道
1.
The affection of the torpedo incipient trajectory of the surface warship swaying;
舰艇摇摆对鱼雷初期弹道影响的研究
2.
Being Expounding the conception of torpedo incipient trajectory to ensure effective usage and reduce the lost and shorten the test time for torpedoes, this paper researches the mometumtherorim and the twist therorem to establish the incipient trajectory mathematic model of the surface warship launching torpedo.
利用动量定理和动量矩定理建立水面舰艇发射鱼雷初期弹道的数学模型。
补充资料:弹道(见弹道学)


弹道(见弹道学)
trajectory

dQfldQO弹道(t rajectory)见弹道学。
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