In this paper, thinking of three-satellite constellation, optimal impulse orbit transfer is studied for constellation launching.
文中基于卫星相对运动状态转移方程,推出了星座双脉沖式变轨控制的理论解;
In this paper, thinking of small satellite constellation, optimal impulse orbit transfer is studied for constellation launching.
针对小卫星星座,进行星座发射中的最优脉沖式变轨研究。
Microwave plasma thruster (MPT) was applied to the sub system of DFH 3 satellite to complete its orbit transfer (OT) and north south station keeping (NSSK).
The results show that the algorithm developed here can monitor and determine whether engine works well or failure precisely and quickly during orbit transfer process.