Output feedback attitude control for rigid spacecraft under attitude constraints

DOI10.3934/jimo.2022173OpenAlexW4296368851MaRDI QIDQ2691448

Yanyan Li

Publication date: 29 March 2023

Published in: Journal of Industrial and Management Optimization (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.3934/jimo.2022173

zbMATH Keywords

spacecraft attitude controlanti-unwinding attitude controlattitude pointing constraintspotential funcitonunmeasurable angualr velocity

Mathematics Subject Classification ID

Stabilization of systems by feedback (93D15)

Uses Software

• Visual MISER

Cites Work

• Visual MISER: an efficient user-friendly visual program for solving optimal control problems
• Rigid-body attitude stabilization with attitude and angular rate constraints
• A control parametrization based path planning method for the quad-rotor UAVs
• Adaptive attitude tracking control for rigid spacecraft with finite-time convergence
• Attitude control without angular velocity measurement: a passivity approach
• Quadratically Constrained Attitude Control via Semidefinite Programming
• Applied and Computational Optimal Control

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