Model predictive control of rigid spacecraft with two variable speed control moment gyroscopes

DOI10.1007/s10483-017-2278-9zbMath1379.70027OpenAlexW2767094345MaRDI QIDQ680974

Ti Chen, Dongping Jin, Pengcheng Wu, Hao Wen

Publication date: 29 January 2018

Published in: AMM. Applied Mathematics and Mechanics. (English Edition) (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10483-017-2278-9

zbMATH Keywords

integrated systemnonlinear model predictive control (NMPC)variable speed control moment gyroscope (VSCMG)

Mathematics Subject Classification ID

Control of mechanical systems (70Q05) Motion of a rigid body with a fixed point (70E17)

Cites Work

• Steering laws analysis of sgcmgs based on singular value decomposition theory
• Passive attitude control of flexible spacecraft from quaternion measurements
• Spacecraft attitude control and stabilization: Applications of geometric control theory to rigid body models
• Controllability of Spacecraft Attitude Using Control Moment Gyroscopes
• Autogenerating microsecond solvers for nonlinear MPC: A tutorial using ACADO integrators

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