Dual attitude and parameter estimation of passively magnetically stabilized nano satellites

Dual attitude and parameter estimation of passively magnetically stabilized nano satellites

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Article ID: iaor20141169
Volume: 94
Issue: 1
Start Page Number: 145
End Page Number: 158
Publication Date: Jan 2014
Journal: Acta Astronautica
Authors: , , ,
Keywords: modelling, aerospace, satellites
Abstract:

  • Attitude dynamics model of nano satellite are calibrated on orbit.
  • Only a measurement of the solar vector is used.
  • Calibrated parameters are shown to differ from pre launch estimates.
  • Attitude determination is performed to a precision of five degrees.
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