Optimal ascent trajectories for delta wing space shuttle flight, using accelerated gradient methods
Near optimal shuttle trajectories using accelerated gradient methods
ASTRODYNAMICS SPECIALISTS CONFERENCE ; 1971 ; FT. LAUDERDALE, FL, US
1971-08-01
Conference paper
No indication
English
Optimal Rocket Trajectories Using Gradient Methods
British Library Conference Proceedings | 2016
|Optimal Trajectories for the Flyback Shuttle
NTIS | 1972
|Constrained optimal ascent-flyback shuttle trajectories.
NTRS | 1972
|Optimal boost trajectories for the shuttle vehicle.
NTRS | 1971
|Optimal Radially Accelerated Interplanetary Trajectories
AIAA | 2006
|