Package | Description |
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agi.foundation.propagators |
Contains types used in producing the state of an object from a known element set.
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Modifier and Type | Method and Description |
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static LambertPathType |
LambertPathType.getDefault()
Get the enum constant that is considered to be the default.
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static LambertPathType |
LambertPathType.getFromValue(int value)
Get the enum constant that is associated with the given numeric value.
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LambertPathType |
LambertOrbitSolver.FailedToConvergeEventArgs.getPathType()
Gets the whether or not this path was the small or large semi major axis.
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static LambertPathType |
LambertPathType.valueOf(String name)
Returns the enum constant of this type with the specified name.
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static LambertPathType[] |
LambertPathType.values()
Returns an array containing the constants of this enum type, in
the order they are declared.
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Modifier and Type | Method and Description |
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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.
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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.
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LambertResult |
LambertOrbitSolver.solveMinimumDurationMultipleRevolutionTransfer(Cartesian initialPosition,
Cartesian finalPosition,
int numberOfRevolutions,
LambertPathType pathType,
OrbitDirectionType directionOfFlight)
Solves the constrained Lambert problem given the input.
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LambertResult |
LambertOrbitSolver.solveMinimumDurationMultipleRevolutionTransfer(Cartesian initialPosition,
Cartesian finalPosition,
int numberOfRevolutions,
LambertPathType pathType,
OrbitDirectionType directionOfFlight,
Cartesian orbitalPlaneVector)
Solves the constrained Lambert problem given the input.
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Constructor and Description |
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FailedToConvergeEventArgs(int finalIteration,
double finalEpsilon,
int revolutionCount,
LambertPathType pathType,
OrbitDirectionType directionOfFlight)
Initializes a new instance.
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