Package agi.foundation.aircraftpropagation

Contains types for propagating an aircraft through various maneuvers subject to flight phase performance models and wind effects.

See: Description

Class Summary

Class	Description
AccelerationPerformanceModel	Defines an aircraft's performance model during acceleration.
AircraftMotionElement	A factory for creating PropagationStateElements representing the position (and velocity) of an aircraft which share the same IntegrationPoint (get) but whose second derivatives are provided by different Maneuvers.
AircraftMotionIntegrationPoint	Represents a Point which reflects the integrated motion elements in an integration state.
AircraftReferenceState	Defines an initial state of an aircraft in terms of its position and velocity.
AircraftStateElementConverter	Represents output associated with a PropagationStateElement corresponding to a set of Cartesian values.
BandedCruisePerformanceModel	Defines a performance model during cruise which changes linearly between altitude bands.
BandedCruisePerformanceModel.Band	Defines an altitude at which a particular set of cruise commanded values applies.
ClimbDescentCommandedValues	Defines the commanded performance values during climb or descent.
ClimbDescentPerformanceModel	Defines an aircraft's performance model during climb or descent, by determining a set of ClimbDescentCommandedValues at a given time.
ClimbPerformanceModel	Defines an aircraft's performance model during climb, by determining a set of ClimbDescentCommandedValues at a given time.
CompositeManeuver	Defines an aircraft maneuver as a combination of a horizontal behavior and vertical behavior.
CruiseBehavior	Defines a vertical behavior of a CompositeManeuver in which an aircraft attempts to achieve cruising flight at a desired altitude.
CruiseCommandedValues	Defines the commanded performance values during cruise.
CruisePerformanceModel	Defines an aircraft's performance model during cruise, by determining a set of CruiseCommandedValues at a given time.
DescentPerformanceModel	Defines an aircraft's performance model during descent, by determining a set of ClimbDescentCommandedValues at a given time.
HorizontalBehavior	Defines the horizontal behavior of a CompositeManeuver.
HorizontalBehaviorDerivatives	The derivatives which define the horizontal behavior of a maneuver.
LinearClimbOrDescentBehavior	Defines a vertical behavior of a CompositeManeuver in which an aircraft accelerates or decelerates longitudinally, linearly increasing or decreasing its true airspeed and rate of climb or descent.
MaintainCourseOrHeadingBehavior	Defines a horizontal behavior of a CompositeManeuver in which a constant course or heading is maintained.
MaintainHorizontalAndVerticalSpeedsBehavior	Defines a vertical behavior of a CompositeManeuver in which the horizontal and vertical speeds are maintained.
Maneuver	An abstract base class which defines an aircraft maneuver.
PerformanceModels	Defines a set of performance models associated with various phases of flight.
PushOverOrPullUpBehavior	Defines a vertical behavior of a CompositeManeuver in which an aircraft's direction of flight is either "pushed over" or "pulled up".
SimpleAccelerationPerformanceModel	Defines a simple performance model for an aircraft during acceleration.
SimpleClimbPerformanceModel	Defines a simple performance model for an aircraft during climb.
SimpleCruisePerformanceModel	Defines a simple performance model for an aircraft during cruise.
SimpleDescentPerformanceModel	Defines a simple performance model for an aircraft during descent.
SimpleFixedWingCoordinatedFlight	Defines a flight condition where the aircraft is assumed to be flying with the following conditions: The forces acting in the lateral direction are zero.
SimpleFixedWingForwardFlightAerodynamics	Defines an aerodynamic model for fixed wing aircraft under nominal forward flight conditions which accounts for lift and drag forces but assumes that the slip (or side) force is zero, by definition.
SimpleForwardFlightJetPropulsion	Defines a propulsion model for a jet or turbofan driven fixed wing aircraft under nominal forward flight conditions.
SimpleForwardFlightPropellerPropulsion	Defines a propulsion model for a propeller driven fixed wing aircraft under nominal forward flight conditions.
TurnAtConstantRateBehavior	Defines a horizontal behavior of a CompositeManeuver in which a constant turn rate is maintained.
VerticalBehavior	Defines the vertical behavior of a CompositeManeuver.
VerticalBehaviorDerivatives	The derivatives which define the vertical behavior of a maneuver.

Enum Summary

Enum	Description
ClimbDescentCommandedValuesElement	An enumeration indicating one value from a ClimbDescentCommandedValues object.
CruiseCommandedValuesElement	An enumeration indicating one value from a CruiseCommandedValues object.
ManeuverReferenceAxes	Indicates the axes that are to be used for defining the maneuver.

Package agi.foundation.aircraftpropagation Description

Contains types for propagating an aircraft through various maneuvers subject to flight phase performance models and wind effects.