1.
Bulletin of the National Research Centre. 2004; 29 (5): 547-563
em Inglês
| IMEMR
| ID: emr-65591
RESUMO
We have derived Euler-Lambert equation for the hyperbolic orbital motion. It is a new derivation and a first time publication for this problem which is relevant to interplanetary rendezvous trajectories encountered in dynamics of space science. Some new additions to elliptic and parabolic trajectories are cited