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- Lambert's_problem abstract "In celestial mechanics Lambert's problem is concerned with the determination of an orbit from two position vectors and the time of flight. It has important applications in the areas of rendezvous, targeting, guidance, and preliminary orbit determination. Suppose a body under the influence of a central gravitational force is observed to travel from point P1 on its conic trajectory, to a point P2 in a time T. The time of flight is related to other variables by Lambert’s theorem, which states:The transfer time of a body moving between two points on a conic trajectory is a function only of the sum of the distances of the two points from the origin of the force, the linear distance between the points, and the semimajor axis of the conic.Stated another way, Lambert's problem is the boundary value problem for the differential equationof the two-body problem for which the Kepler orbit is the general solution.The precise formulation of Lambert's problem is as follows:Two different times and two position vectors are given.Find the solution satisfying the differential equation above for which".
- Lambert's_problem thumbnail Lambert_Fig1.png?width=300.
- Lambert's_problem wikiPageExternalLink keptoolbox.
- Lambert's_problem wikiPageExternalLink 26348-robust-solver-for-lamberts-orbital-boundary-value-problem.
- Lambert's_problem wikiPageID "20293401".
- Lambert's_problem wikiPageRevisionID "603303263".
- Lambert's_problem hasPhotoCollection Lambert's_problem.
- Lambert's_problem subject Category:Conic_sections.
- Lambert's_problem subject Category:Orbits.
- Lambert's_problem type Line108593262.
- Lambert's_problem type Location100027167.
- Lambert's_problem type Object100002684.
- Lambert's_problem type Orbit108612049.
- Lambert's_problem type Orbits.
- Lambert's_problem type Path108616311.
- Lambert's_problem type PhysicalEntity100001930.
- Lambert's_problem type YagoGeoEntity.
- Lambert's_problem type YagoLegalActorGeo.
- Lambert's_problem type YagoPermanentlyLocatedEntity.
- Lambert's_problem comment "In celestial mechanics Lambert's problem is concerned with the determination of an orbit from two position vectors and the time of flight. It has important applications in the areas of rendezvous, targeting, guidance, and preliminary orbit determination. Suppose a body under the influence of a central gravitational force is observed to travel from point P1 on its conic trajectory, to a point P2 in a time T.".
- Lambert's_problem label "Lambert's problem".
- Lambert's_problem label "Задача Ламберта".
- Lambert's_problem sameAs m.04zzcpv.
- Lambert's_problem sameAs Q6481210.
- Lambert's_problem sameAs Q6481210.
- Lambert's_problem sameAs Lambert's_problem.
- Lambert's_problem wasDerivedFrom Lambert's_problem?oldid=603303263.
- Lambert's_problem depiction Lambert_Fig1.png.
- Lambert's_problem isPrimaryTopicOf Lambert's_problem.
