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Attitude tracking of rigid spacecraft subject to disturbances of unknown frequencies

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Outgoing claims: the papers this work cites, builds on, or argues with.

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On the design of robust servomechanisms for minimum phase nonlinear systems

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Attitude stabilization of rigid spacecraft with finite‐time convergence

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Uniform Output Regulation of Nonlinear Systems: A Convergent Dynamics Approach

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Stabilization of the attitude of a rigid spacecraft with external disturbances using finite-time control techniques

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A Lyapunov's direct method for the global robust stabilization of nonlinear cascaded systems

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Parameter convergence and minimal internal model with an adaptive output regulation problem

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Global stabilization and disturbance suppression of a class of nonlinear systems with uncertain internal model

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Design of Robust Adaptive Controllers for Nonlinear Systems with Dynamic Uncertainties

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Spacecraft Dynamics and Control

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Closed-loop manipulator control using quaternion feedback

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Nonlinear H/sub ∞/ control and its application to rigid spacecraft

inferredcites →https://doi.org/10.1109/9.763225openalex-snapshot

Inverse optimal stabilization of a rigid spacecraft

inferredcites →https://doi.org/10.1109/9.940923openalex-snapshot

Semi-global nonlinear output regulation with adaptive internal model

inferredcites →https://doi.org/10.1109/cdc.2002.1184873openalex-snapshot

A constructive proof of ISS small-gain theorem using generalized scaling

inferredcites →https://doi.org/10.1109/tac.2003.817926openalex-snapshot

Limit sets, zero dynamics, and internal models in the problem of nonlinear output regulation

inferredcites →https://doi.org/10.1109/tac.2004.839236openalex-snapshot

A General Framework for Tackling the Output Regulation Problem

inferredcites →https://doi.org/10.1109/tac.2005.858694openalex-snapshot

Inverse optimal adaptive control for attitude tracking of spacecraft

inferredcites →https://doi.org/10.1109/tac.2008.2008350openalex-snapshot

Attitude Tracking and Disturbance Rejection of Rigid Spacecraft by Adaptive Control

inferredcites →https://doi.org/10.1109/tac.2008.927789openalex-snapshot

Unit Quaternion-Based Output Feedback for the Attitude Tracking Problem

inferredcites →https://doi.org/10.1109/tac.2011.2150330openalex-snapshot

Global Disturbance Rejection of Lower Triangular Systems With an Unknown Linear Exosystem

inferredcites →https://doi.org/10.1109/tcst.2007.916352openalex-snapshot

Attitude Control of Missile Via Fliess Expansion

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Adaptive Asymptotic Tracking of Spacecraft Attitude Motion with Inertia Matrix Identification

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Spacecraft Adaptive Attitude and Power Tracking with Variable Speed Control Moment Gyroscopes

What points at this work

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