Rigid-body dynamics from the Euler equations to the attitude control of spacecraft in the works of scientists from St. Petersburg State University. III (Q6638413)
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scientific article; zbMATH DE number 7944457
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Rigid-body dynamics from the Euler equations to the attitude control of spacecraft in the works of scientists from St. Petersburg State University. III |
scientific article; zbMATH DE number 7944457 |
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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. III (English)
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14 November 2024
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rigid body
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spacecraft
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artificial Earth satellite
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dynamics
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attitude motion
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gravitational stabilization
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oscillation damping
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