Uses of Class
agi.foundation.propagators.LambertResult

Packages that use LambertResult

Package	Description
agi.foundation.propagators	Contains types used in producing the state of an object from a known element set.

Uses of LambertResult in agi.foundation.propagators

Methods in agi.foundation.propagators that return LambertResult

Modifier and Type	Method and Description
LambertResult	LambertOrbitSolver.solveFixedDurationTransfer(Cartesian initialPosition, Cartesian finalPosition, Duration timeOfFlight, int numberOfRevolutions, LambertPathType pathType, OrbitDirectionType directionOfFlight) Solves the classic Lambert problem with the specified number of revolutions.
LambertResult	LambertOrbitSolver.solveFixedDurationTransfer(Cartesian initialPosition, Cartesian finalPosition, Duration timeOfFlight, int numberOfRevolutions, LambertPathType pathType, OrbitDirectionType directionOfFlight, Cartesian orbitalPlaneVector) Solves the classic Lambert problem with the specified number of revolutions.
LambertResult	LambertOrbitSolver.solveMinimumDurationMultipleRevolutionTransfer(Cartesian initialPosition, Cartesian finalPosition, int numberOfRevolutions, LambertPathType pathType, OrbitDirectionType directionOfFlight) Solves the constrained Lambert problem given the input.
LambertResult	LambertOrbitSolver.solveMinimumDurationMultipleRevolutionTransfer(Cartesian initialPosition, Cartesian finalPosition, int numberOfRevolutions, LambertPathType pathType, OrbitDirectionType directionOfFlight, Cartesian orbitalPlaneVector) Solves the constrained Lambert problem given the input.
LambertResult	LambertOrbitSolver.solveMinimumEccentricityTransfer(Cartesian initialPosition, Cartesian finalPosition) Solves the constrained Lambert problem given the input.
LambertResult	LambertOrbitSolver.solveMinimumEccentricityTransfer(Cartesian initialPosition, Cartesian finalPosition, Cartesian orbitalPlaneVector) Solves the constrained Lambert problem given the input.
LambertResult	LambertOrbitSolver.solveMinimumEnergyTransfer(Cartesian initialPosition, Cartesian finalPosition) Solves the constrained Lambert problem given the input.
LambertResult	LambertOrbitSolver.solveMinimumEnergyTransfer(Cartesian initialPosition, Cartesian finalPosition, Cartesian orbitalPlaneVector) Solves the constrained Lambert problem given the input.
LambertResult	LambertOrbitSolver.solveParabolicTransfer(Cartesian initialPosition, Cartesian finalPosition, OrbitDirectionType directionOfFlight) Solves the constrained Lambert problem given the input.
LambertResult	LambertOrbitSolver.solveParabolicTransfer(Cartesian initialPosition, Cartesian finalPosition, OrbitDirectionType directionOfFlight, Cartesian orbitalPlaneVector) Solves the constrained Lambert problem given the input.