Statements (58)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:academic
|
| gptkbp:alsoKnownAs |
celestial mechanics
|
| gptkbp:appliesTo |
gptkb:Newton's_laws_of_motion
gptkb:law_of_universal_gravitation |
| gptkbp:hasConcept |
gptkb:restricted_three-body_problem
gptkb:Hill_sphere gptkb:Hohmann_transfer gptkb:Jacobi_constant gptkb:Lambert's_problem gptkb:gravity_assist gptkb:Tsiolkovsky_rocket_equation eccentricity resonance semi-major axis orbital decay escape velocity argument of periapsis delta-v mean anomaly orbital elements orbital inclination orbital maneuver orbital period orbital perturbations patched conics right ascension of ascending node sphere of influence station-keeping synodic period transfer orbits true anomaly |
| https://www.w3.org/2000/01/rdf-schema#label |
Astrodynamics
|
| gptkbp:importantFor |
space debris tracking
satellite launches space mission analysis planetary flybys orbital transfers re-entry calculations rendezvous and docking space navigation |
| gptkbp:relatedTo |
gptkb:astronomy
aerospace engineering physics orbital mechanics |
| gptkbp:studies |
motion of artificial bodies in space
|
| gptkbp:usedIn |
interplanetary mission planning
satellite orbit determination spacecraft trajectory design |
| gptkbp:uses |
gptkb:n-body_problem
gptkb:perturbation_theory gptkb:Lagrange_points gptkb:Kepler's_laws numerical integration patched conic approximation two-body problem |
| gptkbp:bfsParent |
gptkb:Titan
gptkb:Lagrange_point |
| gptkbp:bfsLayer |
5
|