Abstract: During the practical applications, the existence of measurement biases brings a great challenge to the attitude control design because they can lead to the mismatched disturbances in the spacecraft attitude kinematics. In ...

Abstract: In this paper, a robust adaptive iterative learning control (ILC) scheme is developed for the high-precision attitude tracking control of spacecraft in the presence of parametric uncertainties and external disturbances. ...

Abstract: In this paper, we present an adaptive control strategy for the output-constrained attitude tracking of rigid spacecraft under unknown inertia and disturbances. The designed controller is recursively constructed under the ...