<?xml version="1.0"?>

<!-- McDonnell Douglas DC-10 Aerodynamics -->
<!-- Copyright (c) 2026 Josh Davidson (Octal450) -->

<aerodynamics>
	
	<function name="aero/function/kCLge">
		<description>Lift factor due to ground effect</description>
		<table>
			<independentVar lookup="row">aero/h_b-mac-ft</independentVar>
			<tableData>
				0.00  1.203
				0.10  1.127
				0.15  1.090
				0.20  1.073
				0.30  1.046
				0.40  1.028
				0.50  1.019
				0.60  1.013
				0.70  1.008
				0.80  1.006
				0.90  1.003
				1.00  1.002
				1.10  1.000
			</tableData>
		</table>
	</function>
	
	<function name="aero/function/kCDge">
		<description>Drag factor due to ground effect</description>
		<table>
			<independentVar lookup="row">aero/h_b-mac-ft</independentVar>
			<tableData>
				0.00  0.480
				0.10  0.515
				0.15  0.629
				0.20  0.709
				0.30  0.815
				0.40  0.882
				0.50  0.928
				0.60  0.962
				0.70  0.988
				0.80  1.000
			</tableData>
		</table>
	</function>
	
	<axis name="LIFT">
		
		<function name="aero/coefficient/CLalpha">
			<description>Lift due to alpha</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<property>aero/function/kCLge</property>
				<table>
					<independentVar lookup="row">aero/alpha-deg</independentVar>
					<independentVar lookup="column">velocities/mach</independentVar>
					<independentVar lookup="table">fcs/slat-pos-norm</independentVar>
					<tableData breakPoint="0">
						         0.2     0.9
						-9.8475 -0.5652 -0.5935
						-2.0912  0.0625  0.0656
						-0.0098  0.2386  0.2505
						 2.2280  0.4260  0.4473
						 4.2779  0.5779  0.6068
						 6.4218  0.7540  0.7917
						 8.4561  0.9163  0.9621
						 9.2699  0.9842  0.8076
						10.7094  1.0843  0.6617
						11.6170  1.1538  0.5827
						12.6496  1.2184  0.5949
						13.7292  1.0622  0.6074
						14.7930  0.9804  0.5648
						15.6981  0.9051  0.5285
						16.6352  0.9187  0.4910
						17.5725  0.9219  0.4535
						18.6045  0.8842  0.4121
						19.6052  0.8459  0.3720
						30.1264  0.4196 -0.0494
					</tableData>
					<tableData breakPoint="1">
						         0.2     0.9
						-9.8475 -0.5652 -0.5935
						-2.0912  0.0625  0.0656
						-0.0098  0.2386  0.2505
						 2.2280  0.4260  0.4473
						 4.2779  0.5779  0.6068
						 6.4218  0.7540  0.7917
						 8.4561  0.9163  0.9621
						 9.2699  0.9842  1.0303
						10.7094  1.0843  1.1507
						11.6170  1.1538  0.9945
						12.6496  1.2184  0.9127
						13.7292  1.2911  0.8374
						14.7930  1.3444  0.8510
						15.6981  1.1882  0.8542
						16.6352  1.1064  0.8180
						17.5725  1.0311  0.7818
						18.6045  1.0447  0.7441
						19.6052  1.0479  0.7058
						30.1264  0.6376  0.2795
					</tableData>
				</table>
			</product>
		</function>
		
		<function name="aero/coefficient/CLq">
			<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>1.36</value>
			</product>
		</function>
		
		<function name="aero/coefficient/CLadot">
			<description>Lift due to alpha rate</description>
			<product>
				<property>aero/qbarUW-psf</property>
				<property>metrics/Sw-sqft</property>
				<property>aero/alphadot-rad_sec</property>
				<property>aero/ci2vel</property>
				<value>0.6384</value>
			</product>
		</function>
		
		<function name="aero/coefficient/CLflap">
			<description>Lift due to flaps</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<property>aero/function/kCLge</property>
				<table>
					<independentVar lookup="row">fcs/flap-pos-deg</independentVar>
					<tableData>
						 0  0.0000
						15  0.1606
						22  0.3312
						35  0.4541
						50  0.6442
					</tableData>
				</table>
			</product>
		</function>
		
		<function name="aero/coefficient/CLslat">
			<description>Lift due to slats</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<property>aero/function/kCLge</property>
				<property>fcs/slat-pos-norm</property>
				<value>0.1745</value>
			</product>
		</function>
		
		<function name="aero/coefficient/CLde_lo">
			<description>Lift due to left outer elevator</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<toradians><property>/systems/fcs/elevator-out-l/final-deg</property></toradians>
				<value>0.0116548</value>
			</product>
		</function>
		
		<function name="aero/coefficient/CLde_li">
			<description>Lift due to left inner elevator</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<toradians><property>/systems/fcs/elevator-in-l/final-deg</property></toradians>
				<value>0.0116548</value>
			</product>
		</function>
		
		<function name="aero/coefficient/CLde_ri">
			<description>Lift due to right inner elevator</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<toradians><property>/systems/fcs/elevator-in-r/final-deg</property></toradians>
				<value>0.0116548</value>
			</product>
		</function>
		
		<function name="aero/coefficient/CLde_ro">
			<description>Lift due to right outer elevator</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<toradians><property>/systems/fcs/elevator-out-r/final-deg</property></toradians>
				<value>0.0116548</value>
			</product>
		</function>
		
		<function name="aero/coefficient/CLdstab">
			<description>Lift due to stabilizer</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<toradians><property>/systems/fcs/stabilizer/final-deg</property></toradians>
				<value>0.0021645</value>
			</product>
		</function>
		
		<function name="aero/coefficient/CLda_lo">
			<description>Lift due to left outer aileron</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<toradians><property>/systems/fcs/aileron-out-l/final-deg</property></toradians>
				<value>0.018246</value>
			</product>
		</function>
		
		<function name="aero/coefficient/CLda_li">
			<description>Lift due to left inner aileron</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<toradians><property>/systems/fcs/aileron-in-l/final-deg</property></toradians>
				<value>0.018246</value>
			</product>
		</function>
		
		<function name="aero/coefficient/CLda_ri">
			<description>Lift due to right inner aileron</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<toradians><property>/systems/fcs/aileron-in-r/final-deg</property></toradians>
				<value>0.018246</value>
			</product>
		</function>
		
		<function name="aero/coefficient/CLda_ro">
			<description>Lift due to right outer aileron</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<toradians><property>/systems/fcs/aileron-out-r/final-deg</property></toradians>
				<value>0.018246</value>
			</product>
		</function>
		
		<function name="aero/coefficient/CLdsp_l">
			<description>Lift due to left spoiler</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<toradians><property>/systems/fcs/spoiler-left-deg</property></toradians>
				<value>-0.0261</value>
			</product>
		</function>
		
		<function name="aero/coefficient/CLdsp_r">
			<description>Lift due to right spoiler</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<toradians><property>/systems/fcs/spoiler-right-deg</property></toradians>
				<value>-0.0261</value>
			</product>
		</function>
	
	</axis>
	
	<axis name="DRAG">
		
		<function name="aero/coefficient/CD0">
			<description>Drag at zero lift</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<value>0.021</value>
			</product>
		</function>
		
		<function name="aero/coefficient/CDalpha">
			<description>Drag due to alpha</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<table>
					<independentVar lookup="row">aero/alpha-deg</independentVar>
					<tableData>
						-14.7960  0.0549
						-12.2922  0.0512
						 -9.4900  0.0379
						 -6.9768  0.0224
						 -3.2108  0.0049
						  0.0000  0.0000
						  3.2108  0.0049
						  6.9768  0.0224
						  9.4900  0.0379
						 12.2922  0.0512
						 14.7960  0.0549
					</tableData>
				</table>
			</product>
		</function>
		
		<function name="aero/coefficient/CDi">
			<description>Drag due to lift</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<property>aero/function/kCDge</property>
				<property>aero/cl-squared</property>
				<value>0.045</value>
			</product>
		</function>
		
		<function name="aero/coefficient/CDmach">
			<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>
						0.88  0.000
						1.10  0.016
						1.80  0.012
					</tableData>
				</table>
			</product>
		</function>
		
		<function name="aero/coefficient/CDbeta">
			<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  1.23
						-0.26  0.05
						 0.00  0.00
						 0.26  0.05
						 1.57  1.23
					</tableData>
				</table>
			</product>
		</function>
		
		<function name="aero/coefficient/CDgear">
			<description>Drag due to gear</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<property>/systems/gear/all-norm</property>
				<value>0.0171</value>
			</product>
		</function>
		
		<function name="aero/coefficient/CDflap">
			<description>Drag due to flaps</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<property>fcs/flap-pos-deg</property>
				<value>0.00132</value>
			</product>
		</function>
		
		<function name="aero/coefficient/CDslat">
			<description>Drag due to slats</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<property>fcs/slat-pos-deg</property>
				<value>0.00128</value>
			</product>
		</function>
		
		<function name="aero/coefficient/CDde_lo">
			<description>Drag due to left outer elevator</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<abs><toradians><property>/systems/fcs/elevator-out-l/final-deg</property></toradians></abs>
				<value>0.003625</value>
			</product>
		</function>
		
		<function name="aero/coefficient/CDde_li">
			<description>Drag due to left inner elevator</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<abs><toradians><property>/systems/fcs/elevator-in-l/final-deg</property></toradians></abs>
				<value>0.003625</value>
			</product>
		</function>
		
		<function name="aero/coefficient/CDde_ri">
			<description>Drag due to right inner elevator</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<abs><toradians><property>/systems/fcs/elevator-in-r/final-deg</property></toradians></abs>
				<value>0.003625</value>
			</product>
		</function>
		
		<function name="aero/coefficient/CDde_ro">
			<description>Drag due to right outer elevator</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<abs><toradians><property>/systems/fcs/elevator-out-r/final-deg</property></toradians></abs>
				<value>0.003625</value>
			</product>
		</function>
		
		<function name="aero/coefficient/CDdstab">
			<description>Drag due to stabilizer</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<abs><toradians><property>/systems/fcs/stabilizer/final-deg</property></toradians></abs>
				<value>0.0043</value>
			</product>
		</function>
		
		<function name="aero/coefficient/CDda_lo">
			<description>Drag due to left outer aileron</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<abs><toradians><property>/systems/fcs/aileron-out-l/final-deg</property></toradians></abs>
				<value>0.0023147</value>
			</product>
		</function>
		
		<function name="aero/coefficient/CDda_li">
			<description>Drag due to left inner aileron</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<abs><toradians><property>/systems/fcs/aileron-in-l/final-deg</property></toradians></abs>
				<value>0.0023147</value>
			</product>
		</function>
		
		<function name="aero/coefficient/CDda_ri">
			<description>Drag due to right inner aileron</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<abs><toradians><property>/systems/fcs/aileron-in-r/final-deg</property></toradians></abs>
				<value>0.0023147</value>
			</product>
		</function>
		
		<function name="aero/coefficient/CDda_ro">
			<description>Drag due to right outer aileron</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<abs><toradians><property>/systems/fcs/aileron-out-r/final-deg</property></toradians></abs>
				<value>0.0023147</value>
			</product>
		</function>
		
		<function name="aero/coefficient/CDdsp_l">
			<description>Drag due to left spoiler</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<toradians><property>/systems/fcs/spoiler-left-deg</property></toradians>
				<value>0.0200716</value>
			</product>
		</function>
		
		<function name="aero/coefficient/CDdsp_r">
			<description>Drag due to right spoiler</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<toradians><property>/systems/fcs/spoiler-right-deg</property></toradians>
				<value>0.0200716</value>
			</product>
		</function>
	
	</axis>
	
	<axis name="SIDE">
		
		<function name="aero/coefficient/CYbeta">
			<description>Side force due to beta</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<property>aero/beta-rad</property>
				<value>-0.6093</value>
			</product>
		</function>
		
		<function name="aero/coefficient/CYp">
			<description>Side force due to roll rate</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<property>aero/bi2vel</property>
				<property>velocities/p-aero-rad_sec</property>
				<table>
					<independentVar lookup="row">aero/Re</independentVar>
					<tableData>
						29913298  0.4518
						32904628  0.0452
						44869948  0.0201
						59461352  0.0114
					</tableData>
				</table>
			</product>
		</function>
		
		<function name="aero/coefficient/CYr">
			<description>Side force due to yaw rate</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<property>aero/bi2vel</property>
				<property>velocities/r-aero-rad_sec</property>
				<value>0.6597</value>
			</product>
		</function>
		
		<function name="aero/coefficient/CYdr_u">
			<description>Side force due to upper rudder</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<toradians><property>/systems/fcs/rudder-upper/final-deg</property></toradians>
				<value>-0.09015</value>
			</product>
		</function>
		
		<function name="aero/coefficient/CYdr_l">
			<description>Side force due to lower rudder</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<toradians><property>/systems/fcs/rudder-lower/final-deg</property></toradians>
				<value>-0.09015</value>
			</product>
		</function>
	
	</axis>
	
	<axis name="ROLL">
		
		<function name="aero/coefficient/Clbeta">
			<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-deg</property>
				<table>
					<independentVar lookup="row">aero/alpha-deg</independentVar>
					<tableData>
						-4.4412 -0.00150
						-2.2116 -0.00167
						 0.1900 -0.00176
						 2.4828 -0.00189
						 4.9473 -0.00189
						 6.1394 -0.00194
					</tableData>
				</table>
			</product>
		</function>
		
		<function name="aero/coefficient/Clp">
			<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>-0.61</value>
			</product>
		</function>
		
		<function name="aero/coefficient/Clr">
			<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>
				<value>0.1</value>
			</product>
		</function>
		
		<function name="aero/coefficient/Clda_lo">
			<description>Roll moment due to left outer aileron</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<property>metrics/bw-ft</property>
				<toradians><property>/systems/fcs/aileron-out-l/final-deg</property></toradians>
				<value>0.0184579</value>
			</product>
		</function>
		
		<function name="aero/coefficient/Clda_li">
			<description>Roll moment due to left inner aileron</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<property>metrics/bw-ft</property>
				<toradians><property>/systems/fcs/aileron-in-l/final-deg</property></toradians>
				<value>0.0314954</value>
			</product>
		</function>
		
		<function name="aero/coefficient/Clda_ri">
			<description>Roll moment due to right inner aileron</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<property>metrics/bw-ft</property>
				<toradians><property>/systems/fcs/aileron-in-r/final-deg</property></toradians>
				<value>-0.0314954</value>
			</product>
		</function>
		
		<function name="aero/coefficient/Clda_ro">
			<description>Roll moment due to right outer aileron</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<property>metrics/bw-ft</property>
				<toradians><property>/systems/fcs/aileron-out-r/final-deg</property></toradians>
				<value>-0.0184579</value>
			</product>
		</function>
		
		<function name="aero/coefficient/Cldsp_l">
			<description>Roll moment due to left spoiler</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<property>metrics/bw-ft</property>
				<toradians><property>/systems/fcs/spoiler-left-deg</property></toradians>
				<value>-0.0155</value>
			</product>
		</function>
		
		<function name="aero/coefficient/Cldsp_r">
			<description>Roll moment due to right spoiler</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<property>metrics/bw-ft</property>
				<toradians><property>/systems/fcs/spoiler-right-deg</property></toradians>
				<value>0.0155</value>
			</product>
		</function>
		
		<function name="aero/coefficient/Cldr_u">
			<description>Roll moment due to upper rudder</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<property>metrics/bw-ft</property>
				<toradians><property>/systems/fcs/rudder-upper/final-deg</property></toradians>
				<value>0.005</value>
			</product>
		</function>
		
		<function name="aero/coefficient/Cldr_l">
			<description>Roll moment due to lower rudder</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<property>metrics/bw-ft</property>
				<toradians><property>/systems/fcs/rudder-lower/final-deg</property></toradians>
				<value>0.005</value>
			</product>
		</function>
	
	</axis>
	
	<axis name="PITCH">
		
		<function name="aero/coefficient/Cmalpha">
			<description>Pitch moment due to alpha</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<property>metrics/cbarw-ft</property>
				<table>
					<independentVar lookup="row">aero/alpha-deg</independentVar>
					<tableData>
						-9.4468  0.2663
						-6.3284  0.1750
						-5.4416  0.1468
						-4.3131  0.1160
						-3.0234  0.0799
						-2.0214  0.0479
						-0.6629  0.0176
						 0.4655 -0.0120
						 1.6628 -0.0375
						 2.9406 -0.0606
						 4.0685 -0.0755
						 5.2651 -0.0832
						 6.3583 -0.0931
						 7.3937 -0.0957
						 8.5212 -0.0981
						 9.8677 -0.1135
						11.3179 -0.1356
						20.1549 -0.2703
					</tableData>
				</table>
			</product>
		</function>
		
		<function name="aero/coefficient/Cmq">
			<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>-33.1</value>
			</product>
		</function>
		
		<function name="aero/coefficient/Cmadot">
			<description>Pitch moment due to alpha rate</description>
			<product>
				<property>aero/qbarUW-psf</property>
				<property>metrics/Sw-sqft</property>
				<property>metrics/cbarw-ft</property>
				<property>aero/ci2vel</property>
				<property>aero/alphadot-rad_sec</property>
				<value>-12.6734</value>
			</product>
		</function>
		
		<function name="aero/coefficient/Cmde_lo">
			<description>Pitch moment due to left outer elevator</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<property>metrics/cbarw-ft</property>
				<toradians><property>/systems/fcs/elevator-out-l/final-deg</property></toradians>
				<value>-0.17664782</value>
			</product>
		</function>
		
		<function name="aero/coefficient/Cmde_li">
			<description>Pitch moment due to left inner elevator</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<property>metrics/cbarw-ft</property>
				<toradians><property>/systems/fcs/elevator-in-l/final-deg</property></toradians>
				<value>-0.17664782</value>
			</product>
		</function>
		
		<function name="aero/coefficient/Cmde_ri">
			<description>Pitch moment due to right inner elevator</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<property>metrics/cbarw-ft</property>
				<toradians><property>/systems/fcs/elevator-in-r/final-deg</property></toradians>
				<value>-0.17664782</value>
			</product>
		</function>
		
		<function name="aero/coefficient/Cmde_ro">
			<description>Pitch moment due to right outer elevator</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<property>metrics/cbarw-ft</property>
				<toradians><property>/systems/fcs/elevator-out-r/final-deg</property></toradians>
				<value>-0.17664782</value>
			</product>
		</function>
		
		<function name="aero/coefficient/Cmdstab">
			<description>Pitch moment due to stabilizer</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<property>metrics/cbarw-ft</property>
				<toradians><property>/systems/fcs/stabilizer/final-deg</property></toradians>
				<value>-2.39235</value>
			</product>
		</function>
		
		<function name="aero/coefficient/Cmdsp">
			<description>Pitch moment due to symmetrical spoiler</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<property>metrics/cbarw-ft</property>
				<table>
					<independentVar lookup="row">aero/h_b-mac-ft</independentVar>
					<tableData>
						0  0.5
						1  1.0
					</tableData>
				</table>
				<toradians><property>/systems/fcs/spoiler-symmetrical-deg</property></toradians>
				<value>0.011</value>
			</product>
		</function>
	
	</axis>
	
	<axis name="YAW">
		
		<function name="aero/coefficient/Cnbeta">
			<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-deg</property>
				<table>
					<independentVar lookup="row">aero/alpha-deg</independentVar>
					<tableData>
						-4.7093  0.00198
						-2.2164  0.00211
						 0.2903  0.00194
						 2.9836  0.00180
						 5.5629  0.00207
					</tableData>
				</table>
			</product>
		</function>
		
		<function name="aero/coefficient/Cnr">
			<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>-0.3</value>
			</product>
		</function>
		
		<function name="aero/coefficient/Cndr_u">
			<description>Yaw moment due to upper rudder</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<property>metrics/bw-ft</property>
				<toradians><property>/systems/fcs/rudder-upper/final-deg</property></toradians>
				<value>0.01621</value>
			</product>
		</function>
		
		<function name="aero/coefficient/Cndr_l">
			<description>Yaw moment due to lower rudder</description>
			<product>
				<property>aero/qbar-psf</property>
				<property>metrics/Sw-sqft</property>
				<property>metrics/bw-ft</property>
				<toradians><property>/systems/fcs/rudder-lower/final-deg</property></toradians>
				<value>0.01621</value>
			</product>
		</function>
	
	</axis>

</aerodynamics>
