Influence analysis of measurement errors in satellite attitude determination based on extended Kalman filter

著录项

• 来源
  《The Aeronautical Journal》 |2012年第1178期|p.373-389|共17页
• 作者

  Y. Jiao; J. Wang; X. Pan; H.Zhou;

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• 作者单位

  Department of Mathematics and Systems Science National University of Defense Technology Hunan, China;

  Department of Mathematics and Systems Science National University of Defense Technology Hunan, China;

  Department of Mathematics and Systems Science National University of Defense Technology Hunan, China;

  Space Intelligent Control Key Laboratory of Science and Technology for National Defense Beijing, China,Department of Mathematics and Systems Science National University of Defense Technology Hunan, China;

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• 原文格式 PDF
• 正文语种 eng
• 中图分类
• 关键词

  A(q): attitude matrix parameterised using the quaternion; b: constant drift; C: estimated value of innovation sequence's autocorrelation function; d: interrelated drift; E●: expectation et al;

  机译：A（q）：使用四元数参数化的姿态矩阵;b：恒定漂移;C：创新序列自相关函数的估计值;d：相关的漂移;E [●]：期望等;