Q-Law Aided Direct Trajectory Optimization for the High-Fidelity, Many-Revolution Low-Thrust Orbit Transfer Problem
AAS/AIAA Space Flight Mechanics Meeting ; 29. ; 2019 ; Kaanapali, Hawaii
2019
Aufsatz (Konferenz)
Englisch
Minimum-Time Trajectory Optimization of Multiple Revolution Low-Thrust Earth-Orbit Transfers
Online Contents | 2015
|Optimal many-revolution orbit transfer
AIAA | 1985
|