Development of micro-processor controlled CCD star trackers for use on Astro-C

Astronomy and Astrophysics – Astronomy

Scientific paper

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Astronomical Satellites, Charge Coupled Devices, Electronic Control, Microprocessors, Star Trackers, X Ray Astronomy, Environmental Tests, Satellite Attitude Control, Satellite Design, Spaceborne Astronomy

Scientific paper

It is planned to launch an X-ray astronomy satellite, called Astro-C, in 1987. The satellite weighs approximately 430 kg and will be injected into a circular orbit of 500 km altitude with 30 deg inclination. Main objectives of the Astro-C are related to the study of extragalactic X-ray sources. A bias-momentum stabilization, implemented with the aid of a momentum wheel, will be utilized. The spacecraft attitude is to be controlled by means of three magnetic torquers. The attitude determination system of the Astro-C consists of an inertial reference unit (IRU), a pair of star trackers (STT), and a two-dimensional sun aspect sensor (SAS). The STT uses a microprocessor for data processing and mode control. Attention is given to the design of the SST, its performance, and test results verifying SST accuracy.

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