restricted three-body problem
GPTKB entity
Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:mathematical_concept
|
| gptkbp:appliesTo |
gptkb:Earth-Moon-Satellite_system
gptkb:Sun-Earth-Asteroid_system Jupiter-Sun-Comet system |
| gptkbp:assumes |
the small body has negligible mass
the two larger bodies move in Keplerian orbits |
| gptkbp:describes |
motion of a small body under the gravitational influence of two larger bodies
|
| gptkbp:field |
astrophysics
celestial mechanics dynamical systems |
| gptkbp:first_studied_in |
19th century
|
| gptkbp:has_solution_type |
analytical solutions for special cases
numerical solutions |
| gptkbp:hasSpecialCase |
circular restricted three-body problem
elliptic restricted three-body problem |
| https://www.w3.org/2000/01/rdf-schema#label |
restricted three-body problem
|
| gptkbp:namedFor |
gptkb:Henri_Poincaré
|
| gptkbp:originatedIn |
three-body problem
|
| gptkbp:relatedConcept |
gptkb:Hill_sphere
gptkb:Jacobi_integral gptkb:Poincaré_section zero-velocity surface |
| gptkbp:studies |
gptkb:Lagrange_points
|
| gptkbp:used_in |
space mission trajectory design
study of asteroid orbits study of planetary satellites |
| gptkbp:bfsParent |
gptkb:Astrodynamics
gptkb:Celestial_mechanics |
| gptkbp:bfsLayer |
6
|