Dynamic behaviour of a tethered system with multi-sub-satellites in elliptic orbits
- 3 April 2000
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 9 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. I - Analytical and numerical determination.AIAA Journal, 1969