Lambert's problem

GPTKB entity

Statements (62)
Predicate Object
gptkbp:instanceOf mathematical problem
gptkbp:appliesTo celestial navigation
gptkbp:canBe transfer orbits
gptkbp:canLeadTo lunar missions
https://www.w3.org/2000/01/rdf-schema#label Lambert's problem
gptkbp:involves two points in space
velocity vectors
gptkbp:isA classical mechanics problem
geometric problem
gptkbp:isActiveIn dynamics courses
mission planning studies
gptkbp:isAttendedBy orbital analysts
gptkbp:isAvenueFor orbital transfers
spacecraft trajectory planning
gptkbp:isConnectedTo gravity assists
Hohmann_transfer_orbits
gptkbp:isCriticizedFor mission design
spacecraft navigation systems
gptkbp:isDiscussedIn transfer times
gptkbp:isExploredIn astrophysics research
orbital mechanics literature
gptkbp:isImportantFor satellite communications
space exploration missions
spacecraft rendezvous
gptkbp:isInformedBy two-body problem
gptkbp:isLocatedIn polar coordinates
Cartesian coordinates
gptkbp:isPartOf celestial mechanics
orbital dynamics
space mission analysis
gptkbp:isRelatedTo gptkb:Kepler's_laws
space exploration
astrodynamics
trajectory optimization
spacecraft propulsion
spacecraft navigation
orbital transfer calculations
spacecraft rendezvous maneuvers
spacecraft trajectory optimization
space_trajectory_analysis
gptkbp:isStudiedIn engineering programs
analytical methods
physics courses
gptkbp:isSurroundedBy iterative methods
gptkbp:isUsedBy launch windows
gptkbp:isUsedFor numerical methods
a set of equations
a conic section
gptkbp:isUsedIn space mission planning
satellite deployment
interplanetary missions
planetary missions
gptkbp:isUtilizedFor interplanetary travel
spacecraft maneuvering
gptkbp:isUtilizedIn spacecraft design
trajectory design
gptkbp:keyIssues interstellar travel
deep space missions
gptkbp:namedAfter gptkb:Johann_Heinrich_Lambert
gptkbp:offersServices finding an orbit
gptkbp:relatedTo orbital mechanics
gptkbp:requires time of flight