A direct optimization method intended to be used primarily for preliminary design of low-thrust interplanetary trajectories, including those with multiple gravity assists, is presented.
Preliminary Design of Low-Thrust Interplanetary Missions
16.08.1999
Sonstige
Keine Angabe
Englisch
Preliminary Design of Low-Thrust Interplanetary Missions
NTRS | 1997
|Preliminary Design of Low-Thrust Interplanetary Missions
NTRS | 1999
|Preliminary Design of Low-Thrust Interplanetary Missions
NTIS | 1997
|Preliminary Design of Low-Thrust Interplanetary Missions (AAS 99-338)
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