Model for solar torque effects on DSCS II

Details Model for solar torque effects on DSCS II Model for solar torque effects on DSCS II

Jun 1976

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1976jansc..24..165s&link_type=abstract

Journal of the Astronautical Sciences, vol. 24, Apr.-June 1976, p. 165-184.

Astronomy and Astrophysics

Astronomy

Satellite Antennas, Satellite Perturbation, Satellite Rotation, Solar Radiation, Spin Stabilization, Synchronous Satellites, Torque, Pointing Control Systems, Satellite Attitude Control, Spin Dynamics

Scientific paper

An analytic model useful in predicting attitude changes of a spin stabilized vehicle which arise from solar torques has been developed. The motivation behind such a development was the requirement to predict such effects for the DSCS II synchronous satellite. The validity of the model has been verified by a comparison of the actual attitude changes of this vehicle, as deduced from telemetry, with the predictions of the theory.

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