Robust adaptive backstepping attitude stabilization and vibration reduction of flexible spacecraft subject to actuator saturation

DOI10.1177/1077546310384001zbMath1271.74156OpenAlexW2108997818MaRDI QIDQ2846374

Qinglei Hu, Bing Xiao

Publication date: 5 September 2013

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

Full work available at URL: https://doi.org/10.1177/1077546310384001

zbMATH Keywords

vibration controlflexible spacecraftattitude stabilizationadaptive backstepping controlsaturation input

Mathematics Subject Classification ID

Vibrations in dynamical problems in solid mechanics (74H45) Adaptive or robust stabilization (93D21)

Related Items (3)

Investigation on attitude disturbance control and vibration suppression for fuel-filled flexible spacecraft ⋮ Nonlinear output feedback control of a flexible link using adaptive neural network: stability analysis ⋮ Nonlinear output feedback control of a flexible link using adaptive neural network: controller design

Cites Work

• Control of underactuated spacecraft with bounded inputs
• Adaptive variable structure maneuvering control and vibration reduction of three-axis stabilized flexible spacecraft
• Lyapunov Optimal Saturated Control for Nonlinear Systems
• Variable structure control and active vibration suppression of flexible spacecraft during attitude maneuver

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