Computer algorithm to determine minimum-time optimal control for continuous low-thrust propulsion systems operating in inverse-square gravity field
Low-thrust guidance study Final report
1966-07-01
Report
No indication
English
Low-Thrust Guidance Study Final Report
NTIS | 1966
|Tape guidance study Final report
NTRS | 1966
|Tape Guidance Study Final Report
NTIS | 1966
|Voyager Terminal Guidance Study Final Report
NTIS | 1968
|Optimum Rendezvous Guidance Study Final Report
NTIS | 1969
|