1) elliptic orbiting capture
椭圆轨道捕获
2) Orbit capture
轨道捕获
3) elliptical orbit
椭圆轨道
1.
Relative dynamics and initialization condition for formation flying in elliptical orbits;
椭圆轨道编队飞行相对动力学初始化条件
2.
The configuration stability of the elliptical orbit satellite constellation requires the stabilization of the ascending node right ascension,the argument of perigee and the mean anomaly at the same time.
椭圆轨道星座构型稳定性要求同时实现升交点赤经、近地点幅角和平近点角的稳定。
3.
A theorem that the elliptical orbit parameters can be acquired by the latitudes and longitudes of flyer which flies around the earth with the gravitation is given and proved.
就能唯一确定它的椭圆轨道参数。
4) Ellipse orbit
椭圆轨道
1.
With the application of quanta general rule and ellipse equation, this paper concludes the relation between ellipse orbit and quantum number.
运用量子化通则和椭圆参数方程推导电子椭圆轨道的长半轴a和短半轴b与主量子数n、角量子数nφ、径量子数nr的关系。
2.
According to the requirement of application and design of early warning satellite covering with the northern hemisphere of earth,the project of non-isomorphic early warning satellites constellation is put forward using coverage characteristics of ellipse orbit,which is composed of ellipse orbit satellites and equator circle orbit satellites.
针对北半球预警卫星的应用背景和设计要求,结合椭圆轨道的覆盖特点,提出了一种由中椭圆轨道卫星和赤道圆轨道卫星组成的异构预警卫星星座设计方案,并对该预警星座的预警性能进行了仿真分析。
5) Elliptic orbit
椭圆轨道
1.
Aconcise discussion of elliptic orbit and energy level in hydrogen atom;
氢原子椭圆轨道和能级的简明讨论
6) orbital ellipse
轨道椭圆
补充资料：轨道保持(见航天器轨道控制)
轨道保持(见航天器轨道控制)
orbit keeping
guidQo baoehi轨道保持(o rbit keePing)见航天器轨道控制。
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