The small satellite mission CHAMP was initiated by the German Aerospace Cen
ter (DLR) as a lead project for the East German space industry in order to
consolidate their national and international position. After a short survey
over the mission goals the main requirements on the Attitude and Orbit Con
trol System (AOCS) of the satellite will be outlined. Furthermore the techn
ical solution will be described which fulfils best the requirements on the
AOCS. For that a functional block diagram is given, which shows the sensors
and actuators in use. In the following the operational AOCS Modes and the
sensor data processing up to the generation of actuator commands are descri
bed. Finally this paper outlines that the system is currently in the test s
tatus and that the system has been realised under strong cost and schedule
constraints. (C) 2000 Elsevier Science Ltd. All rights reserved.