Nonlinear H~ ¿ Flight Control of General Six-Degree-of-Freedom Motions

By C. Yang, C. Kung. 2000

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Attitude Tracking and Disturbance Rejection of Rigid Spacecraft by Adaptive Control (2009, methodology): “TTITUDE control of spacecraft systems has been a benchmark control problem and has been extensively studied under various assumptions and scenarios [1], [6], [12], [17], [ 20 ], [21].”
Inverse optimal adaptive control for attitude tracking of spacecraft (2005, background): “In comparison with the suboptimal controllers in [15], [16], [24], [25] that were designed for the attitude stabilizing problem and required the -gain to be larger than certain values, the inverse optimal adaptive controller presented in this paper allows the disturbance attenuation level of the clo”