AGI.Foundation.AircraftPropagation Namespace

Defines an aircraft's performance model during acceleration.

A factory for creating PropagationStateElements representing the position (and velocity) of an aircraft which share the same IntegrationPoint but whose second derivatives are provided by different Maneuvers.

Represents a Point which reflects the integrated motion elements in an integration state.

Defines an initial state of an aircraft in terms of its position and velocity.

Represents output associated with a PropagationStateElement corresponding to a set of Cartesian values. This represents the indexed state, and a means of converting the raw output information back into a Motion<Cartesian>.

Defines a performance model during cruise which changes linearly between altitude bands.

Defines an altitude at which a particular set of cruise commanded values applies.

Defines an aircraft's performance model during climb or descent, by determining a set of ClimbDescentCommandedValues at a given time.

Defines an aircraft's performance model during climb, by determining a set of ClimbDescentCommandedValues at a given time.

Defines an aircraft maneuver as a combination of a horizontal behavior and vertical behavior.

Defines a vertical behavior of a CompositeManeuver in which an aircraft attempts to achieve cruising flight at a desired altitude.

Defines an aircraft's performance model during cruise, by determining a set of CruiseCommandedValues at a given time.

Defines an aircraft's performance model during descent, by determining a set of ClimbDescentCommandedValues at a given time.

Defines the horizontal behavior of a CompositeManeuver.

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.

Defines a horizontal behavior of a CompositeManeuver in which a constant course or heading is maintained. If the ManeuverReferenceAxes is StaticAtmosphere, then the true course of the aircraft is maintained. If the ManeuverReferenceAxes is MovingAtmosphere, then the true heading of the aircraft is maintained.

Defines a vertical behavior of a CompositeManeuver in which the horizontal and vertical speeds are maintained. If the ManeuverReferenceAxes is StaticAtmosphere, then speeds relative to the static atmosphere are maintained. If the ManeuverReferenceAxes is MovingAtmosphere, then speeds relative to the moving atmosphere are maintained.

An abstract base class which defines an aircraft maneuver.

Defines a set of performance models associated with various phases of flight.

Defines a vertical behavior of a CompositeManeuver in which an aircraft's direction of flight is either "pushed over" or "pulled up".

Defines a simple performance model for an aircraft during acceleration.

Defines a simple performance model for an aircraft during climb.

Defines a simple performance model for an aircraft during cruise.

Defines a simple performance model for an aircraft during descent.

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. The thrust force is assumed to be along the longitudinal axis (x-direction in the body axes).

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.

Defines a propulsion model for a jet or turbofan driven fixed wing aircraft under nominal forward flight conditions.

Defines a propulsion model for a propeller driven fixed wing aircraft under nominal forward flight conditions.

Defines a horizontal behavior of a CompositeManeuver in which a constant turn rate is maintained. If the ManeuverReferenceAxes is StaticAtmosphere, then the turn rate applies to the rate of change in the true course of the aircraft. If the ManeuverReferenceAxes is MovingAtmosphere, then the turn rate applies to the rate of change in the true heading of the aircraft.

Defines the vertical behavior of a CompositeManeuver.

Defines the commanded performance values during climb or descent.

Defines the commanded performance values during cruise.

The derivatives which define the horizontal behavior of a maneuver.

The derivatives which define the vertical behavior of a maneuver.

An enumeration indicating one value from a ClimbDescentCommandedValues object.

An enumeration indicating one value from a CruiseCommandedValues object.

Indicates the axes that are to be used for defining the maneuver.