Get the console touchdown reporting feature @return true if reporting is turned on */

Returns true if the propeller is in reverse position.

Retrieves the reverse pitch command.

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

Retrieves the script object

If the tank is set to supply fuel, this function returns true. @return true if this tank is set to a non-zero priority.*/

Returns the cumulative simulation time in seconds.

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

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

Get the sine of Longitude. */

Prevent C++ from hiding GetSoundSpeed(void)

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

Returns the sea level speed of sound in ft/sec.

Gets the initial speedset. @return Initial speedset */

Get target state value for trim @return state target */

Returns the ratio of the standard temperature at the supplied altitude over the standard sea level temperature.

Returns the standard sea level temperature in degrees Rankine. @return The STANDARD temperature at sea level in degrees Rankine.

Gets the tailhook position (0 up, 1 down) @return tailhook position (0 up, 1 down) */

Retrieves a tank object pointer from the list of tanks. @param index the tank index within the vector container @return the address of the

Gets the target normal load factor set from IC. @return target normal load factor set from IC*/

Transform matrix from the earth centered to local horizontal frame. The local frame is the NED (North-East-Down) frame. Since the Down dir

Gets the temperature of the fuel. The temperature of the fuel is calculated if an initial tempearture is given in the configuration file.

Returns the temperature bias over the sea level value in degrees Rankine.

Returns the temperature gradient to be applied on top of the standard temperature gradient.

Returns the ratio of the at-current-altitude temperature as modeled over the sea level value.

Returns the actual, modeled sea level temperature in degrees Rankine. @return The modeled temperature in degrees Rankine at sea level.

Gets the temperature of the fuel. The temperature of the fuel is calculated if an initial tempearture is given in the configuration file.

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

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

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

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

Retrieves the thrust of the rotor.

Retrieves the thrust coefficient

Returns the thrust variation, if any. */

Get control tolerance @return value of control tolerance */

Get the tolerance for declaring a state trimmed. @return tolerance. */

Retrieves the Torque in foot-pounds (Don't you love the English system?)

Gets the total impulse of the rocket. @return The cumulative actual total impulse of the rocket up to this time.*/

Returns the Total Isp variation, if any. */

Returns the total pressure. Total pressure is freestream total pressure for subsonic only. For supersonic it is the 1D total pressure

Gets trim result status @return trim_failed (boolean) */

Retrieves a turbulence component in NED frame.

Retrieves the type of tank: Fuel or Oxidizer. @return the tank type, 0 for undefined, 1 for fuel, and 2 for oxidizer. */

Gets the initial body axis X velocity. @return Initial body axis X velocity in feet/second. */

Gets the initial body velocity @return Initial body velocity in feet/second. */

Get a random number which probability of occurrence is uniformly * distributed over the segment [-1;1( */

Returns the unusable volume of fuel in the tank. @return the volume in gal. */

Gets the initial body axis Y velocity. @return Initial body axis Y velocity in feet/second. */

Gets the initial local frame Z (Down) velocity. @return Initial local frame Z (Down) axis velocity in feet/second. */

Gets the initial local frame Y (East) velocity. @return Initial local frame Y (East) axis velocity in feet/second. */