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Rigid-body dynamics from the Euler equations to the attitude control of spacecraft in the works of scientists from St. Petersburg state university. II - MaRDI portal

Rigid-body dynamics from the Euler equations to the attitude control of spacecraft in the works of scientists from St. Petersburg state university. II (Q6638399)

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scientific article; zbMATH DE number 7944446
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English
Rigid-body dynamics from the Euler equations to the attitude control of spacecraft in the works of scientists from St. Petersburg state university. II
scientific article; zbMATH DE number 7944446

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    Rigid-body dynamics from the Euler equations to the attitude control of spacecraft in the works of scientists from St. Petersburg state university. II (English)
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    14 November 2024
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    rigid body
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    spacecraft
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    artificial satellite
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    dynamics
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    rotational motion
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    control
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    stabilization
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    oscillations
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