1) concomitant orbit
伴随轨道
1.
There are some important application values and wide application prospect of relative research on concomitant orbit maneuver application.
伴随轨道机动应用相关研究具有重要的应用价值和广阔的应用前景。
2.
Two-impulse control is used for concomitant orbital control.
文中利用伴随轨道方程推导出伴随卫星相对运动状态转移方程。
2) Adjoint orbit
伴飞轨道
3) stochastic trajectory
随机轨道
1.
Based on the consideration of the dispersed phase interaction with continuous phase, applying the k-ε model and the stochastic trajectory model with to the gas phase and solid phase,the particle motion trajectory was simulated successfully.
在考虑气相与颗粒固相之间相互作用的前提下,对气相采用带旋流修正的k-ε模型,对颗粒固相采用随机轨道模型,成功地模拟出颗粒的运动轨迹。
4) Trajectories of concomitant satellites
伴随卫星轨迹
5) largrangian stochastic trajectory approach
Lagrangian随机轨道
6) Tributary satellite coordinate system
伴飞卫星轨道系
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