<?xml version="1.0"?>
<initialize name="reset01">
  <vbody unit="FT/SEC">    0.0  </vbody>
  <wbody unit="FT/SEC">    0.0  </wbody>

  <altitude unit="FT">35000.0  </altitude>
  <vt unit="KTS">238</vt>

  <latitude unit="DEG">   54.0  </latitude>
  <longitude unit="DEG">   1.0  </longitude>
  <phi unit="DEG">         0.0  </phi>
<!--
  <mach>0.5</mach>
<theta unit="DEG">      10.0  </theta> 
<vt unit="KTS">250</vt>

alpha -8.5478
eleve -11.422 deg
mach 0.5632
alt 35509
mass 50777

Time	Aileron Command (norm)	Elevator Command (norm)	Rudder Command (norm)	Flap Command (norm)	Left Aileron Position (deg)	Right Aileron Position (deg)	Elevator Position (deg)	Rudder Position (deg)	Flap Position (deg)	P (deg/s)	Q (deg/s)	R (deg/s)	P dot (deg/s^2)	Q dot (deg/s^2)	R dot (deg/s^2)	P_{inertial} (deg/s)	Q_{inertial} (deg/s)	R_{inertial} (deg/s)	q bar (psf)	Reynolds Number	V_{Total} (ft/s)	V_{Inertial} (ft/s)	UBody	VBody	WBody	UdotBody	VdotBody	WdotBody	UdotBody_i	VdotBody_i	WdotBody_i	BodyAccel_X	BodyAccel_Y	BodyAccel_Z	Aero V_{X Body} (ft/s)	Aero V_{Y Body} (ft/s)	Aero V_{Z Body} (ft/s)	V_{X_{inertial}} (ft/s)	V_{Y_{inertial}} (ft/s)	V_{Z_{inertial}} (ft/s)	V_{X_{ecef}} (ft/s)	V_{Y_{ecef}} (ft/s)	V_{Z_{ecef}} (ft/s)	V_{North} (ft/s)	V_{East} (ft/s)	V_{Down} (ft/s)	F_{Drag} (lbs)	F_{Side} (lbs)	F_{Lift} (lbs)	L/D	F_{Aero x} (lbs)	F_{Aero y} (lbs)	F_{Aero z} (lbs)	F_{Prop x} (lbs)	F_{Prop y} (lbs)	F_{Prop z} (lbs)	F_{Gear x} (lbs)	F_{Gear y} (lbs)	F_{Gear z} (lbs)	F_{Ext x} (lbs)	F_{Ext y} (lbs)	F_{Ext z} (lbs)	F_{Buoyant x} (lbs)	F_{Buoyant y} (lbs)	F_{Buoyant z} (lbs)	F_{Total x} (lbs)	F_{Total y} (lbs)	F_{Total z} (lbs)	Rho (slugs/ft^3)	Absolute Viscosity	Kinematic Viscosity	Temperature (R)	P_{SL} (psf)	P_{Ambient} (psf)	Turbulence Magnitude (ft/sec)	Turbulence X Direction (deg)	Wind V_{North} (ft/s)	Wind V_{East} (ft/s)	Wind V_{Down} (ft/s)	Roll Turbulence (deg/sec)	Pitch Turbulence (deg/sec)	Yaw Turbulence (deg/sec)	I_{xx}	I_{xy}	I_{xz}	I_{yx}	I_{yy}	I_{yz}	I_{zx}	I_{zy}	I_{zz}	Mass	Weight	X_{cg}	Y_{cg}	Z_{cg}	Altitude ASL (ft)	Altitude AGL (ft)	Phi (deg)	Theta (deg)	Psi (deg)	Q(1)_{LOCAL}	Q(2)_{LOCAL}	Q(3)_{LOCAL}	Q(4)_{LOCAL}	Q(1)_{ECEF}	Q(2)_{ECEF}	Q(3)_{ECEF}	Q(4)_{ECEF}	Q(1)_{ECI}	Q(2)_{ECI}	Q(3)_{ECI}	Q(4)_{ECI}	Alpha (deg)	Beta (deg)	Latitude (deg)	Latitude Geodetic (deg)	Longitude (deg)	X_{ECI} (ft)	Y_{ECI} (ft)	Z_{ECI} (ft)	X_{ECEF} (ft)	Y_{ECEF} (ft)	Z_{ECEF} (ft)	Earth Position Angle (deg)	Distance AGL (ft)	Terrain Elevation (ft)	aero/force/DRAG	aero/force/SIDE	aero/force/LIFT	aero/force/ROLL	aero/force/PITCH	aero/force/YAW	calculations/pitch-weights-delta/mass-center-m	fcs/wing-sweep-dmd	propulsion/engine[0]/EGT-R	propulsion/engine[1]/EGT-R	aero/function/KdGE	aero/function/kCLge	aero/coefficients/Cmach	aero/coefficients/CdTNK	aero/coefficients/CdMach	aero/coefficients/ClSweepFactor	aero/coefficients/ClBAS	aero/coefficients/ClDSLM	aero/coefficients/ClDFM	aero/coefficients/ClDSp	aero/coefficients/ClDS1	aero/coefficients/ClUC	aero/coefficients/ClDS2	aero/coefficients/Cl	aero/coefficients/CdUC	aero/coefficients/CdDSp	aero/coefficients/CdDBRK	aero/coefficients/CdBAS	aero/coefficients/CdDSLM	aero/coefficients/CdDFM	aero/coefficients/CdDS1	aero/coefficients/CdDS2	aero/coefficients/Cd	aero/coefficients/CyBAS	aero/coefficients/CyP	aero/coefficients/CyR	aero/coefficients/CyDA	aero/coefficients/CyDR	aero/coefficients/Cy	aero/coefficients/CLBAS	aero/coefficients/CLP	aero/coefficients/CLR	aero/coefficients/CLDA	aero/coefficients/CLDR	aero/coefficients/CL	aero/coefficients/CMBAS	aero/coefficients/DCMAIM	aero/coefficients/DCMB0	aero/coefficients/CMQ	aero/coefficients/CMDS1	aero/coefficients/CMDS2	aero/coefficients/DCMDS1	aero/coefficients/DCMDS2	aero/coefficients/CMBRK	aero/coefficients/CMUC	aero/coefficients/CMDSp	aero/coefficients/CMDFM	aero/coefficients/CM	aero/coefficients/CNBAS	aero/coefficients/DCNDS	aero/coefficients/CNP	aero/coefficients/CNR	aero/coefficients/CNDA	aero/coefficients/CNDR	aero/coefficients/CN	systems/hook/tailhook-control	systems/hook/tailhook-cmd-disagreement	systems/hook/ready	systems/hook/hook-decel-multiplier	systems/hook/hook-decel-force	systems/hook/force	systems/hook/animation-norm	Pitch Trim Sum	Elevator Control	Sweep Position	Sweep Control	elevator position	Ground Spoilers Control	Left elevator normalization	Right elevator normalization	Stabilizer Control	elevator normalization	fcs/stabilizer-1p-factor	fcs/stabilizer-2p-factor	fcs/flap-windfx-volume	fcs/gear-windfx-volume	fcs/stabilizer-1p	fcs/stabilizer-2p	Roll Trim Sum	Left Aileron Control	Right Aileron Control	left aileron normalization	right aileron normalization	aero/cn-sin-82beta	fcs/yaw-damper-active	fcs/pitch-damper-active	fcs/roll-damper-active	Pilot G	Yaw Damper Rate	Pitch Damper Rate	Roll Damper Rate	Rudder Command Sum	Rudder Sum	Rudder Control	rudder normalization	Flaps Control	flap normalization	Slats Control	Slat normalization	Gear Control	Speedbrake Control	fcs/hook-control	cg-x-offset-chord-in	cg-x-chord-percent	aero-cos-alpha	cbarq-2vo	aero-sin-alpha	CLxzcg	CNycg	NOSE_LG WOW	NOSE_LG stroke (ft)	NOSE_LG stroke velocity (ft/sec)	NOSE_LG compress force (lbs)	NOSE_LG wheel side force (lbs)	NOSE_LG wheel roll force (lbs)	NOSE_LG body X force (lbs)	NOSE_LG body Y force (lbs)	NOSE_LG wheel velocity vec X (ft/sec)	NOSE_LG wheel velocity vec Y (ft/sec)	NOSE_LG wheel rolling velocity (ft/sec)	NOSE_LG wheel side velocity (ft/sec)	NOSE_LG wheel slip (deg)	LEFT_MLG WOW	LEFT_MLG stroke (ft)	LEFT_MLG stroke velocity (ft/sec)	LEFT_MLG compress force (lbs)	LEFT_MLG wheel side force (lbs)	LEFT_MLG wheel roll force (lbs)	LEFT_MLG body X force (lbs)	LEFT_MLG body Y force (lbs)	LEFT_MLG wheel velocity vec X (ft/sec)	LEFT_MLG wheel velocity vec Y (ft/sec)	LEFT_MLG wheel rolling velocity (ft/sec)	LEFT_MLG wheel side velocity (ft/sec)	LEFT_MLG wheel slip (deg)	RIGHT_MLG WOW	RIGHT_MLG stroke (ft)	RIGHT_MLG stroke velocity (ft/sec)	RIGHT_MLG compress force (lbs)	RIGHT_MLG wheel side force (lbs)	RIGHT_MLG wheel roll force (lbs)	RIGHT_MLG body X force (lbs)	RIGHT_MLG body Y force (lbs)	RIGHT_MLG wheel velocity vec X (ft/sec)	RIGHT_MLG wheel velocity vec Y (ft/sec)	RIGHT_MLG wheel rolling velocity (ft/sec)	RIGHT_MLG wheel side velocity (ft/sec)	RIGHT_MLG wheel slip (deg)	LEFT_WING_TIP WOW	LEFT_WING_TIP stroke (ft)	LEFT_WING_TIP stroke velocity (ft/sec)	LEFT_WING_TIP compress force (lbs)	RIGHT_WING_TIP WOW	RIGHT_WING_TIP stroke (ft)	RIGHT_WING_TIP stroke velocity (ft/sec)	RIGHT_WING_TIP compress force (lbs)	FRONT_BODY_LEFT WOW	FRONT_BODY_LEFT stroke (ft)	FRONT_BODY_LEFT stroke velocity (ft/sec)	FRONT_BODY_LEFT compress force (lbs)	REAR_BODY_LEFT WOW	REAR_BODY_LEFT stroke (ft)	REAR_BODY_LEFT stroke velocity (ft/sec)	REAR_BODY_LEFT compress force (lbs)	REAR_BODY_RIGHT WOW	REAR_BODY_RIGHT stroke (ft)	REAR_BODY_RIGHT stroke velocity (ft/sec)	REAR_BODY_RIGHT compress force (lbs)	 Total Gear Force_X (lbs)	 Total Gear Force_Y (lbs)	 Total Gear Force_Z (lbs)	 Total Gear Moment_L (ft-lbs)	 Total Gear Moment_M (ft-lbs)	 Total Gear Moment_N (ft-lbs)	F110-GE-400_N1[0]	F110-GE-400_N2[0]	Direct Thrust (engine 0 in lbs)	F110-GE-400_N1[1]	F110-GE-400_N2[1]	Direct Thrust (engine 1 in lbs)	Fuel Tank 0	Fuel Tank 1	Fuel Tank 2	Fuel Tank 3	Fuel Tank 4	Fuel Tank 5	Fuel Tank 6	Fuel Tank 7	Fuel Tank 8	Fuel Tank 9	Fuel Tank 10	Fuel Tank 11	/fdm/jsbsim/fcs/speedbrake-pos-norm	/fdm/jsbsim/fcs/slat-pos-norm-deg	/fdm/jsbsim/fcs/slat-cmd-norm	/fdm/jsbsim/propulsion/engine/fuel-flow-rate-pps	/fdm/jsbsim/propulsion/engine[1]/fuel-flow-rate-pps	/fdm/jsbsim/velocities/mach	/fdm/jsbsim/systems/hook/tailhook-cmd-norm	/fdm/jsbsim/systems/hook/hook-decel-force	/fdm/jsbsim/forces/fbx-prop-lbs	/fdm/jsbsim/gear/tailhook-pos-norm	/fdm/jsbsim/fcs/wing-sweep-dmd	/fdm/jsbsim/fcs/wing-sweep-cmd
529.9	-1.53E-05	-0.139238581	1.53E-05	0.033262425	-0.000426764	-0.000426764	-11.20838394	0.001977488	0.997872748	0.003468656	0.069416595	0.002387844	-0.002455189	-0.004810929	0.000937877	0.003109188	0.066547607	-0.000628113	115.5453587	13227337.29	564.0978744	1639.75724	556.612435	-8.630019848	82.06197367	-1.523333283	0.004328888	-0.223497985	0.166225442	-1.464745026	0.755488507	2.749278592	-0.000865226	-32.63085207	558.0631464	0.022814002	82.29177337	-2.545021709	1636.629439	-101.1998337	78.78841997	547.8841357	-101.1998338	-133.7838307	546.4967643	8.319906862	7077.63459	-0.979229577	47198.07936	6.668623361	-116.56373	-1.265472762	-47725.65368	4137.639173	0	0	0	0	0	0	0	0	0	0	0	4021.075443	-1.265472762	-47725.65368	0.000726229	3.04E-07	0.000418645	401.2056277	2116.22	500.1492004	0	0	8.743213601	0.764932073	8.25E-42	0	0	0	62259.98593	-0.378194696	741.000948	-0.378194696	236352.9918	-1.673986875	741.000948	-1.673986875	292915.7087	1462.592934	47057.53674	405.1760432	0.004057879	-7.219121373	35633.10244	34818.40554	-0.249604462	7.543184531	104.5980847	0.610100981	-0.053374411	0.038506823	0.789585455	-0.269139229	0.744288722	0.554040512	-0.258142372	0.26410188	-0.733446161	-0.568316214	0.263293764	8.388362044	0.002317233	44.53458829	44.72666896	0.953755469	14894315.05	824303.389	14676712.62	14915040.84	248301.288	14676712.62	2.213961483	34818.40554	814.6923057	7077.63	-0.97923	47198.1	-18.0377	-11427.3	3.64514	10.2915	0.299779	1600.44	1600.44	0.0052045	1	0.773818	0	0.773818	1	0.873833	0.0445515	0.0184895	0	-0.00257786	0	-1.21671	0.934296	0	0	0	0.1325	0.00435748	0.0035036	-0.000257539	0.166275	0.140103	-3.23E-05	5.88E-07	1.21E-06	8.82E-07	1.02E-05	-1.94E-05	-4.27E-06	-9.15E-07	1.74E-07	-7.75E-07	2.06E-07	-5.58E-06	0.0159145	0	-0.055	-0.000202691	-0.0131942	-0.0188388	0.147885	0.278599	0	0	0	-0.0010398	-0.023043	4.48E-06	-9.04E-09	-3.53E-07	-3.17E-07	-1.96E-07	-2.89E-06	1.13E-06	0	0	0	0	0	4137.6035	3.00E-08	-0.337893088	-0.195623204	0.299779185	20.3849846	-0.195623204	0	-11.208812	-11.2079558	-0.195623086	-0.337893088	0	10	6.14492287	0	0	-112.083839	-3.27E-05	-7.45E-06	-7.45E-06	-3.27E-05	-3.27E-05	0.000331635	1	1	1	1.01504051	8.34E-05	0.000345291	-1.73E-05	1.53E-05	9.86E-05	3.45E-05	9.86E-05	0.997872748	0.033262425	0.100795227	1.71351886	0	0	0	-13.8239568	-0.138239568	0.989301985	0.01	0.145882084	-0.130600408	4.10E-07	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	0	65.0005	80.0003	2068.82	65.0005	80.0003	2068.82	2575.08	3642.86	0	281.251	0	286.2	73.0516	73.0516	0	0	11.0231	11.0231	0	1.71351886	0.100795227	0.361292044	0.361292044	0.574483346	0	0	4137.639173	3.00E-08	0.2997786	0.299779185

UBody	VBody	WBody
556.612435	-8.630019848	82.06197367
weight 47057.53674

Altitude ASL (ft)
35633.10244

Phi (deg)	Theta (deg)
-0.249604462	7.543184531
Psi (deg)
104.5980847
Alpha (deg)
8.388362044
elevator normalization -0.337893088
Fuel Tank 0	Fuel Tank 1	Fuel Tank 2	Fuel Tank 3	Fuel Tank 4	Fuel Tank 5	Fuel Tank 6	Fuel Tank 7	Fuel Tank 8	Fuel Tank 9	Fuel Tank 10	Fuel Tank 11
2575.08	3642.86	0	281.251	0	286.2	73.0516	73.0516	0	0	11.0231	11.0231
/fdm/jsbsim/velocities/mach
0.574483346

-->
  <psi unit="DEG">       200.0  </psi>
  <roc unit="FT/SEC">0</roc>
  <alpha unit="DEG">8.5479</alpha>
</initialize>
