抄録
A lot of space satellites are launched and have been developed for launch by Development of space industry in recent years. Robotic arm attached to them is light. Therefore, the rigidity is low. The dynamics of the arm has the vibration from the flexibility. Therefore, it is difficult to stabilize the posture change to the target posture accurately and promptly in the satellite where a flexible robotic arm is attached. The purpose of this research is the influence given to the main body by the vibration is analyzed and we do the angular control and the location control with the force control in movement of the satellite with a flexible robotic arm limited to the gyration in one axis circumference and the keep abreast of movement in one direction.
