Two types of satellite rendezvous trajectories were discussed: direct ascent from burnout and transfer from a parking orbit coplanar with the target orbit. Equations for the orbital elements and velocity requirements of the trajectories were presented, and numerical solutions were obtained for selected trajectories. (Author)
Satellite Rendezvous Trajectories
1962
2 pages
Report
No indication
English
Ion Drive multi-asteroid rendezvous trajectories
NTRS | 1977
|Control of omni-directional rendezvous trajectories
Online Contents | 1994
|Control of omni-directional rendezvous trajectories
Elsevier | 1993
|