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Let’s define the state vector \(\textbf{X}\) of the lunar module (LM) as \(\textbf{X} = (\textbf{R},\textbf{V},\textbf{A},\textbf{J},\textbf{S})\) . This definition of the state vector will be used throughout the monograph. Time interval between terminal instant and middle points of the approach phase is computed as [1].

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Approach-Phase Ground-Based Targeting

  • 章节

  • 发表日期：

    2026年

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  • Dilmurat M. Azimov,
  • Robert H. Bishop

摘要

Let’s define the state vector \(\textbf{X}\) of the lunar module (LM) as \(\textbf{X} = (\textbf{R},\textbf{V},\textbf{A},\textbf{J},\textbf{S})\) . This definition of the state vector will be used throughout the monograph. Time interval between terminal instant and middle points of the approach phase is computed as [1].