The proposed control law is simple and robust, and each controller can be designed independently, based on the semi-globally ISS concept. The stability of the ...
In this paper, the three-axis attitude stabilization of the axisymmetric spacecraft with bounded inputs is studied. By constructing some novel state ...
In this paper, an optimal PID-like controller is proposed for a spacecraft attitude stabilization problem subject to continuous inequality constraints on ...
In this study, a constrained dual-loop attitude control law is proposed for rigid spacecraft with model uncertainties, actuator saturation and bound angular ...
Jan 28, 2022 · A hierarchical controller is designed for the spacecraft attitude stabilization in [43], where the attitude constraints and the input saturation ...
This paper deals with the attitude stabilizing control problem for a rigid spacecraft in the presence of model uncertainties, external disturbances, and.
This paper addresses the attitude stabilization and vibration suppression problem for flexible spacecraft subject to model parameter uncertainty, controller ...
A constrained dual-loop controller is designed for the attitude control of rigid spacecraft with inertia uncertainties, assigned angular velocity and control ...
... Control Theory Applic., 2017, 11, (7), pp. 931–940. 15). 31. Li, M., Hou, M., Yin, C.: 'Constrained dual-loop attitude control design for spacecraft', Aerosp.
Robust Attitude Control Design for Spacecraft under Assigned Velocity ...
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A novel feedback controller under the constraints of assigned velocity and actuator control is investigated for attitude stabilization of a rigid spacecraft ...