针对高面质比航天器可以利用太阳光压进行轨道控制的特点,本文提出一种太阳帆航天器编队构型维持和重构的方法.该方法通过控制主从航天器太阳帆姿态角和反射系数,调整主从航天器之间的光压差,产生抵消编队成员间相对运动受到摄动差或进行轨道机动时所需的连续小推力,从而实现编队构型的维持和重构.仿真结果表明,在主航天器太阳帆的姿态角和反射系数相对固定的条件下,对于太阳同步轨道上的高面质比太阳帆航天器编队,使用滑模控制方法,能够调整编队中从航天器太阳帆的姿态角和反射系数产生推力抵消摄动力影响,达到长期维持太阳帆航天器编队构型的目的;通过开环控制方法,能够调整编队中从航天器太阳帆的姿态角和反射系数产生连续小推力,在较长时间周期内实现编队重构. In view of the characteristics that the high aspect ratio spacecraft can control the orbital with solar light pressure, this paper presents a method to maintain and reconstruct the formation configuration of the solar sail spacecraft. By controlling the solar sail attitude and reflection Coefficient to adjust the light pressure difference between the master and slave spacecraft to generate the continuous small thrust needed to offset the perturbation of the relative movement between formation members or the orbital maneuver so as to maintain and reconstruct the formation configuration.The simulation results The results show that using the sliding mode control method to adjust the attitude of the main spacecraft solar sail from the sun of the spacecraft to the formation of a solar spacecraft with high surface area ratio and solar reflectance under the relatively fixed attitude and reflection coefficient of the solar sail, Sail posture angle and reflection coefficient produce thrust offset perturbation effect, to achieve the long-term maintenance of solar sail aircraft formation configuration purposes; through open-loop control method can be adjusted formation from the spacecraft solar sail attitude angle and reflection coefficient continuous Small thrust, formation reconstruction in a long period of time.