Error analysis and a new steering law design for spacecraft control system using SGCMGs

DOI10.1007/S10409-011-0502-4zbMath1270.70080OpenAlexW2053133551MaRDI QIDQ362974

Jing-Rui Zhang, Zao-Zhen Liu, Jin Jin

Publication date: 30 August 2013

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

Full work available at URL: https://doi.org/10.1007/s10409-011-0502-4

zbMATH Keywords

singularity analysisattitude controlsteering lawsingle gimbal controlmoment gyros (SGCMGs)

Mathematics Subject Classification ID

Control of mechanical systems (70Q05) Motion of the gyroscope (70E05)

Related Items (3)

Influence of flexible solar arrays on vibration isolation platform of control moment gyroscopes ⋮ Path planning for rapid large-angle maneuver of satellites based on the Gauss pseudospectral method ⋮ Attitude control of a rigid spacecraft with one variable-speed control moment gyro

Cites Work

• Attitude control for part actuator failure of agile small satellite
• Steering laws analysis of sgcmgs based on singular value decomposition theory

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