Study program written in FORTRAN 4 developes an oribital rendezvous guidance scheme for large, constant thrust launch vehicles. It concentrates on /1/ an investigation of the direct extension of the present Saturn Iterative Guidance Mode /IGM/ scheme and /2/ a scheme formulated in a reference frame moving with the target satellite.
Earth orbit rendezvous evaluation program
1967-11-01
Miscellaneous
No indication
English
Rendezvous mission to an earth orbit crossing asteroid
AIAA | 1992
|Low Earth Orbit Rendezvous Strategy for Lunar Missions
NTRS | 2006
|Near Earth Asteroid Rendezvous Orbit Phase Trajectory Design
British Library Conference Proceedings | 1998
|AIAA | 1967
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