The invention discloses a method for coordination control over
satellite arms of a space
robot based on an expanded Jacobian matrix. The method achieves integrated coordination control over a space
manipulator operating in
orbit and a base
satellite. The method comprises the steps of computing kinetic parameters and dynamic parameters of the space
robot, establishing a
mathematical model of the space motor based on the expanded Jacobian matrix, designing a coordination controller of the
satellite arms of the space
robot, conducting parameterization on the trajectory of the
tail end of the
manipulator, optimizing the trajectory of the
manipulator, and computing an
angular velocity instruction of a single
gimbal control moment gyro
system of the space robot. According to the method, hysteretic
feedback control conducted by a satellite according to attitude measurement is not needed, overall mathematical modeling is conducted on the
coupled motion of the satellite arms, the
angular velocity instruction of the single
gimbal control moment gyro
system is directly computed according to the input trajectory of the
tail end of the manipulator, the single
gimbal control moment gyro
system is used for compensation, needed by the satellite, for manipulator motion, and then overall coordination control over the satellite arms is realized; the trajectory of the
tail end of the manipulator is optimized, so that the energy consumed by a satellite
state control system for compensating for the restoring torque of the manipulator is small.