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A composite control scheme for attitude maneuvering and elastic mode stabilization of flexible spacecraft with measurable output feedback

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Publication:2853541
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DOI10.1016/J.AST.2007.06.007zbMath1273.70056OpenAlexW2029930464MaRDI QIDQ2853541

Qinglei Hu

Publication date: 22 October 2013

Published in: Aerospace Science and Technology (Search for Journal in Brave)

Full work available at URL: http://www.sciencedirect.com/science/article/pii/S1270963807000971


zbMATH Keywords

vibration controlflexible spacecraftpiezoelectric materialsadaptive sliding mode control (ASMC)positive position feedback (PPF)


Mathematics Subject Classification ID

Feedback control (93B52) Vibrations in dynamical problems in solid mechanics (74H45) Control of mechanical systems (70Q05) Orbital mechanics (70M20)


Related Items (2)

Dynamics and control of a smart flexible satellite moving in an orbit ⋮ Investigation on attitude disturbance control and vibration suppression for fuel-filled flexible spacecraft







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