1) Phase orbit
相轨道
2) phasing orbit
调相轨道
1.
The first is phasing orbits segment which includes three orbits with periods of 16,24 and 48 hours;The second is translunar-trajectory being key part of the flight.
嫦娥一号的这条飞行轨道由三大部分组成:第一部分是绕地飞行的调相轨道,它们由周期为16h、24h、48h的三段轨道组成;第二部分是关键的地月转移轨道;第三部分是200km高度绕月飞行的使命轨道。
3) Relative orbit
相对轨道
1.
Study on perturbations in the relative orbit of satellite formation flying;
卫星编队飞行相对轨道的摄动研究综述
2.
J_2 perturbation effect on relative orbital configuration of satellites in formation flying;
J_2摄动对编队飞行卫星相对轨道构形的影响
3.
J2 perturbation makes the relative orbit drift in the in-track direction, nutation or procession.
详细分析了J2摄动对编队卫星相对轨道构形的影响。
4) similarity orbit
相似轨道
1.
Theorem about the similarity orbit closure of linear bonded operator acting of hilbert space;
Hilbert 空间有界线性算子相似轨道一个定理的证明
2.
With the theory of similarity orbits, it is proved that there is only one nontrivial similarity invariant subspace in C_1, and no nontrivial similarity invariant subspace in C_p(1<p<∞), At the same time, the representations of bounded linear maps which prserve similarity in both directions are given.
利用相似轨道理论,证明了C_1中有唯一的非平凡相似不变子空间,C_p(1
3.
Given T∈B(H), the equivalence class containing T with respect to unitary equivalence (similarity), denoted by U(T)(S(T)), is called the unitary orbit (similarity orbit, respectively) of T.
若T∈B(H),那么S[π(T)]和S(T)分别表示π(T)和T的相似轨道。
5) orbit phase diagram
轨道相图
1.
We analyse the stability of the central-field orbit with the orbit phase diagram induced from the Binet s formula,and prove that the ordit in the central field-which is inverse ratio-are stable at any case.
利用由比尼公式得到的“轨道相图”分析有心力为轨道的稳定性,证明平方反比有心力作用下的轨道,不论其形式如何都是稳定的,并用线性稳定性方法证明在有心力F=K~2m/r~2的作用下,质点运动轨道稳定与不稳定分界点n的取值范围为2
6) phase trajectory
相位轨道
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