The Hipparcos dedicated control system: A case stuudy of a high reliability scientific spacecraft control system

Astronomy and Astrophysics – Astronomy

Scientific paper

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Availability, Ground Based Control, Hipparcos Satellite, Reliability, Satellite Control, Spacecraft Recovery, System Effectiveness, Contingency, Countermeasures, Payloads, Satellite Guidance, Spaceborne Astronomy

Scientific paper

The Hipparcos satellite, launched on 8 Aug. 1989 is described. The Hipparcos mission was planned to prepare catalogues of the position of stars to accuracies at the milliarc second level. In order to achieve this ambitious aim, a continuous uplink of instructions to the payload is necessary. This imposes severe availability and continuity requirements. The effect of these reliability requirements in the ground control system is discussed. The failure of the apogee boost motor firing had the consequence that the geostationary orbit could not be reached. Modifications to the ground control system to accommodate the recovery mission are described. Preliminary figures on availability and continuity since the start of the mission are given which demonstrate how the requirements are being met.

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