Optionally provides source filename and line for contextual diagnostics.

* @return \e f the flattening of the ellipsoid. This is the value * inherited from the Geodesic object used in the constructor. *********

* @return \e f the flattening of the ellipsoid. This is the * value used in the constructor. *******************************************

Ignore text formatting.

Forces the specified output object to print its items once */

Applies a formatting hint to subsequent output.

* A default constructor. If GeodesicLine::Position is called on the * resulting object, it returns immediately (without doing any * calcula

* Constructor * * @param[in] msg a string message, which is accessible in the catch * clause via what(). ***********************

Retrieves the rotor's coning angle

Retrieves the longitudinal flapping angle with respect to the rotor shaft

Compute the altitude above ground. */

@name Viscosity access functions. @{ Returns the absolute viscosity.

Gets the initial angle of attack. @return Initial alpha in degrees */

Gets the initial angle of attack. @return Initial alpha in radians */

Get the altitude above sea level dependent on the location. */

Get the altitude above ground level. @return the altitude AGL in feet. @param location Location at which the AGL is evaluated. @see

Returns the current altitude above sea level. This function returns the altitude above sea level. units meters @return The current a

Retrieves the lateral flapping angle with respect to the rotor shaft

Gets the initial sideslip angle. @return Initial beta in degrees */

Gets the initial angle of sideslip. @return Initial sideslip angle in radians */

Gets the location of the gear in Body axes

Gets the center brake. @return the center brake setting. */

Retrieves propeller power table

Retrieves the thrust coefficient

Retrieves propeller thrust table

Gets the capacity of the tank. @return the capacity of the tank in pounds. */

Gets the capacity of the tank. @return the capacity of the tank in gallons. */

Gets a particular child FDM.

Retrieves the square of the lift coefficient. */

Gets the initial climb rate. @return Initial climb rate in feet/minute */

Retrieves the collective control input in radians.

Gets the gear compression force in pounds

Gets the current compressed length of the gear in feet

Gets the current gear compression velocity in ft/sec

Returns a non-zero value if the propeller is constant speed.