Package | Description |
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agi.foundation.aircraftpropagation |
Contains types for propagating an aircraft through various maneuvers subject to
flight phase performance models and wind effects.
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Modifier and Type | Method and Description |
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static ManeuverReferenceAxes |
ManeuverReferenceAxes.getDefault()
Get the enum constant that is considered to be the default.
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static ManeuverReferenceAxes |
ManeuverReferenceAxes.getFromValue(int value)
Get the enum constant that is associated with the given numeric value.
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ManeuverReferenceAxes |
VerticalBehaviorDerivatives.getManeuverReferenceAxes()
Gets the axes in which the vertical behavior of a maneuver is defined.
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ManeuverReferenceAxes |
TurnAtConstantRateBehavior.getManeuverReferenceAxes()
Gets the reference axes for the behavior.
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ManeuverReferenceAxes |
MaintainHorizontalAndVerticalSpeedsBehavior.getManeuverReferenceAxes()
Gets the reference axes for the behavior.
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ManeuverReferenceAxes |
MaintainCourseOrHeadingBehavior.getManeuverReferenceAxes()
Gets the reference axes for the behavior.
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ManeuverReferenceAxes |
HorizontalBehaviorDerivatives.getManeuverReferenceAxes()
Gets the axes in which the horizontal behavior of a maneuver is defined.
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ManeuverReferenceAxes |
AircraftReferenceState.getVelocityReferenceAxes()
Gets the reference axes used to define the velocity of the aircraft with respect to either the static or moving local atmosphere.
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static ManeuverReferenceAxes |
ManeuverReferenceAxes.valueOf(String name)
Returns the enum constant of this type with the specified name.
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static ManeuverReferenceAxes[] |
ManeuverReferenceAxes.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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void |
TurnAtConstantRateBehavior.setManeuverReferenceAxes(ManeuverReferenceAxes value)
Sets the reference axes for the behavior.
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void |
MaintainHorizontalAndVerticalSpeedsBehavior.setManeuverReferenceAxes(ManeuverReferenceAxes value)
Sets the reference axes for the behavior.
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void |
MaintainCourseOrHeadingBehavior.setManeuverReferenceAxes(ManeuverReferenceAxes value)
Sets the reference axes for the behavior.
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void |
AircraftReferenceState.setVelocityReferenceAxes(ManeuverReferenceAxes value)
Sets the reference axes used to define the velocity of the aircraft with respect to either the static or moving local atmosphere.
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Constructor and Description |
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HorizontalBehaviorDerivatives(ManeuverReferenceAxes maneuverReferenceAxes,
double angularRate)
Initializes the horizontal derivatives with respect to the indicated maneuver axes.
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MaintainCourseOrHeadingBehavior(ManeuverReferenceAxes maneuverReferenceAxes)
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MaintainHorizontalAndVerticalSpeedsBehavior(ManeuverReferenceAxes maneuverReferenceAxes)
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TurnAtConstantRateBehavior(ManeuverReferenceAxes maneuverReferenceAxes,
double turnRate)
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VerticalBehaviorDerivatives(ManeuverReferenceAxes maneuverReferenceAxes,
double horizontalAcceleration,
double verticalAcceleration)
Initializes the vertical derivatives with respect to the indicated maneuver axes.
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