ARTIFICIAL SATELLITE CONFIGURATION FOR CONTINUOUS ATTITUDE MONITORING FOLLOWING THREE AXES

摘要

IT IS CHARACTERIZED BY A SERVICE MODULE 21 CARRYING OPTICAL STABILIZATION DEVICES 25, 26 RELATIVE TO TWO INERTIALLY FIXED TARGETS AND SOLAR PANELS 23 FIXED RIGIDLY TO EXTEND IN THE ORBITAL PLAN AND NEVER OBSTRUCT THE FIELD OF VIEW OF THE DEVICES OF STABILIZATION. THE PAYLOAD MODULE 22 IS ATTACHED TO A SIDE OF THE SERVICE MODULE VIA A ROTATING INTERFACE DEVICE 24.