Globally stabilizing saturated attitude control in the presence of bounded unknown disturbances

By Robert James Wallsgrove, M. Akella. 2005

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Adaptive Sliding Mode Control for Attitude Stabilization With Actuator Saturation (2011, background): “However, the uncertainty in the inertia matrix is not considered in [12] and [ 13 ].”
Fault-Tolerant Tracking Control of Spacecraft with Attitude-Only Measurement Under Actuator Failures (2014, background): “Analysis and design of attitude systems with actuator saturation were studied in [40–45].”
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”
Indirect Robust Adaptive Fault -Tolerant Control for Attitude Tracking of Spacecraft (2008, background): “A similar assumption was proposed in [13,14,18,22] without considering thrust faults.”
Finite‐time angular velocity observers for rigid‐body attitude tracking with bounded inputs (2017, unknown): “As first introduced in [2], p(2)(t) is a positive sharpness function satisfying 0 < p(2)min≤p(2) t ð Þ < ∞ and _ p t ð Þ∈ ∞.”