Stability Analysis of Planetary Satellite Orbiters: Application to the Europa Orbiter
- 1 July 2001
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 24 (4), 778-787
- https://doi.org/10.2514/2.4778
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- The Restricted Hill Four-Body Problem with Applications to the Earth–Moon–Sun SystemCelestial Mechanics and Dynamical Astronomy, 1998
- Dynamics of Distant Moons of AsteroidsIcarus, 1997
- Dynamics of binary asteroids: I. Hill's caseIcarus, 1990
- Methods of Celestial MechanicsPublished by Elsevier BV ,1961