An attitude control apparatus (20) includes an ideal thrust direction calculator (22), an ideal attitude calculator (24), a target attitude calculator (26), and a torque calculator (28). The ideal thrust direction calculator (22) calculates an ideal thrust direction of a thruster. The target attitude calculator (26) calculates a target attitude that is the attitude of a satellite in which a deviation from an ideal attitude is minimized within a movement limitation of an attitude control actuator (14) while a panel surface faces the sun. The torque calculator (28) calculates a torque for turning the satellite from an actual attitude to the target attitude and transmits a torque instruction to the attitude control actuator (14).
ORIENTATION CONTROL DEVICE, SATELLITE, ORIENTATION CONTROL METHOD, AND PROGRAM
AUSRICHTUNGSSTEUERUNGSVORRICHTUNG, SATELLIT, AUSRICHTUNGSSTEUERUNGSVERFAHREN UND PROGRAMM
DISPOSITIF DE COMMANDE D'ORIENTATION, SATELLITE, PROCÉDÉ DE COMMANDE D'ORIENTATION ET PROGRAMME
07.06.2023
Patent
Elektronische Ressource
Englisch
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