<?xml version="1.0"?>

  <!--
	This file sets up the aircraft initial conditions.

	Allowable units are:
		Length:			M IN FT
		Angles:			DEG RAD
		Velocity:		M/S FT/SEC KTS
		Area:			M2 FT2
		Volume:			CC LTR M3 IN3 FT3
		Mass/Weight:		KG LBS
		Moments of Inertia: KG*M2 SLUG*FT2
		Torque:			N*M FT*LBS
		Force:			N LBS
		Spring Force:	N/M LBS/FT
		Damping Force:	N/M/SEC LBS/FT/SEC
		Power:			WATTS HP
		Pressure:		PA ATM PSI PSF INHG

	Some example initial conditions are given below. Not all are needed.

	Note that the launch condition body aligned forward velocity is given in sim_ac_fw.c
	and can be defined in the SIMU section of the airframe file. See jsbsim.xml for example.

	Other ICs are allowable, see JSBSim source for more info:
		FGInitialCondition::Load	()
		FGInitialCondition::Load_v1()
		FGInitialCondition::Load_v2()

  -->

<initialize name="beforelaunch">
<!-- Location -->
  <latitude 		unit="DEG">		43.46223	</latitude> <!-- Muret, FR -->
  <longitude 	unit="DEG"> 		1.27289 	</longitude> <!-- Muret, FR -->
  <elevation		unit="M"	>		186.0		</elevation> <!-- terrain elevation -->
  <altitudeAGL	unit="M"> 		2.0 		</altitudeAGL> <!-- altitude above ground level -->
<!-- Orientation -->
  <psi 			unit="DEG">		0.0 		</psi> <!-- heading (yaw) -->
  <theta 		unit="DEG">		0.0 		</theta> <!-- pitch -->
  <phi 			unit="DEG">		0.0 		</phi> <!-- roll -->
<!-- Wind -->
  <winddir 		unit="DEG">		0.0 		</winddir> <!-- positive velocity direction (0.0 is wind from south) -->
  <vwind 		unit="KTS">		20.0 		</vwind>
<!--Do not modify-->
  <vground		unit="KTS">		0.0		</vground> <!-- ground speed -->
  <running>						-1		</running> <!-- set all engines running -->
</initialize>
