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中文摘要：
利用太阳光压力可以实现地日限制性三体问题中L2点附近编队控制．该编队需要的控制力量级小，常规的推进方式难以实现．太阳帆能产生微小的连续光压力，可以用于Halo轨道附近的编队控制．由于太阳光压力的方向受到限制，只有部分编队构型可以利用太阳光压力实现．该文主要讨论了两种常见的编队构型——直线编队和圆编队，给出了太阳帆能实现的编队构型需要满足的条件．最后，对每种构型的编队进行了数值仿真，仿真结果表明太阳帆能有效的进行编队控制．
英文摘要：
Solar radiation pressure is made use to control the formation flying around L2 libration point in the Sun-Earth system. Controlling formation flying around a Halo orbit requires very thrust that cannot be satisfied by latest thrusters. Key contribution of this paper is the low continuous thrust produced by the solar radiation pressure to achieve the tight formation flying around libration point. However, only certain families of formation types can be controlled by solar radiation pressure force since the direction of solar radiation pressure is restricted to certain range. Two types of feasible formation using solar radiation pressure force control were designed. The conditions of the feasible formations were given analytically. Simulations were given for each case and the restflts show that the formations are well controlled by the solar radiation pressure.
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Satellite scheduling considering maximum observation coverage time and minimum orbital transfer fuel
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