The trajectories of a spaceprobe ejected from a space station in circular orbit
- 1 November 1979
- journal article
- Published by Springer Nature in Celestial Mechanics and Dynamical Astronomy
- Vol. 20 (4) , 405-431
- https://doi.org/10.1007/bf01230406
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
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- 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
- RELATIVE TRAJECTORIES OF OBJECTS EJECTED FROM A NEAR SATELLITEAIAA Journal, 1963