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
1968-09-01
Conference paper
No indication
English
Trajectory optimization using regularized variables.
NTRS | 1969
|Trajectory optimization using regularized variables.
AIAA | 1969
|