
		
		<axis name="LIFT">
			
			<!-- Lift above 0.85 and below -0.85 is generalised -->
			<function name="aero/force/Lift_alpha">
				<description>Lift due to alpha</description>
				<product>
					<property>aero/qbar-psf</property>
					<property>metrics/Sw-sqft</property>
					<table>
						<independentVar lookup="row">aero/alpha-rad</independentVar>
						<tableData>
							-1.57  0.0000
							-1.22 -0.5736
							-1.05 -0.7728
							-0.88 -0.8924
							-0.61 -0.3918
							-0.03 -0.9796
							0.00  0.3313
							0.02  1.3108
							0.60  0.7231
							0.88  1.1076
							1.05  0.9592
							1.22  0.7120
							1.57  0.0000
						</tableData>
					</table>
				</product>
			</function>
			
			<function name="aero/force/Lift_pitch_rate">
				<description>Lift due to pitch rate</description>
				<product>
					<property>aero/qbar-psf</property>
					<property>metrics/Sw-sqft</property>
					<property>velocities/q-aero-rad_sec</property>
					<property>aero/ci2vel</property>
					<value> 7.3646 </value>
				</product>
			</function>
			
			<function name="aero/force/Lift_alpha_rate">
				<description>Lift due to alpha rate</description>
				<product>
					<property>aero/qbar-psf</property>
					<property>metrics/Sw-sqft</property>
					<property>aero/alphadot-rad_sec</property>
					<property>aero/ci2vel</property>
					<value> 1.0635 </value>
				</product>
			</function>
			
			<function name="aero/force/Lift_elevator">
				<description>Lift due to Elevator Deflection</description>
				<product>
					<property>aero/qbar-psf</property>
					<property>metrics/Sw-sqft</property>
					<property>fcs/elevator-pos-rad</property>
					<value> 0.2581 </value>
				</product>
			</function>
			
			<function name="aero/force/Lift_flap">
				<description>Delta Lift due to flaps</description>
				<product>
					<property>aero/qbar-psf</property>
					<property>metrics/Sw-sqft</property>
					<property>fcs/flap-pos-deg</property>
					<value> 0.0061 </value>
				</product>
			</function>
			
			
			<function name="aero/force/Lift_spoilers">
				<description>Delta Lift due to spoilers</description>
				<product>
					<property>aero/qbar-psf</property>
					<property>metrics/Sw-sqft</property>
					<property>fcs/speedbrake-pos-norm</property>
					<value> -0.0500 </value>
				</product>
			</function>
			
		</axis>
		
		<axis name="DRAG">
			
			<!-- CD0 is based on fuselage, wing, horizontal- en vertical tail -->
			<!-- Antennas, struts and wires are not taken into account        -->
			<!-- CD for gear (fixed and retractable) is defined below         -->
			<function name="aero/force/Drag_minimum">
				<description>Minimum drag</description>
				<product>
					<property>aero/qbar-psf</property>
					<property>metrics/Sw-sqft</property>
					<value> 0.0199 </value>
				</product>
			</function>
			
			<function name="aero/force/Drag_alpha">
				<description>Drag due to alpha</description>
				<product>
					<property>aero/qbar-psf</property>
					<property>metrics/Sw-sqft</property>
					<table>
						<independentVar lookup="row">aero/alpha-rad</independentVar>
						<tableData>
							-1.57    1.4088
							-0.02    0.0080
							0.00    0.0000
							0.02    0.0080
							1.57    1.4088
						</tableData>
					</table>
				</product>
			</function>
			
			<function name="aero/force/Drag_induced">
				<description>Induced drag</description>
				<product>
					<property>aero/qbar-psf</property>
					<property>metrics/Sw-sqft</property>
					<property>aero/cl-squared</property>
					<value> 0.0124 </value>
				</product>
			</function>
			
			<function name="aero/force/Drag_mach">
				<description>Drag due to mach</description>
				<product>
					<property>aero/qbar-psf</property>
					<property>metrics/Sw-sqft</property>
					<table>
						<independentVar lookup="row">velocities/mach</independentVar>
						<tableData>
							0.00    0.0000
							0.70    0.0000
							1.10    0.0230
							1.80    0.0150
						</tableData>
					</table>
				</product>
			</function>
			
			<function name="aero/force/Drag_beta">
				<description>Drag due to sideslip</description>
				<product>
					<property>aero/qbar-psf</property>
					<property>metrics/Sw-sqft</property>
					<table>
						<independentVar lookup="row">aero/beta-rad</independentVar>
						<tableData>
							-1.57    1.2300
							-0.26    0.0500
							0.00    0.0000
							0.26    0.0500
							1.57    1.2300
						</tableData>
					</table>
				</product>
			</function>
			
			<function name="aero/force/Drag_elevator">
				<description>Drag due to Elevator Deflection</description>
				<product>
					<property>aero/qbar-psf</property>
					<property>metrics/Sw-sqft</property>
					<abs><property>fcs/elevator-pos-rad</property></abs>
					<value> 0.0400 </value>
				</product>
			</function>
			
			<function name="aero/force/Drag_gear">
				<description>Drag due to gear</description>
				<product>
					<property>aero/qbar-psf</property>
					<property>metrics/Sw-sqft</property>
					<property>gear/gear-pos-norm</property>
					<value> 0.0120 </value>
				</product>
			</function>
			
			<function name="aero/force/Drag_flap">
				<description>Drag due to flaps</description>
				<product>
					<property>aero/qbar-psf</property>
					<property>metrics/Sw-sqft</property>
					<property>fcs/flap-pos-deg</property>
					<value> 0.0007 </value>
				</product>
			</function>
			
			
			<function name="aero/force/Drag_spoilers">
				<description>Drag due to spoilers</description>
				<product>
					<property>aero/qbar-psf</property>
					<property>metrics/Sw-sqft</property>
					<property>fcs/speedbrake-pos-norm</property>
					<value> 0.0199 </value>
				</product>
			</function>
			
		</axis>
		
		<axis name="SIDE">
			
			<function name="aero/force/Side_beta">
				<description>Side force due to beta</description>
				<product>
					<property>aero/qbar-psf</property>
					<property>metrics/Sw-sqft</property>
					<property>aero/beta-rad</property>
					<value> -0.4217 </value>
				</product>
			</function>
			
		</axis>
		
		<axis name="PITCH">
			
			<function name="aero/moment/Pitch_alpha">
				<description>Pitch moment due to alpha</description>
				<product>
					<property>aero/qbar-psf</property>
					<property>metrics/Sw-sqft</property>
					<property>metrics/cbarw-ft</property>
					<property>aero/alpha-rad</property>
					<value> -3.2148 </value>
				</product>
			</function>
			
			<function name="aero/moment/Pitch_elevator">
				<description>Pitch moment due to elevator</description>
				<product>
					<property>aero/qbar-psf</property>
					<property>metrics/Sw-sqft</property>
					<property>metrics/cbarw-ft</property>
					<property>fcs/elevator-pos-rad</property>
					<table>
						<independentVar lookup="row">velocities/mach</independentVar>
						<tableData>
							0.0    -2.3527
							2.0    -0.5882
						</tableData>
					</table>
				</product>
			</function>
			
			<function name="aero/moment/Pitch_damp">
				<description>Pitch moment due to pitch rate</description>
				<product>
					<property>aero/qbar-psf</property>
					<property>metrics/Sw-sqft</property>
					<property>metrics/cbarw-ft</property>
					<property>aero/ci2vel</property>
					<property>velocities/q-aero-rad_sec</property>
					<value> -67.5192 </value>
				</product>
			</function>
			
			<function name="aero/moment/Pitch_alphadot">
				<description>Pitch moment due to alpha rate</description>
				<product>
					<property>aero/qbar-psf</property>
					<property>metrics/Sw-sqft</property>
					<property>metrics/cbarw-ft</property>
					<property>aero/ci2vel</property>
					<property>aero/alphadot-rad_sec</property>
					<value> -9.7501 </value>
				</product>
			</function>
			
		</axis>
		
		<axis name="ROLL">
			
			<function name="aero/moment/Roll_beta">
				<description>Roll moment due to beta</description>
				<product>
					<property>aero/qbar-psf</property>
					<property>metrics/Sw-sqft</property>
					<property>metrics/bw-ft</property>
					<property>aero/beta-rad</property>
					<property>fcs/gear-no-wow</property>
					<table>
						<independentVar lookup="row">aero/alpha-rad</independentVar>
						<independentVar lookup="column">aero/Re</independentVar>
						<tableData>
							1088234  1197057  1632351  2164732
							-0.0349  -0.7131  -0.6943  -0.6932  -0.6928
							0.3491  -0.7131  -0.6943  -0.6932  -0.6928
						</tableData>
					</table>
				</product>
			</function>
			
			<function name="aero/moment/Roll_damp">
				<description>Roll moment due to roll rate</description>
				<product>
					<property>aero/qbar-psf</property>
					<property>metrics/Sw-sqft</property>
					<property>metrics/bw-ft</property>
					<property>aero/bi2vel</property>
					<property>velocities/p-aero-rad_sec</property>
					<value> -4.3832 </value>
				</product>
			</function>
			
			<function name="aero/moment/Roll_yaw">
				<description>Roll moment due to yaw rate</description>
				<product>
					<property>aero/qbar-psf</property>
					<property>metrics/Sw-sqft</property>
					<property>metrics/bw-ft</property>
					<property>aero/bi2vel</property>
					<property>velocities/r-aero-rad_sec</property>
					<table>
						<independentVar lookup="row">aero/alpha-rad</independentVar>
						<independentVar lookup="column">aero/Re</independentVar>
						<tableData>
							1088234  1197057  1632351  2164732
							-0.0349  -0.2764  -0.2764  -0.2764  -0.2764
							0.3491   3.6324   3.6324   3.6324   3.6324
						</tableData>
					</table>
				</product>
			</function>
			
			<function name="aero/moment/Roll_aileron">
				<description>Roll moment due to aileron</description>
				<product>
					<property>aero/qbar-psf</property>
					<property>metrics/Sw-sqft</property>
					<property>metrics/bw-ft</property>
					<property>fcs/left-aileron-pos-rad</property>
					<table>
						<independentVar lookup="row">velocities/mach</independentVar>
						<tableData>
							0.0    0.0600
							2.0    0.0150
						</tableData>
					</table>
				</product>
			</function>
			
			<function name="aero/moment/Roll_rudder">
				<description>Roll moment due to rudder</description>
				<product>
					<property>aero/qbar-psf</property>
					<property>metrics/Sw-sqft</property>
					<property>metrics/bw-ft</property>
					<property>fcs/rudder-pos-rad</property>
					<value> 0.0100 </value>
				</product>
			</function>
			
		</axis>
		
		<axis name="YAW">
			
			<!-- Stall initiator -->
			<function name="aero/moment/Yaw_alpha">
				<description>Yaw moment due to alpha</description>
				<product>
					<property>aero/qbar-psf</property>
					<property>metrics/Sw-sqft</property>
					<property>metrics/bw-ft</property>
					<property>aero/alpha-rad</property>
					<property>fcs/gear-no-wow</property>
					<table>
						<independentVar lookup="row">aero/beta-rad</independentVar>
						<independentVar lookup="column">aero/Re</independentVar>
						<tableData>
							1088234  1197057
							-0.3491  -1.0000   0.0000
							0.3491   1.0000   0.0000
						</tableData>
					</table>
				</product>
			</function>
			
			<function name="aero/moment/Yaw_beta">
				<description>Yaw moment due to beta</description>
				<product>
					<property>aero/qbar-psf</property>
					<property>metrics/Sw-sqft</property>
					<property>metrics/bw-ft</property>
					<property>aero/beta-rad</property>
					<value> 0.0608 </value>
				</product>
			</function>
			
			<function name="aero/moment/Yaw_roll_rate">
				<description>Yaw moment due to roll rate</description>
				<product>
					<property>aero/qbar-psf</property>
					<property>metrics/Sw-sqft</property>
					<property>metrics/bw-ft</property>
					<property>aero/bi2vel</property>
					<property>velocities/p-rad_sec</property>
					<table>
						<independentVar lookup="row">aero/Re</independentVar>
						<tableData>
							1088234  -0.0745
							1197057  -0.0074
							1632351  -0.0033
							2164732  -0.0019
						</tableData>
					</table>
				</product>
			</function>
			
			<function name="aero/moment/Yaw_damp">
				<description>Yaw moment due to yaw rate</description>
				<product>
					<property>aero/qbar-psf</property>
					<property>metrics/Sw-sqft</property>
					<property>metrics/bw-ft</property>
					<property>aero/bi2vel</property>
					<property>velocities/r-aero-rad_sec</property>
					<value> -0.0480 </value>
				</product>
			</function>
			
			<function name="aero/moment/Yaw_rudder">
				<description>Yaw moment due to rudder</description>
				<product>
					<property>aero/qbar-psf</property>
					<property>metrics/Sw-sqft</property>
					<property>metrics/bw-ft</property>
					<property>fcs/rudder-pos-rad</property>
					<value> -0.0374 </value>
				</product>
			</function>
			
			<function name="aero/moment/Yaw_aileron">
				<description>Adverse yaw</description>
				<product>
					<property>aero/qbar-psf</property>
					<property>metrics/Sw-sqft</property>
					<property>metrics/bw-ft</property>
					<property>fcs/left-aileron-pos-rad</property>
					<value> -0.0200 </value>
				</product>
			</function>
			
		</axis>
