Uses of Package
agi.foundation.aircraftpropagation

Packages that use agi.foundation.aircraftpropagation

Package	Description
agi.foundation.aircraftpropagation	Contains types for propagating an aircraft through various maneuvers subject to flight phase performance models and wind effects.

Classes in agi.foundation.aircraftpropagation used by agi.foundation.aircraftpropagation

Class and Description
AccelerationPerformanceModel Defines an aircraft's performance model during acceleration.
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.
ClimbDescentCommandedValuesElement An enumeration indicating one value from a ClimbDescentCommandedValues object.
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.
CruiseCommandedValues Defines the commanded performance values during cruise.
CruiseCommandedValuesElement An enumeration indicating one value from a CruiseCommandedValues object.
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.
Maneuver An abstract base class which defines an aircraft maneuver.
ManeuverReferenceAxes Indicates the axes that are to be used for defining the maneuver.
PerformanceModels Defines a set of performance models associated with various phases of flight.
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.
VerticalBehavior Defines the vertical behavior of a CompositeManeuver.
VerticalBehaviorDerivatives The derivatives which define the vertical behavior of a maneuver.