NASA/CR-2006-214432, Levin, E.M. and Pearson, J. and Oldson, J.C., Dynamics Simulation Model for Space Tethers, George C. Marshall Space Flight Center, Marshall Space Flight Center, Alabama 35812, June, 2006, pp. 66, Format(s): PDF 9034k |
This document describes the development of an accurate model for the dynamics of the Momentum Exchange Electrodynamic Reboost (MXER) system. The MXER is a rotating tether about 100-km long in elliptical Earth orbit designed to catch payloads low Earth orbit and throw them to geosynchronous orbit or to Earth escape. To ensure successful rendezvous between the MXER tip catcher and a payload, a high-fidelity model of the system dynamics is required. The model developed here quantifies the major environmental perturbations, and can predict the MXER tip position to within meters over one orbit.
| Keywords: | space tethers, dynamics, estimation, control, orbit propagation, perturbations, drag, outgassing, thermal effects |
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| Subjects: | Astronautics: Astrodynamics |
| ID Code: | 725 |
| Deposited On: | 18 October 2006 |