Uses of Class
agi.foundation.coordinates.OrbitDirectionType

Packages that use OrbitDirectionType

Package	Description
agi.foundation.coordinates	Contains types for quantifying and converting between various coordinate representations.
agi.foundation.propagators	Contains types used in producing the state of an object from a known element set.

Uses of OrbitDirectionType in agi.foundation.coordinates

Methods in agi.foundation.coordinates that return OrbitDirectionType

Modifier and Type	Method and Description
static OrbitDirectionType	OrbitDirectionType.getDefault() Get the enum constant that is considered to be the default.
static OrbitDirectionType	OrbitDirectionType.getFromValue(int value) Get the enum constant that is associated with the given numeric value.
static OrbitDirectionType	OrbitDirectionType.valueOf(String name) Returns the enum constant of this type with the specified name.
static OrbitDirectionType[]	OrbitDirectionType.values() Returns an array containing the constants of this enum type, in the order they are declared.

Uses of OrbitDirectionType in agi.foundation.propagators

Methods in agi.foundation.propagators that return OrbitDirectionType

Modifier and Type	Method and Description
OrbitDirectionType	LambertOrbitSolver.FailedToConvergeEventArgs.getDirectionOfFlight() Gets the rotation sense of the Lambert path.

Methods in agi.foundation.propagators with parameters of type OrbitDirectionType

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.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.

Constructors in agi.foundation.propagators with parameters of type OrbitDirectionType

Constructor and Description
FailedToConvergeEventArgs(int finalIteration, double finalEpsilon, int revolutionCount, LambertPathType pathType, OrbitDirectionType directionOfFlight) Initializes a new instance.