Solar radiation force modeling for TDRS orbit determination

Details Solar radiation force modeling for TDRS orbit determination Solar radiation force modeling for TDRS orbit determination

Oct 1981

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1981fmet.symp.....l&link_type=abstract

In NASA. Goddard Space Flight Center Sixth Ann. Flight Mech./Estimation Theory Symp. 25 p (SEE N82-10064 01-12)

Physics

Loads (Forces), Orbital Position Estimation, Radiation Pressure, Satellite Orbits, Solar Radiation, Ephemerides, Flight Mechanics, Orbit Calculation, Radiation Effects, Satellite Tracking

Scientific paper

The relative orbit determination accuracies resulting from several TDRS models are evaluated. These models include spherical, single-plate, and restricted two-plate models. The plate models can be adjusted in both area and reflectivity through differential correction. The restricted two-plate model has an Earth-pointing plate and a solar plate; the orientation of the solar plate is restricted to rotation about an axis perpendicular to the satellite's orbital plane.

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