Robust Attitude Control Design for Spacecraft under Assigned Velocity and Control Constraints

Abstract

A novel robust nonlinear control design under the constraints of assigned velocity and actuator torque is investigated for attitude stabilization of a rigid spacecraft. More specifically, a nonlinear feedback control is firstly developed by explicitly taking into account the constraints on individual angular velocity components as well as external… (More)
DOI: 10.1016/j.isatra.2013.03.003

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