English translation for "orbital maneuver"
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- 轨道机动
Related Translations:
- Example Sentences:
| 1. | Design and simulation of satellite orbital maneuver model on stk
的卫星轨道机动模型设计与仿真 | | 2. | This paper mainly discuss the problem of method and policy of spacecraft ' s large scale orbital maneuver
论文研究了航天器大范围轨道机动的方法与策略。 | | 3. | Orbital maneuver is the primary condition for satellite autonomy , and it is the basis of phase keeping , phase maneuver and rendezvous
卫星轨道机动是卫星自治的首要条件，它是相位保持、相位机动、交会对接的基础。 | | 4. | The dissertation presents a new method for orbital maneuver based on zero effort miss steering , and many problems in this method are studied
本文提出了基于零控流型的卫星轨道机动方法，并对此方法所涉及的具体问题进行了研究。 | | 5. | Unlike comet and asteroid orbital elements which can be reliably used for many months , satellite orbits are constantly changing due to both orbital maneuvering by the satellite and the effects of atmospheric drag
小行星和彗星的轨道计算数据可以使用数月，但是人造卫星不行，因为它们的轨道会随时被人造卫星自己或者大气阻力所修正。 | | 6. | Finally , this paper tried to start a new research field that named as rendezvous area and space control body , by introducing these concept , visualization for large scale orbital maneuver was able to show directly
最后,论文尝试性的提出并研究了点对面的机动及追踪器控制体的概念,给出了高度直观的大范围轨道机动可及范围,从面的覆盖的概念上分析得到了最佳机动时限。 | | 7. | The basis of dynamics and simulation includes the iterative flyout angle algorithm to the solutions to lambert problem and battin ' s universal conic section state extrapolate method . then spacecraft ' s orbit roots , maneuver impulse and maneuver time are discussed as the following four part : first of all , the chaser ' s one orbit roots is selected as a variable to simulate its influence to the large scale orbital maneuver . the research reveals fact that the orbit roots both of chaser and target should be close to each other to achieve better maneuver and rendezvous " ability , moreover , the best orbit maneuver and rendezvous occurs when both chaser and target ' s initial phase angle are equal
为了研究了交会机动中追踪器和目标器的轨道根数、机动时限和机动能耗等因素对交会机动的影响,仿真和分析分为以下四个部分:首先,研究了追踪器轨道单个参数为变量情况下两航天器大范围交会机动问题,研究表明,追踪器的变化参量与目标器相应的参量在接近的情况下可以获得良好的交会机动特性,而对于两航天器轨道共面的情况下,初始相位角相等时则获得最佳的机动效果。 |
- Similar Words：
- "orbital longitude" English translation, "orbital lymphoma" English translation, "orbital lymphosarcoma" English translation, "orbital machining" English translation, "orbital magnetic moment" English translation, "orbital maneuvering system" English translation, "orbital maneuvering system (oms)" English translation, "orbital manoeuvre" English translation, "orbital margin" English translation, "orbital mechanics" English translation
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