Provided is a method of controlling horizontal translational motion of a rocket without changing the attitude of the body and without increasing manufacturing costs and operation costs. This allows for accurate execution of rocket landing operation. A rocket control system includes a gimbal actuator that controls a steering angle of a gimbal mechanism located on a lower side of the body of the rocket with respect to the center of gravity; a fin actuator that controls a steering angle of an attitude control fin located on an upper side of the body of the rocket with respect to the center of gravity; a measurement unit that measures a physical quantity related to motion of the body of the rocket; and a control unit that controls the gimbal mechanism and the attitude control fin according to a result of measurement by the measurement unit to control horizontal translational motion of the rocket.
ROCKET CONTROL SYSTEM AND METHOD OF CONTROLLING LANDING OPERATION OF ROCKET
RAKETENSTEUERUNGSSYSTEM UND VERFAHREN ZUR STEUERUNG DES LANDEBETRIEBS EINER RAKETE
SYSTÈME DE COMMANDE DE FUSÉE ET PROCÉDÉ DE COMMANDE D'OPÉRATION D'ATTERRISSAGE DE FUSÉE
2023-05-24
Patent
Elektronische Ressource
Englisch
ROCKET CONTROL SYSTEM, AND METHOD FOR CONTROLLING LANDING OPERATION OF ROCKET
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