Spacecraft attitude control by combination of various torquers

DOI10.1080/00207720902974587zbMath1175.93105OpenAlexW2008947464MaRDI QIDQ3644975

Hyochoong Bang, H. Leeghim, Donghun Lee, Kyungwon Lee

Publication date: 16 November 2009

Published in: International Journal of Systems Science (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1080/00207720902974587

zbMATH Keywords

least square methodsaerospace controlsingularity avoidancecontrol moment gyrosvirtual actuatorsmagnetic torquers

Mathematics Subject Classification ID

Design techniques (robust design, computer-aided design, etc.) (93B51) Control/observation systems governed by ordinary differential equations (93C15)

Related Items (1)

Decentralised finite-time attitude synchronisation and tracking control for rigid spacecraft

Cites Work

• Inverse Kinematic Solutions With Singularity Robustness for Robot Manipulator Control
• Quaternion feedback for spacecraft large angle maneuvers

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