地球同步轨道薄膜太阳帆的姿态轨道控制方法

doi:10.7527/S1000-6893.2020.24291

Abstract

Abstract: The film solar sailcraft (FSS) with variable reflectivity is a huge flexible spacecraft capable of propulsion, electric power generation, and attitude and orbit control. The FSS can generate force and torque for attitude and orbit control via varying film reflectivity. In this paper, the orbit drifting motion is analyzed according to the force characteristics of the FSS on the geostationary orbit, and the dynamics model and force and torque model of variable film reflectivity for the FSS are built respectively. Based on the proposed models, an orbit correction method is presented to change the attitudes of the FSS. A stable and reliable attitude control method with double momentum wheels fixed in the plane of the FSS is also proposed. The momentum accumulation of the wheels for attitude control can be unloaded by the solar torque produced from variable film reflectivity. The mathematical simulations show that the proposed methods are reasonable and fit for engineering applications, enabling the FSS to work at a fixed longitude position over a long period of time.

Key words: film solar sailcraft, geosynchronous orbits, attitude and orbit control, super large flexible spacecraft, film reflectivity

CLC Number:

V412.4

WU Yunli, ZHAO Tianyi, ZUO Huaping, MENG Bin. Orbit and attitude control design for film solar sailcrafts on geosynchronous orbit[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(S2): 724291-724291.

References

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Orbit and attitude control design for film solar sailcrafts on geosynchronous orbit

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