1)Reentry trajectory再入弹道
1.in this paper, an adaptive estimator of reentry trajectory parameters is proposed.本文研究再入弹道参数的自适应估计。
英文短句/例句
1.Object oriented simulation for six freedom degree reentry trajectory再入弹道六自由度面向对象仿真研究
2.maneuverable ballistic reentry vehicle机动弹道式再入飞行器
3.advance ballistic reentry system (ABRS)高级弹道式再入系统
4.Optimization Design of Reentry Trajectory for Maneuverable Warhead Based on Genetic Algorithms基于遗传算法的机动弹头再入段弹道优化设计
5.In this paper, the principles and methods of target recognition are discussed mainly, using infrared optical technical equipment through the measurement of the target′ s temperature, radiant intensity and infrared thermal image.反导系统对于来袭弹道导弹弹道中段及再入段的识别可以用微波雷达技术，也可用光学技术。
6.MIRV (multiple independently targeted reentry vehicle)多弹头分导再入飞行器（多弹头导弹）
7.multiple independent reentry vehicle多弹头分导再入飞行器
8.Analysis and Prediction of Reentry Error for Reentry Maneuvering Warhead With Integrated Navigation System复合制导再入机动弹头再入误差分析
9.Estimate, Discriminate, Modeling and Mathematics Simulation Research of Ballistic Coefficient for Reentry Object;再入目标弹道系数的估计、辨识、建模及其数学仿真研究
10.Research on application of virtual guidance to the trajectory optimization of reentry-glide flight虚拟导引方法在再入滑翔弹道优化中的应用研究
11.To place into an orbit, a trajectory, or a stream.置于放入一个轨道、弹道或潮流中
12.THE ECHO BEHAVIOR ANALYSIS OF THE NONEQUILIBRIUM WAKE再入弹头非平衡尾迹的回波特性分析
13.Research on Restriction of Initial Space Maneuver of Reentry Missile弹头初始再入点空间约束范围的研究
14.Study of Missile Reentry Dynamic Decoupling Control Based on Variable Structure Robustness Compensating动态解耦和变结构鲁棒补偿的导弹再入控制
15.An Optimal Guidance Law for Reentry Warhead Base on Angular Velocity一种基于角速率的再入弹头最优制导律
16.Study of Reentry Trajectory Optimization of Maneuverable Warhead Based on Spline Curve基于样条曲线的机动弹头再入轨迹优化研究
17.Interceptive Research of Missile with the Mobility of the End Zone at It’s Re-Entry Phase带末端机动的导弹再入段拦截问题研究
18.Variable structure guidance law of reentry maneuvering warhead with terminal angular constraint带落角约束的再入机动弹头的变结构导引律
相关短句/例句
Ballistic Reentry弹道式再入
1.Neural network is used in the ballistic reentry guidance of orbit weapon to get flight-path angle in real time.将神经网络应用于轨道武器的弹道式再入制导中,实时得到所需航迹角,以此形成制导信号。
3)re-entry vehicle再入弹道段
4)reentry trajectory optimization再入弹道优化
1.Maneuver reentry trajectory optimization with inner state constraints;具有内点状态约束的机动再入弹道优化设计
5)reentry trajectoriy simulation再入弹道仿真
6)Maneuverable Reentry Trajectory再入机动弹道
延伸阅读
弹道(见弹道学)弹道(见弹道学)trajectory dQfldQO弹道(t rajectory)见弹道学。
