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
Control of the vibrations of a tethered satellite system
โ Scribed by F. Dignath; W. Schiehlen
- Publisher
- Elsevier Science
- Year
- 2000
- Tongue
- English
- Weight
- 613 KB
- Volume
- 64
- Category
- Article
- ISSN
- 0021-8928
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โฆ Synopsis
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 symbolic equations of motion. Active damping is provided by an actuator between the main body and the tether. The control parameters are optimized. The energy decay of the system is used as the performance criterion. The complex dynamics of the motion of this system are demonstrated in simulations with different initial conditions including structural vibrations. It is shown that an optimization process enables the control parameters be improved with respect to the dissipation of energy of longitudinal structural vibrations.
๐ SIMILAR VOLUMES
## of a Tethered satellites can be lowered to altitudes where unusually strong atmospheric perturbations occur. A command-adaptive model follower substantially improves three-dimension tension-only control compared to an existing concept using constant commands.