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月球卫星的精密定轨
引用本文:刘迎春, 刘林. 月球卫星的精密定轨[J]. 空间科学学报, 2002, 22(3): 249-255.
作者姓名:刘迎春  刘林
作者单位:南京大学天文系,南京,210093;南京大学天文系,南京,210093
基金项目:国家自然科学基金(10173006),高等院校博士点基金(2000028416)共同资助课题
摘    要:发射月球卫星是探测月球的一个重要途径,而且为了找水,多采用极轨方式.由于作为中心天体的月球与地球有所不同,导致月球卫星的运动及其相应的轨道摄动解亦有明显差异.在这种背景下,本文选择采用一组适用于0≤e<1和0°≤i<180°的无奇点根数、充分利用数值法和分析法各自特点的定轨方法,给出月球卫星的精密定轨方案,并以测距的模拟资料进行了实算,计算结果与理论分析相符,有实用前景.

关 键 词:月球卫星-无奇点根数-精密定轨
收稿时间:2001-10-05
修稿时间:2001-10-05

A METHOD ON THE PRECISE ORBIT DETERMINATION FOR LUNAR SATELLITE
LIU Yingchun, LIU Lin. A METHOD ON THE PRECISE ORBIT DETERMINATION FOR LUNAR SATELLITE[J]. Chinese Journal of Space Science, 2002, 22(3): 249-255.
Authors:LIU Yingchun LIU Lin
Affiliation:Department of Astronomy, Nanjing University, Nanjing 210093, China
Abstract:Lunar satellite is the most popular concept in the recent and future lunar exploration missions, such as Clementine (NASA, 1994), Lunar Prospector (NASA, 1998) and Smart-1 (ESA, 2002). The scientific goals of these missions, such as the global mapping, the determination for the high resolution of the lunar gravitational potential and the lunar mass, require the precise orbit determination support. Comparing with that of the Earth satellite, the motion of the lunar satellite could still be regarded as a perturbed two-body problem. However, it is complicated by the fact that the Moon, as the central body of the satellite, is different from the Earth, such as it is rotating slowly, it has no atmosphere, and its harmonic coefficient of the oblate, J2, isn't much larger than other harmonic coefficients. All of these bring us both the advantage and the disadvantage in building an analytical perturbing theory for the lunar satellite. And the corresponding analytical solution of the motion is not the same as that of the Earth satellite. It is not convenient to use the analytical theory directly during the procedure of orbit determination. A numerical method that combines with some properties of the analytical method seems to be a wise choice, which is investigated in this paper. Since the lunar satellite is usually in the polar orbit for finding the water, we use a set of non singular orbital elements to discuss the precise orbit determination for lunar satellite, which is suitable for the lunar orbiter with 0≤e <1 and 0°≤ i < 180°. Then we could take the most advantage of both the analytical method and the numerical method. An overall strategy and make a simulation with the range data is given in the paper. The result is in agreement with the theoretical analysis and suggests that this strategy have a practical prospect.
Keywords:Lunar satellite   Nonsingular orbital elements   Precise orbit de-termination
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