Dynamics of a tethered satellite in elliptical, non-equatorial orbits
- 1 May 1992
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 15 (3) , 621-626
- https://doi.org/10.2514/3.20883
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
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- Tethered subsatellite swinging from atmospheric gradientsJournal of Guidance, Control, and Dynamics, 1988
- Dynamics of the orbital cable systemActa Astronautica, 1985
- Shuttle-tethered subsatellite system stability with a flexible massive tetherJournal of Guidance, Control, and Dynamics, 1985
- Optimal control of the Shuttle-Tethered-Subsatellite systemActa Astronautica, 1980