Study on Displaced Orbits Below the Moon’s South Pole Near L2 Point Based on Solar Sail

Q4 Engineering
W. Yu, O. L. Starinova
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引用次数: 0

Abstract

This work explores displaced orbits of solar sails below the Moon’s south pole, near the L2 libration point in the Earth-Moon system. Light pressure provides acceleration for displaced orbits. These orbits enable continuous communication and observation of the Moon’s south polar region, where a lunar base is planned. Linearized dynamic equations yield analytical solutions of displaced orbits, which are either quasi-periodic or periodic. Quasi-periodic orbits have varying altitudes of hundreds of kilometers and a period of about a year, while periodic orbits have fixed altitudes аnd the same period. A sliding mode controller maintains the orbits using sail attitude angles and reflectivity as control variables. With a reflective area to mass ratio of 18 m2/kg, the displaced heights of quasiperiodic and periodic orbits near L2 are 2010.38 km and 2210.06 km, respectively. Numerical simulations confirm the controller’s effectiveness for both orbit types
基于太阳帆的月球南极附近 L2 点以下的位移轨道研究
这项工作探索了月球南极下太阳帆的位移轨道,在地月系统的L2振动点附近。轻压为位移轨道提供加速度。这些轨道可以实现对月球南极地区的持续通信和观测,月球南极地区是计划建立月球基地的地方。线性化动力学方程得到了准周期或周期位移轨道的解析解。准周期轨道的高度变化为数百公里,周期约为一年,而周期轨道的高度固定,周期相同。滑模控制器使用船帆姿态角和反射率作为控制变量来维持轨道。L2附近准周期轨道和周期轨道的位移高度分别为2010.38 km和2210.06 km,反射面积质量比为18 m2/kg。数值仿真验证了该控制器对两种轨道类型的有效性
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来源期刊
Mekhatronika, Avtomatizatsiya, Upravlenie
Mekhatronika, Avtomatizatsiya, Upravlenie Engineering-Electrical and Electronic Engineering
CiteScore
0.90
自引率
0.00%
发文量
68
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