Targeting Ballistic Lunar Capture Trajectories Using Periodic Orbits

著录项

• 来源
  《Journal of guidance, control, and dynamics》 |2011年第3期|p.893-902|共10页
• 作者

  Paul Ricord Griesemer; Cesar Ocampo; D. S. Cooley;

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• 作者单位

  University of Texas at Austin, Austin, Texas 78712,Department of Aerospace Engineering and Engineer-ing Mechanics, 1 University Station C0600;

  University of Texas at Austin, Austin, Texas 78712,Department of Aerospace Engineering and Engineer-ing Mechanics, 1 University Station C0600;

  NASA Goddard Space Flight Center, Greenbelt, Maryland 20771,Navigation and Mission Design Branch, Mail Stop 595.0;

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• 收录信息
• 原文格式 PDF
• 正文语种 eng
• 中图分类
• 关键词

  a; acceleration vector of spacecraft in a coordinate system centered on Earth-moon barycenter; c; Jacobi constant in circular restricted three-body problem; c; constraint vector in targeting and optimization algorithms; F(t); state propagation matrix; f_m; true anomaly in moon-centered coordinate frame; et al;

  机译：一个;航天器在以月球重心为中心的坐标系中的加速度矢量;C;圆约束三体问题中的雅可比常数;C;目标和优化算法中的约束向量;F（t）;状态传播矩阵调频;月球中心坐标系中的真实异常;等;