Controllability of Spacecraft Attitude Using Control Moment Gyroscopes
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Publication:4974492
DOI10.1109/TAC.2008.2008324zbMath1367.70052OpenAlexW2160216531MaRDI QIDQ4974492
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Publication date: 8 August 2017
Published in: IEEE Transactions on Automatic Control (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1109/tac.2008.2008324
Controllability (93B05) Control of mechanical systems (70Q05) Orbital mechanics (70M20) Attainable sets, reachability (93B03) Control/observation systems governed by ordinary differential equations (93C15)
Related Items (7)
Controllability of an underactuated spacecraft with one thruster under disturbance ⋮ Small-time local controllability of spacecraft attitude using control moment gyros ⋮ Complex-coefficient frequency domain stability analysis method for a class of cross-coupled antisymmetrical systems and its extension in MSR systems ⋮ On the attitude stabilization of a rigid spacecraft using two skew control moment gyros ⋮ Model predictive control of rigid spacecraft with two variable speed control moment gyroscopes ⋮ Dynamics modeling and attitude stabilization control of a multiarmed space robot for on-orbit servicing ⋮ Attitude control of a rigid spacecraft with one variable-speed control moment gyro
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