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.
AMERICAN ASTRONAUTICAL SOCIETY AND AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, ASTRODYNAMICS SPECIALIST CONFERENCE ; 1968 ; JACKSON, WYO.
1969-06-01
Miscellaneous
No indication
English
Trajectory optimization using regularized variables.
NTRS | 1968
|Trajectory optimization using regularized variables.
AIAA | 1969
|