@name Functions that rely on the ground callback The following functions allow to set and get the vehicle position above the ground. The g

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

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

Gets the control value @return value */

Gets the control maximum value @return control nax value */

Gets the control minimum value @return control min value */

Gets the control name @return control name */

inline State GetStateType(void) { return state; } Return the control type @return TaControl */

Retrieves the cosine of a vehicle Euler angle component. Retrieves the cosine of an Euler angle (Phi, Theta, or Psi) from the quaternion t

Retrieves cosine of the given euler angle. @return the sine of the Euler angle theta (pitch attitude) corresponding to this quaternion rot

Get the cosine of Longitude. */

Retrieves the coefficient of power multiplier

Retrieves propeller power Mach effects factor

Retrieves the coefficient of thrust multiplier

Retrieves propeller thrust Mach effects factor

@name Pilot input command retrieval @{ Gets the aileron command. @return aileron command in range from -1.0 - 1.0 */

@name Aerosurface position retrieval @{ Gets the left aileron position. @return aileron position in radians */

Gets the right aileron position. @return aileron position in radians */

Gets the elevator command. @return elevator command in range from -1.0 - 1.0 */

Gets the elevator position. @return elevator position in radians */

Retrieves the current debug level setting. */

Returns the simulation delta T.

Prevent C++ from hiding GetDensity(void)

Returns the fuel density. @return the density in lbs/gal. */

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

Returns the sea level density in slugs/ft^3

Gets the flaps command. @return flaps command in range from 0 to 1.0 */

Gets the flaps position. @return flaps position in radians */

Retrieves the propeller diameter

Gets the rudder command. @return rudder command in range from -1.0 - 1.0 */

Gets the rudder position. @return rudder position in radians */

Gets the speedbrake command. @return speedbrake command in range from 0 to 1.0 */

Gets the speedbrake position. @return speedbrake position in radians */

Gets the spoiler command. @return spoiler command in range from 0 to 1.0 */

Gets the spoiler position. @return spoiler position in radians */

Returns the Earth position angle. @return Earth position angle in radians. */

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

Calculates the RPMs of the engine based on gear ratio

Retrieves a vehicle Euler angle component. Retrieves an Euler angle (Phi, Theta, or Psi) from the quaternion that stores the vehicle orien

Retrieves the Euler angles. @param i the Euler angle index. units radians. @return a reference to the i-th euler angles correspondin

Retrieves a vehicle Euler angle component in degrees. Retrieves an Euler angle (Phi, Theta, or Psi) from the quaternion that stores the ve

Retrieves the Euler angles. @param i the Euler angle index. @return a reference to the i-th euler angles corresponding to this quate

Gets the number of child FDMs.

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

Gets the flame-out status. The engine will "flame out" if the throttle is set below the minimum sustainable-thrust setting. @return

Gets the initial flight path angle. @return Initial flight path angle in degrees */

Gets the aerodynamic force for an axis. @param n Axis index. This could be 0, 1, or 2, or one of the axis enums: eX, eY, eZ.

Retrieves the total forces applied on the body. Retrieves the total forces applied on the body. This does include the friction forces but

Retrieves the aerodynamic forces in the stability axes, given an axis. @param axis the axis to return the force for (eX, eY, eZ). @return a refere

Retrieves the current frame count. */