Optimal two-impulse rendezvous with terminal tangent burn considering the trajectory constraints
Advances in space research ; 54 , 4 ; 734-743
2014
Aufsatz (Zeitschrift)
Unbekannt
| British Library Conference Proceedings | 2014
Reachable domain of spacecraft with a single tangent impulse considering trajectory safety
| Online Contents | 2013
Optimal multiple-impulse orbital rendezvous
| NTRS | 1967
Optimal multiple-impulse orbital rendezvous
| NTRS | 1967