NASA NTRS · 20060030142
Doppler aided attitude determination for spin stabilized spacecraft
Abstract
This paper describes the theory of spin signature removal and the results obtained during the Genesis and Contour missions, during which spin axis pointing measurement errors of 1 degree or less were achieved.
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Han, D., McElrath, T., Taylor, T., Howell, D., Voth, C.. 2003-02-09. Doppler aided attitude determination for spin stabilized spacecraft. https://ntrs.nasa.gov/citations/20060030142
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