Investigation on attitude disturbance control and vibration suppression for fuel-filled flexible spacecraft

DOI10.1007/s10409-015-0431-8zbMath1342.70070OpenAlexW2223546480MaRDI QIDQ740012

Bao-Zeng Yue, Xiao-Juan Song, Wen-tsün Wu

Publication date: 11 August 2016

Published in: Acta Mechanica Sinica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10409-015-0431-8

zbMATH Keywords

adaptive sliding modefuel-filled flexible spacecraftLyapunov approach control lawthermal payload

Mathematics Subject Classification ID

Control of mechanical systems (70Q05)

Related Items

Modal parameter identification of flexible spacecraft using the covariance-driven stochastic subspace identification (SSI-COV) method

Cites Work

• Attitude maneuver of liquid-filled spacecraft with a flexible appendage by momentum wheel
• High dimensional integration of smooth functions over cubes
• Robust adaptive backstepping attitude stabilization and vibration reduction of flexible spacecraft subject to actuator saturation
• A composite control scheme for attitude maneuvering and elastic mode stabilization of flexible spacecraft with measurable output feedback
• Attitude manoeuvre of spacecraft with long cantilever beam appendage by momentum wheel
• Solution theorems for the standard eigenvalue problem of structures with uncertain-but-bounded parameters
• A tangent modulus method for rate dependent solids
• Barycentric Lagrange Interpolation
• Variable structure control and active vibration suppression of flexible spacecraft during attitude maneuver