Particularly, the method of coverage orbit design is given in view of the orbital period deviation, which is based on recursiveorbit.
特别是,以循环轨道为基础,考虑轨道周期的误差,给出覆盖轨道的设计方法。
2
In this paper, a series of characters for recursiveorbit and coverage orbit of satellites are discussed, and the method of recursiveorbit design is given.