Design of attitude control systems for cubesat-class nanosatellite

DOI10.1155/2013/657182zbMath1263.93163OpenAlexW2028180020WikidataQ59012434 ScholiaQ59012434MaRDI QIDQ1953735

Regina Lee, Junquan Li, Mark Post, Thomas Wright

Publication date: 10 June 2013

Published in: Journal of Control Science and Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1155/2013/657182

zbMATH Keywords

numerical simulationnonlinear controllernanosatelliteattitude control systemsproportional-integral-derivative controller.

Mathematics Subject Classification ID

Related Items (2)

Research on high-precision attitude control of joint actuator of three-axis air-bearing test bed ⋮ On stability and stabilization of the linearized spacecraft attitude control system with bounded inputs

Cites Work

• Comparative study of various control methods for attitude control of a LEO satellite
• Smooth sliding-mode control for spacecraft attitude tracking maneuvers

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