The control of in-plane transversal vibrations of a tethered satellite system by means of a longitudinal force exerted by subsatellite thrusts is analyzed. A one-mode model is derived for describing the inplane dynamics of such a system. On the basis of this model, two different nonlinear (and simpl
β¦ LIBER β¦
Nonlinear oscillations of space tethers
β Scribed by E.M. Levin
- Publisher
- Elsevier Science
- Year
- 1994
- Tongue
- English
- Weight
- 193 KB
- Volume
- 32
- Category
- Article
- ISSN
- 0094-5765
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