Satellite-to-satellite attitude control of a long-distance spacecraft formation for the next generation gravity mission

DOI10.1016/j.ejcon.2015.03.003zbMath1360.93015OpenAlexW2050488291MaRDI QIDQ522883

Enrico Canuto, Luigi Colangelo, Mauricio Lotufo, Sabrina Dionisio

Publication date: 19 April 2017

Published in: European Journal of Control (Search for Journal in Brave)

Full work available at URL: http://porto.polito.it/2569336/

zbMATH Keywords

attitude controlgravimetryhybridizationdrag-free controlpointing control

Mathematics Subject Classification ID

Application models in control theory (93C95) Variable mass, rockets (70P05) Decentralized systems (93A14)

Related Items (1)

Control of systems with sector-bounded nonlinearities: robust stability and command effort minimization by disturbance rejection

Cites Work

• Unnamed Item
• Drag-free and attitude control for the GOCE satellite
• The internal model principle of control theory
• Bode's integral theorem for discrete-time systems
• Right half plane poles and zeros and design tradeoffs in feedback systems
• Pole Placement by Static Output Feedback for Generic Linear Systems
• High-Gain Observers in Nonlinear Feedback Control
• The output control of linear time-invariant multivariable systems with unmeasurable arbitrary disturbances

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