Spacecraft optimum low thrust trajectory analyzed by Hamilton-Jacobi perturbation theory, obtaining canonic constants of motion
The Hamilton-Jacobi method applied to the low-thrust trajectory problem.
INTERNATIONAL ASTRONAUTICAL FEDERATION, INTERNATIONAL ASTRONAUTICAL CONGRESS ; 1967 ; BELGRADE, YUGOSLAVIA
1968-01-01
Conference paper
No indication
English
AIAA | 1998
|British Library Online Contents | 2002
|Hamilton-Jacobi Perturbation Theory
AIAA | 1998
|