This invention relates to the field of
spacecraft attitude control technology, and more particularly to an ultra-precise and ultra-stable on-
orbit adaptive control method and
system for pointing under additional stiffness disturbances. This on-
orbit adaptive control method, by applying specific excitations to actuators and measuring their responses, combined with a recursive filtering
algorithm, can accurately identify the total
actuator stiffness, including the additional stiffness of the cable, in real-time on-
orbit, overcoming problems caused by differences in
ground testing environments and time-varying stiffness. Based on the real-time identified stiffness values, the parameters of the axial compensation controller and the
actuator compensation controller are dynamically adjusted, enabling the
control system to adapt to changes in the additional stiffness of the cable and maintain excellent control performance at all times. By employing dual compensation control at the
axial load level and the
actuator level, additional stiffness disturbances are synergistically suppressed at both the overall
system and local actuator levels, improving the comprehensiveness and accuracy of control, and achieving ultra-precise and ultra-stable on-orbit
adaptive control for pointing under cable additional stiffness disturbances.