Guidance, Navigation, and Control System Performance Trades for Mars Pinpoint Landing

著录项

• 来源
  《Journal of Spacecraft and Rockets》 |2010年第1期|188-198|共11页
• 作者

  Bradley A. Steinfeldt; Michael J. Grant; Daniel A. Matz; Robert D. Braun; Gregg H. Barton;

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• 作者单位

  Georgia Institute of Technology, Atlanta, Georgia 30332;

  Georgia Institute of Technology, Atlanta, Georgia 30332;

  rnGeorgia Institute of Technology, Atlanta, Georgia 30332;

  Georgia Institute of Technology, Atlanta, Georgia 30332;

  rnCharles Stark Draper Laboratory, Inc., Houston, Texas 77058;

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• 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
• 原文格式 PDF
• 正文语种 eng
• 中图分类
• 关键词

  a =acceleration vector,a_1,a_2 a_3~T; a_i =acceleration along the j'th direction; b =scalar weighting parameter on the terminal constraint sensitivity; C_(ji) =jth constant coefficient used in the modified Apollo lunar module guidance algorithm; dt_f =terminal time increment;

  机译：a =加速度矢量;[a_1;a_2 a_3]〜T;a_i =沿第j个方向的加速度;b =终端约束灵敏度的标量加权参数;C_（ji）=在修正的阿波罗登月舱制导算法中使用的第j个常数系数;dt_f =终端时间增量;