Influence of flexible solar arrays on vibration isolation platform of control moment gyroscopes

DOI10.1007/S10409-012-0148-XzbMath1345.74091OpenAlexW2009291742MaRDI QIDQ315357

Jing-Rui Zhang, Shi-Jie Xu, Yao Zhang

Publication date: 21 September 2016

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

Full work available at URL: https://doi.org/10.1007/s10409-012-0148-x

zbMATH Keywords

attitude controlcontrol moment gyroscopeultra quiet platformvibration isolation platform

Mathematics Subject Classification ID

Inhomogeneity in solid mechanics (74E05) Impact in solid mechanics (74M20) Motion of the gyroscope (70E05)

Related Items (3)

Combined control of fast attitude maneuver and stabilization for large complex spacecraft ⋮ The transmissibility of nonlinear energy sink based on nonlinear output frequency-response functions ⋮ Attitude control of a rigid spacecraft with one variable-speed control moment gyro

Cites Work

• Error analysis and a new steering law design for spacecraft control system using SGCMGs
• Attitude control for part actuator failure of agile small satellite
• Study on relative orbital configuration in satellite formation flying
• A Newton-Euler formulation for the inverse dynamics of the Stewart platform manipulator
• Underactuated spacecraft angular velocity stabilization and three-axis attitude stabilization using two single gimbal control moment gyros
• A new design approach of PD controllers

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