Orbital dynamics of the hanging tether interferometer
Abstract
An examination is conducted of the consequences of Coriolis forces, analyzing a strategy for the cancellation of the Coriolis forces by means of ion thrusters. The thrust levels thus employed are found to be easily achievable by existing technology, for the case of a 10-km baseline interferometer that operated in GEO. The major remaining question regarding the scheme's practicality involves vibrations induced in the tether by the central station of its configuration.
- Publication:
-
Journal of Guidance Control Dynamics
- Pub Date:
- December 1991
- DOI:
- 10.2514/3.20788
- Bibcode:
- 1991JGCD...14.1309D
- Keywords:
-
- Coriolis Effect;
- Orbital Mechanics;
- Satellite Control;
- Tethered Satellites;
- Computerized Simulation;
- Gravity Gradient Satellites;
- Interferometers;
- Ion Propulsion;
- Synchronous Satellites;
- Tetherlines;
- Astrodynamics