通过设计航天器轨道,可使航天器发射入轨后无需机动即实现对Walker星座中非共轨的多颗卫星的快速、近距离接近。给出了该轨道的搜索方法以及基于星座特性的代换法,并给出了仿真示例。 By designing the orbit of the spacecraft, the spacecraft can be launched into the orbit without the need of maneuvering to realize the quick and close proximity to the non-common-rail multiple satellites in the Walker constellation. The search method of the track and the substitution method based on the constellation characteristics are given, and the simulation examples are given.