姿态四元数相关问题

Abstract

Abstract:

The quaternion calculation for spacecraft attitude determination is investigated in this paper，including the transformation between quaternion and the direction cosine matrix，the quaternion differential equation，the selection of time steps for integrating the quaternion equation，and the compensation methods for the noncommutativity error in high dynamic motion．The dual quaternion is also addressed．

Key words: font-family:Calibri, sans-serif, attitude determination">attitude determinationfont-family:宋体, ')">">, font-family:Calibri, sans-serif, direction cosine matrix">direction cosine matrixfont-family:宋体, ')">">, font-family:Calibri, sans-serif, quatemion"> quatemionfont-family:宋体, ')">">, font-family:Calibri, sans-serif, noncommutatiVity error"> noncommutatiVity errorfont-family:宋体, ')">">, font-family:Calibri, sans-serif, dual quatemion">dual quatemion')">">

CLC Number:

V448.22

MA Yanhong, HU Jun. On Attitude Quaternion[J].Aerospace Contrd and Application, 2008, 34(3): 55-60.

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On Attitude Quaternion

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