Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
orbital mechanics problem
|
| gptkbp:application |
space mission design
interplanetary trajectory planning |
| gptkbp:describes |
determining an orbit connecting two points in space in a given time
|
| gptkbp:field |
gptkb:astrodynamics
celestial mechanics |
| gptkbp:formedBy |
18th century
|
| https://www.w3.org/2000/01/rdf-schema#label |
Lambert's problem
|
| gptkbp:namedAfter |
gptkb:Johann_Heinrich_Lambert
|
| gptkbp:relatedTo |
gptkb:Kepler's_laws
two-body problem |
| gptkbp:solvedBy |
gptkb:Lambert's_theorem
numerical methods |
| gptkbp:usedIn |
orbital transfer
spacecraft rendezvous |
| gptkbp:bfsParent |
gptkb:Astrodynamics
gptkb:Lambert gptkb:Johann_Heinrich_Lambert |
| gptkbp:bfsLayer |
6
|