国家极地轨道伴随卫星 Suomi NPP
Simulation results indicate that the proposed control method can carry out the suboptimal control of the periodic relative motion.
仿真计算结果表明,所设计的控制律是稳定的,能够以较少的燃料消耗实现伴随轨道的控制。
参考来源 - 基于θ·2,447,543篇论文数据，部分数据来源于NoteExpress
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.
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。
There are some important application values and wide application prospect of relative research on concomitant orbit maneuver application.
此外，文中还提出了“同步伴随轨道”的概念，这在未来航天中可能是有用的。
In addition, a new concept for Synchro-Adjoint Orbit is proposed. It will be very useful in space flight.
应用推荐