Trajectory optimization of space vehicle with continuous thrust based on regularized equations, comparing perturbation method for earth-Jupiter rendezvous transfer
Trajectory optimization using regularized variables.
ASTRODYNAMICS SPECIALIST CONFERENCE ; 1968 ; JACKSON, WY, US
01.09.1968
Aufsatz (Konferenz)
Keine Angabe
Englisch
Trajectory optimization using regularized variables.
NTRS | 1969
|Trajectory optimization using regularized variables.
AIAA | 1969
|