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Periodic Orbits Design based on the Center Manifold Theory in the Circular Restricted Three-Body Problem

机译:周期性轨道设计基于中心歧管理论在循环限制的三体问题中

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This paper proposes a design method for a three-dimensional periodic orbit in the vicinity of a collinear libration point in the circular restricted three-body problem. The proposed method consists of two steps: the orbit design step and the correction step. The first step is based on the center manifold theorem and systematically provides a quasi-periodic orbit parametrized by a single parameter vector. In the second step, the parameter vector in the first step is corrected by using the state transition matrix. The advantage of the proposed method is that it requires neither an initial guess for a periodic orbit in advance nor complex algebraic manipulations, hence it is easy to implement in computers. Two types of correction equations are derived and verified in numerical simulations.
机译:本文提出了在循环限制的三体问题中的基线释放点附近的三维周期轨道的设计方法。所提出的方法包括两个步骤:轨道设计步骤和校正步骤。第一步基于中心歧管定理,并系统地提供由单个参数向量的准周期性轨道轨道化。在第二步中,通过使用状态转换矩阵校正第一步骤中的参数向量。所提出的方法的优点在于,它既不需要提前的周期性轨道初始猜测,也不需要复杂的代数操作,因此在计算机中易于实现。在数值模拟中导出和验证两种类型的校正方程。

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