相对轨道 relative orbit
- 采用相对轨道要素设计了理想的基准伴随轨道。
The periodic relative orbit was designed based on the relative orbit elements and the mission requirements. - 其次,针对编队飞行卫星队形保持控制,以对地等张角绕飞编队为背景设计相对轨道模型预测控制算法。
Secondly, a model predictive control method is designed for the satellite formation keeping and formation of invariant angular to the ground as the background. - 为了得到更丰富的相对轨道,同时考虑到相对速度测量困难,研究了仅利用位置反馈进行相对轨道设计的方法。
With the difficulty of measuring relative velocity considered, a relative orbit design method is proposed to obtain diverse relative orbits with only position feedback.
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