Dynamic Behavior of a Tethered System with Multiple Subsatellites in Elliptic Orbits
- 1 November 2001
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 38 (6) , 914-921
- https://doi.org/10.2514/2.3763
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
- Nonlinear Dynamics of the Tethered Subsatellite System in the Station Keeping PhaseJournal of Guidance, Control, and Dynamics, 1997
- Optimal attitude control of a tethered end mass in the Earth's upper atmospherePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1997
- Coupling of tether lateral vibration and subsatellite attitude motionJournal of Guidance, Control, and Dynamics, 1992
- Chaos in the pitch equation of motion for the gravity-gradient satellitePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- Dynamics of a tethered satellite in elliptical, non-equatorial orbitsJournal of Guidance, Control, and Dynamics, 1992
- Dynamics of a tethered satellite subjected to aerodynamic forcesJournal of Guidance, Control, and Dynamics, 1991
- Tethered subsatellite swinging from atmospheric gradientsJournal of Guidance, Control, and Dynamics, 1988
- Dynamics of the orbital cable systemActa Astronautica, 1985
- Periodic solutions associated with the gravity- gradient-oriented system. II - Stability analysis.AIAA Journal, 1969
- Periodic solutions associated with the gravity- gradient-oriented system. I - Analytical and numerical determination.AIAA Journal, 1969