IGS

International GNSS Service

Yaw-Attitude Modelling for Eclipsing Satellites

Verification of Modelling

IGS

OBJECTIVE
Understanding the satellite attitude is important for:
  • Properly relate measurements to the CoM of satellites (esp. Block II/IIA)
  • Correct for the phase wind up effect
  • Modelling solar pressure effects correctly
  • What are ACs are using for the yaw-attitude model for GNSS orbits?
  • What are the differences in ACs yaw-attitude models?
TOPICAL LINKS
COMPARISON DATA SET

The eclipsing yaw-attitude control, for GPS, consists of three distinct regimes:
  1. noon, and midnight (for Block IIR satellites only) turns
  2. maximum yaw rate during a shadow crossing (BLOCK II/IIA only)
  3. post shadow recovery to nominal yaw attitude (BLOCK II/IIA)


Send comments to IGS ACC Privacy Policy 3rd January 2018