Optimization of rocket ascent trajectories using an indirect procedure
Guidance, Navigation, and Control Conference ; 1995 ; Baltimore , MD , U.S.A.
1995-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Initial Guess Generation for Rocket Ascent Trajectory Optimization Using Indirect Methods
Online Contents | 2002
|Lunar descent and ascent trajectories
AIAA | 1970
|Study of optimal ascent trajectories
AIAA | 1994
|APOLLO Lunar Descent and Ascent Trajectories
NTIS | 1970
|