Relative Motion of Particles in Coplanar Elliptic Orbits
- 1 September 1979
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance and Control
- Vol. 2 (5) , 443-446
- https://doi.org/10.2514/3.55906
Abstract
No abstract availableKeywords
This publication has 9 references indexed in Scilit:
- An exact and a new first-order solution for the relative trajectories of a probe ejected from a space stationCelestial Mechanics and Dynamical Astronomy, 1976
- Relative motion of near orbiting satellitesCelestial Mechanics and Dynamical Astronomy, 1973
- Relative motion of two particles in elliptic orbitsAIAA Journal, 1970
- Second-order solution to the elliptical rendezvous problem.AIAA Journal, 1967
- Rendezvous Problem for Nearly Circular OrbitsAIAA Journal, 1965
- ELLIPTIC ELEMENTS IN TERMS OF SMALL INCREMENTS OF POSITION AND VELOCITY COMPONENTSAIAA Journal, 1963
- SECOND APPROXIMATION TO THE SOLUTION OF THE RENDEZVOUS EQUATIONSAIAA Journal, 1963
- RELATIVE TRAJECTORIES OF OBJECTS EJECTED FROM A NEAR SATELLITEAIAA Journal, 1963
- Terminal Guidance System for Satellite RendezvousJournal of the Aerospace Sciences, 1960