A method of damping structural vibrations using optimization techniques is presented and applied to a tethered satellite system. Such systems show large displacements and require active or passive damping mechanisms. A tethered satellite system is modelled by the method of multibody systems using sy
β¦ LIBER β¦
Investigation of the spatial vibrations of a controlled satellite
β Scribed by A. I. Makarenko
- Publisher
- Springer US
- Year
- 1973
- Tongue
- English
- Weight
- 353 KB
- Volume
- 9
- Category
- Article
- ISSN
- 1573-8582
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