Gets the total aerodynamic moment vector about the CG in the stability axes. @return a moment vector reference. */

Gets the total aerodynamic moment vector about the CG in the wind axes. @return a moment vector reference. */

Gets the aerodynamic moment about the Moment Reference Center for an axis. @return the moment about a single axis (as described also in the

Retrieves the tip-speed (aka advance) ratio

Retrieves the total local NED velocity in ft/sec. */

The North East Up (NEU) frame is a local tangential frame fixed in the ECEF frame (i.e following the Earth's rotation). The NEU frame's or

Retrieves the name of the function.

Get a random number which probability of occurrence is following Gauss * normal distribution with a mean of 0.0 and a standard deviation of 1.0 *

Retrieves the induced inflow ratio

Returns the number of lines of data stored

Returns the number of child elements for this element.

Retrieves the number of tanks defined for the aircraft.

The longitudinal acceleration in g's of the aircraft center of gravity. */

The lateral acceleration in g's of the aircraft center of gravity. */

The vertical acceleration in g's of the aircraft center of gravity. */

Retrieves the current output filename. @param n index of file @return the name of the output file for the output specified by the flight m

Kinematic component output value. @return the current output of the kinematic object on the range of [0,1]. */

Retrieves a body frame angular velocity component relative to the ECEF frame. Retrieves a body frame angular velocity component. The angular vel

Gets the initial body rotation rate @return Initial body rotation rate in radians/second */

Retrieves a body frame angular velocity component relative to the ECI (inertial) frame. Retrieves a body frame angular velocity component. The a

Gets the initial body axis roll rate. @return Initial body axis roll rate in radians/second */

Returns a pointer to the parent of an element. @return a pointer to the parent Element, or 0 if this is the top level Element. */

Gets the tank fill level. @return the fill level in percent, from 0 to 100.*/

Downwash angle - positive values point leftward (given a horizontal spinning rotor)

Gets the initial roll angle. @return Initial phi in degrees */

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

Gets the pitch trim command. @return pitch trim command in range from -1.0 to 1.0 */

Returns the power required by the rotor.

Prevent C++ from hiding GetPressure(void)

Returns the ratio of at-altitude pressure over the sea level value.

Returns the sea level pressure in target units, default in psf.

Gets the prop pitch position. @param engine engine ID number @return prop pitch position for the given engine in range from 0 - 1.0 */

Gets the prop pitch command. @param engine engine ID number @return pitch command in range from 0.0 - 1.0 for the given engine */

Gets the prop feather position. @param engine engine ID number @return prop fether for the given engine (on / off)*/

Returns a pointer to the property manager object.

Retrieves the value of a property. @param property the name of the property @result the value of the specified property */

Gets the initial heading angle. @return Initial psi in degrees */

Gets Euler angle psi @return phi [rad] */

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

Gets the initial body axis pitch rate. @return Initial body axis pitch rate in radians/second */

Returns the quaternion that goes from Local to Body. */

Returns the quaternion that goes from ECEF to Body. */

Returns the quaternion that goes from ECI to Body. */

Getters for the protected members

Getters for the protected members

Getters for the protected members

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

Retrieves the RPMs of the propeller

Gets the initial body axis yaw rate. @return Initial body axis yaw rate in radians/second */

Get the distance from the center of the earth in feet. @return the distance of the location represented with this class instance to the ce

Get the output rate for the model in frames