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Solar sail equilibria with albedo radiation pressure in the circular restricted three-body problem

机译:圆形受限三体问题中具有反照率辐射压力的太阳帆平衡

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Solar Radiation Pressure (SRP) and albedo effects are investigated in the circular restricted three-body problem for a system consisting of the Sun, a reflective minor body and a solar sail. As an approximation of albedo radiation pressure (ARP), the minor body is treated as Lambertian with reflected flux scattered by the bidirectional reflectance distribution function. Incorporating ARP, which is a function of SRP, into the solar sail equations of motion renders additional artificial equilibrium points in a volume between the L_1 and L_2 points which is defined as the region of influence. Based on the model, characterization of the findings are provided that are theoretically applicable to any body with discernible albedo such as for instance Earth, Mars or an asteroid. Example results are presented for a Sun-Vesta system which show that the inclusion of ARP generates artificial equilibrium points requiring solar sail designs with very low mass-to-area ratio. The equilibrium points are found to be unstable in general but asymptotic stability may be enforced with sail attitude feedback control.
机译:在由太阳,反射性小物体和太阳帆组成的系统的圆形受限三体问题中,研究了太阳辐射压力(SRP)和反照率效应。作为反照率辐射压力(ARP)的近似值,次要物体被视为朗伯型,其反射通量由双向反射率分布函数散射。将ARP(是SRP的功能)纳入运动的太阳帆方程,可以在L_1和L_2点之间的体积中定义为影响区域,从而提供其他人工平衡点。基于该模型,提供了这些发现的特征,这些发现在理论上适用于任何具有可辨别的反照率的物体,例如地球,火星或小行星。给出了一个针对Sun-Vesta系统的示例结果,该结果表明,包含ARP会生成人为的平衡点,这需要太阳帆设计具有非常低的质量面积比。人们发现平衡点通常是不稳定的,但是可以通过航行姿态反馈控制来增强渐近稳定性。

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