Modelling the Attitude Noise of the Gaia Spacecraft. A Simplified Approach

Details Modelling the Attitude Noise of the Gaia Spacecraft. A Simplified Approach Modelling the Attitude Noise of the Gaia Spacecraft. A Simplified Approach

Mar 2010

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2010ssrv..151..197k&link_type=abstract

Space Science Reviews, Volume 151, Issue 1-3, pp. 197-207

Astronomy and Astrophysics

Astronomy

Satellite, Astrometry, Simulation, Modelling

Scientific paper

A high-precision attitude determination and control of the forthcoming European Gaia satellite is an essential task for the success of the whole mission. The requirements for the spacecraft’s attitude require exceptional efforts in the simulation of the rotations of the satellite under the influence of continuous and randomly arising effects. This paper describes the structure of a physically-motivated noise model for simulating the attitude in a closed loop configuration. It deals with the analysis of the most important disturbing forces and torques acting on the Gaia spacecraft.

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