1) orbital circularization
轨道圆化
2) Circlet polarization track
圆环极化轨道
3) quantized elliptical orbit
量子化椭圆轨道
1.
A quantized elliptical orbit of electron in hydrogen_like atom is concisely derived from Binet equation with the aid of Bohr_Sommerfeld s quantized condition.
从比耐公式出发 ,结合玻尔———索末菲量子化条件 ,对类氢原子电子的量子化椭圆轨道 ,给出了一个简化的推导 ,并在此基础上 ,对轨道的稳定性进行进一步的讨论。
4) cirular radius variation
圆形轨道变化
5) γ circular polarization tracks
γ圆极化轨道
6) 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。
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