Magnetic attitude control system for low-Earth orbit satellites (Q5944976)

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scientific article; zbMATH DE number 1655763
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English
Magnetic attitude control system for low-Earth orbit satellites
scientific article; zbMATH DE number 1655763

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    Magnetic attitude control system for low-Earth orbit satellites (English)
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    7 October 2002
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    The stabilization of a small spacecraft on the low-Earth orbit is done by a three-axis magnetometer. Both orbital motion parameters and attitude can be estimated by the vector function Lyapunov method. The authors also propose a recursive state estimation algorithm with enhanced convergence.
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    magnetic attitude control
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    stabilization of spacecraft
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    low-Earth orbit
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    three-axis magnetometer
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    vector function Lyapunov method
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    recursive state estimation algorithm
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    enhanced convergence
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