orbit maneuver

Orbit maneuver hydrogen-oxygen thruster based on gas dynamic resonance igniter is a novel chemical propulsion technology especially prospective in space station application.

结合气动谐振点火器进行头部设计的氢氧变轨火箭发动机是一项新颖化学火箭推进技术，尤其适于空间站应用。

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Retrofit design and analysis of composite truss structure of orbit maneuver motor bracket

复合材料桁架式发动机支架改型设计分析

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Attitude control during orbit maneuver

轨道机动期间的姿态控制

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The energy of space target is a character signal of orbit maneuver.

空间目标的轨道机动是与机械能的变化联系在一起的。

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Based on the analysis of the operational process of space-based weapons aiming at ground targets, this paper firstly educes that the orbit maneuver is the pivotal element in the rapid operation.

首先通过对天基武器作战过程的分析，得出在轨机动是实现天基快速对地打击的关键的结论；

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According to the problem of examining GEO satellites, the paper has given a method of using orbit maneuver vehicle on highly eccentric orbit to photograph the target and studied related technologies.

对于地球同步轨道卫星的检查，论文提出了一种利用大椭圆轨道机动飞行器对其抵近照相的方法，并研究了相关技术。

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Optimal orbit maneuver of the space station adjoint satellite

空间站伴随卫星的最优轨道机动

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And a transfer trajectory of orbit maneuver with safe and optimal fuel consumption is able to be selected in combination with the analysis of collision probability and fuel consumption.

利用碰撞概率计算公式分析航天器发生碰撞的可能性，并结合燃料消耗选择一条碰撞概率小于给定的警戒值且燃料最优的转移轨道。

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Influence of Satellite Control Force on Its Flexible Solar Panel during Orbit Maneuver

卫星轨道控制力对挠性帆板振动的影响

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The Research of Visual Simulation Technology for Orbit Maneuver Based on STK

基于STK的轨道机动视景仿真技术研究

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Based on "Space maneuver platform technology" issues and using genetic algorithms on spacecraft orbit maneuver, this paper conducted a study.

本文结合XXX追踪与反追踪技术课题，利用遗传算法对航天器轨道机动问题进行了研究。

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An Autonomous Navigation Method for Spacecrafts during Orbit Maneuver

航天器轨道机动过程中的自主导航方法

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Research on Space-based Orbit Maneuver Identification Algorithms

基于天基观测的空间目标变轨识别算法研究

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The first orbit maneuver of lunar orbit insertion ( LOI) must be implemented at the first perilune of the spacecraft flight to the moon.

月球捕获控制第一次制动必须在卫星飞向月球的第一近月点完成。

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Large Altitude Simulation Test Stand for Orbit Maneuver Motor

变轨发动机大型高空模拟试验台

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Evaluation Analysis on Control Technique of Attitude Based on Spacecraft Orbit Maneuver

基于轨道机动的航天器姿态控制技术评估分析

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Development of Optimal Control Scheme in Orbit Maneuver of Flight Vehicles

飞行器最优机动策略研究方法及进展

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A study on the optimal low-thrust orbit maneuver of lunar satellite

月球卫星最优小推力变轨研究

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Ground Ignition Test of an Orbit Maneuver H_2/ O_2 Thruster Based on Gas Dynamic Resonance Igniter

基于气动谐振点火器的氢氧变轨火箭发动机地面点火试验

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Detection of space target orbit maneuver by wavelet analysis

利用小波分析识别空间目标的轨道机动

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Firstly, it briefly describes technical conditions and methods of synthetic orbit maneuver.

文章首先简要描述了综合变轨的技术条件和策略方法；

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Investigation on head of novel chemical thruster for orbit maneuver

新颖机动变轨化学火箭发动机头部研究

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This paper presents the approaches and practical theoretical models on synthetic orbit maneuver during long distance guidance stage of space rendezvous.

文章研究了空间交会远程导引阶段综合变轨问题的变轨策略方法和实用理论模型。

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Genetic algorithms to solve the multi-objective optimization problems have their unique advantages, and the spacecraft orbit maneuver was a typical multi-objective optimization problem.

遗传算法在解决多目标优化问题中有其独特的优势，而航天器轨道机动是典型的多目标优化问题。

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This paper deduces the orbit maneuver equations for relative motion control of satellite formations based on the relative orbit elements.

导出了基于相对轨道要素的编队飞行卫星群轨道相对运动控制的轨道机动方程；

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Finally, it gives the example simulation of synthetic orbit maneuver under multi impulse during long distance guidance using the self developed simulation software.

然后重点建立了多脉冲综合变轨的轨道动力学模型，并给出了数值求解方法；

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An optimal orbit maneuver method based on continuous low thrust was presented to solve relative motion control.

针对近距离相对运动的轨道控制问题，提出用常值小推力完成最优转移的方法。

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The configuration initialization of satellite formations is carried out based on orbit maneuver control of relative elements.

根据相对轨道要素的变轨机动控制，进行编队飞行卫星群构型的初始化。

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The algorithms for detecting orbit maneuver of artificial satellite

人造卫星变轨检测算法

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Simulation of Satellite Orbit Maneuver with Gauss Formula

利用高斯型方程进行卫星轨道机动仿真

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