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
Attitude Control of Space Platform Based Tethered Satellite System
โ Scribed by Modi, Vinod J.; Gilardi, Gabriele; Misra, Arun K.
- Book ID
- 121077585
- Publisher
- American Society of Civil Engineers
- Year
- 1998
- Tongue
- English
- Weight
- 730 KB
- Volume
- 11
- Category
- Article
- ISSN
- 0893-1321
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