Robust Adaptive Variable Structure Control of Spacecraft Under Control Input Saturation

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Adaptive Sliding Mode Control for Attitude Stabilization With Actuator Saturation (2011, background): “In [14] and [15], the research work gives a control design based on the assumption that the external disturbance is bounded by a known upper bound.”
Robust adaptive sliding mode attitude maneuvering and vibration damping of three-axis-stabilized flexible spacecraft with actuator saturation limits (2009, background): “Extensive results pertaining to spacecraft attitude control systems containing actuator saturation nonlinearities have been presented by Boskovi´ Li, and Mehra [ 8 , 9], Tsiotras and Luo [17], Robinett et al. [18], Wallsgrove and Akella [19]; Yakoubi and Chitour [20], Xu and Lam [21], and Grimm et a”
Inertia-Free Spacecraft Attitude Tracking with Disturbance Rejection and Almost Global Stabilization (2009, background): “An additional consideration in spacecraft control is the need to account for constraints on the magnitudes of the control torques [19–21].”