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I think you're gonna need the "eliteness" tools and an XML editor. Looks like the values are stored in an xml file (which is in a pbo file).

Here is my config:

<!--

REFERENCES

[1] Technical Description.pdf

[2] Wikipedia

[3] Field manual

[4] Technical manual

[5] Blueprints

-->

<?xml version="1.0"?>

<GenHeli600 version="1.0">

<!-- Estimation

Calculated after the ration R_mass = (empty weight of dauphin) / (empty weight of MD500) ratio = (2271)/(722) = 3.1454293629.

Ixx = 11000/R_Mass = 3497

Iyy = 2704/R_Mass = 859

Ixx = 9900/R_Mass = 3147

-->

<MomentsOfInertia Ixx="3497" Iyy="859" Izz="3147"/>

<!--[2]

Empty Weight=722 kg

Max Takeoff Weight=1610 kg

Any value between empty weight and max takeoff weight is valid.

-->

<Mass mass="722"/>

<Fuselage rotationalResistance="100" >

<MainRotorDownwash scale="0.5">

<Low_a1 a1 ="-6">

0 1.4958

10.0000 1.4955

20.0000 1.4939

30.0000 1.4881

40.0000 1.4694

50.0000 1.4149

60.0000 1.2801

70.0000 1.0072

80.0000 0.5652

90.0000 0.0000

</Low_a1>

<Medium_a1 a1 ="0" scale="0.5">

0 1.4958

10.0000 1.4955

20.0000 1.4939

30.0000 1.4881

40.0000 1.4694

50.0000 1.4149

60.0000 1.2801

70.0000 1.0072

80.0000 0.5652

90.0000 0.0000

</Medium_a1>

<High_a1 a1 ="6" scale="0.5">

0 1.4958

10.0000 1.4955

20.0000 1.4939

30.0000 1.4881

40.0000 1.4694

50.0000 1.4149

60.0000 1.2801

70.0000 1.0072

80.0000 0.5652

90.0000 0.0000

</High_a1>

</MainRotorDownwash>

<MainRotorInplanewash scale="0.5">

<Low_a1 a1 ="-6">

0 0.1124

10.0000 0.1125

20.0000 0.1127

30.0000 0.1138

40.0000 0.1176

50.0000 0.1333

60.0000 0.2000

70.0000 0.4472

80.0000 1.0415

90.0000 1.5000

</Low_a1>

<Medium_a1 a1 ="0" scale="0.5">

0 0.1124

10.0000 0.1125

20.0000 0.1127

30.0000 0.1138

40.0000 0.1176

50.0000 0.1333

60.0000 0.2000

70.0000 0.4472

80.0000 1.0415

90.0000 1.5000

</Medium_a1>

<High_a1 a1 ="6" scale="0.5">

0 0.1124

10.0000 0.1125

20.0000 0.1127

30.0000 0.1138

40.0000 0.1176

50.0000 0.1333

60.0000 0.2000

70.0000 0.4472

80.0000 1.0415

90.0000 1.5000

</High_a1>

</MainRotorInplanewash>

<LiftDueToAoA scale="0.1">

-180.0000 -0.0001

-170.0000 0.4658

-160.0000 0.9087

-150.0000 2.7566

-140.0000 4.1489

-130.0000 4.9260

-120.0000 4.9619

-110.0000 3.3846

-100.0000 1.7154

-90.0000 -0.0005

-80.0000 -1.7144

-70.0000 -3.3820

-60.0000 -4.9578

-50.0000 -4.9208

-40.0000 -4.1432

-30.0000 -2.7511

-20.0000 -0.5829

-18.0000 -0.5107

-16.0000 -0.4336

-14.0000 -0.3544

-12.0000 -0.2757

-10.0000 -0.1996

-8.0000 -0.1278

-6.0000 -0.0620

-4.0000 -0.0034

-2.0000 0.0474

0 0.0898

2.0000 0.1237

4.0000 0.1492

6.0000 0.1671

8.0000 0.1781

10.0000 0.1835

12.0000 0.1848

14.0000 0.1839

16.0000 0.1829

18.0000 0.1843

20.0000 0.1907

30.0000 -0.0001

40.0000 0.4658

50.0000 0.9087

60.0000 2.7566

70.0000 4.1489

80.0000 4.9260

90.0000 4.9619

100.0000 3.3846

110.0000 1.7154

120.0000 -0.0005

130.0000 -1.7144

140.0000 -3.3820

150.0000 -4.9578

160.0000 -4.9208

170.0000 -4.1432

180.0000 -2.7511

</LiftDueToAoA>

<SideForceDueToSideslip scale="0.1">

-180.0000 0

-171.4977 0.3326

-154.4931 0.8516

-130.4378 1.4803

-100.5760 1.9598

-79.4240 2.0621

-63.6636 2.0724

-48.7327 2.0314

-30.4839 1.7361

-20.0000 1.3702

-18.0000 1.2471

-16.0000 1.1193

-14.0000 0.9873

-12.0000 0.8515

-10.0000 0.7125

-8.0000 0.5708

-6.0000 0.4269

-4.0000 0.2815

-2.0000 0.1349

0 -0.0121

2.0000 -0.1592

4.0000 -0.3057

6.0000 -0.4511

8.0000 -0.5949

10.0000 -0.7365

12.0000 -0.8755

14.0000 -1.0111

16.0000 -1.1431

18.0000 -1.2708

20.0000 -1.3937

30.4839 -1.7361

48.7327 -2.0314

63.6636 -2.0724

79.4240 -2.0621

100.5760 -1.9598

130.4378 -1.4803

154.4931 -0.8516

171.4977 -0.3326

180.0000 0

</SideForceDueToSideslip>

<DragDueToAoA scale="0.1">

-180.0000 0.8000

-170.0000 0.8133

-160.0000 1.0119

-150.0000 2.2253

-140.0000 4.0787

-130.0000 6.4404

-120.0000 9.1441

-110.0000 9.8355

-100.0000 10.2580

-90.0000 10.4000

-80.0000 10.2581

-70.0000 9.8365

-60.0000 9.1465

-50.0000 6.4448

-40.0000 4.0856

-30.0000 2.2349

-20.0000 1.3727

-18.0000 1.2424

-16.0000 1.1396

-14.0000 1.0621

-12.0000 1.0077

-10.0000 0.9740

-8.0000 0.9582

-6.0000 0.9578

-4.0000 0.9700

-2.0000 0.9918

0 1.0203

2.0000 1.0528

4.0000 1.0862

6.0000 1.1179

8.0000 1.1450

10.0000 1.1650

12.0000 1.1754

14.0000 1.1739

16.0000 1.1583

18.0000 1.1268

20.0000 1.0776

30.0000 0.8000

40.0000 0.8133

50.0000 1.0119

60.0000 2.2253

70.0000 4.0787

80.0000 6.4404

90.0000 9.1441

100.0000 9.8355

110.0000 10.2580

120.0000 10.4000

130.0000 10.2581

140.0000 9.8365

150.0000 9.1465

160.0000 6.4448

170.0000 4.0856

180.0000 2.2349

</DragDueToAoA>

<PitchingMomentDueToAoA scale="0.1" >

-180.0000 -7.9390

-170.7661 -7.7714

-162.7016 -6.7996

-158.2661 -5.7272

-138.5081 6.8733

-130.4435 10.3251

-126.0081 11.0958

-118.7500 11.5315

-109.4758 11.7661

-99.7984 11.5315

-94.5565 10.8613

-65.5242 -6.6655

-60.0000 -7.7275

-51.8145 -8.2071

-39.7177 -8.3412

-30.8468 -8.1401

-20.0000 -7.7275

-18.0000 -7.3963

-16.0000 -7.0066

-14.0000 -6.5610

-12.0000 -6.0621

-10.0000 -5.5124

-8.0000 -4.9147

-6.0000 -4.2714

-4.0000 -3.5852

-2.0000 -2.8587

0 -2.0944

2.0000 -1.2951

4.0000 -0.4632

6.0000 0.3986

8.0000 1.2877

10.0000 2.2016

12.0000 3.1376

14.0000 4.0931

16.0000 5.0655

18.0000 6.0522

20.0000 7.0507

23.9919 8.5824

31.2500 9.8559

42.9435 11.0958

56.2500 11.4645

70.7661 11.6320

85.2823 11.5650

102.6210 11.0288

116.7339 9.8224

126.8145 7.9792

141.3306 4.4269

150.6048 1.3773

157.8629 -1.3036

163.1048 -3.6830

168.7500 -6.5650

172.3790 -7.6709

180.0000 -7.9390

</PitchingMomentDueToAoA>

<YawingMomentDueToSideslip scale="0.1" >

-180.0000 0

-170.0000 -4.0856

-159.9496 -6.8499

-145.2520 -9.5845

-133.8206 -9.8794

-123.1149 -9.6113

-111.8649 -7.9491

-100.2520 -4.8291

-88.9631 -1.1184

-78.5945 2.1930

-66.5668 5.0658

-53.8004 7.5302

-45.0907 8.9779

-38.7788 9.1447

-32.1429 8.7500

-25.5069 7.5029

-20.0000 6.1514

-18.0000 5.5362

-16.0000 4.9211

-14.0000 4.3060

-12.0000 3.6908

-10.0000 3.0757

-8.0000 2.4606

-6.0000 1.8454

-4.0000 1.2303

-2.0000 0.6151

0 0

2.0000 -0.6151

4.0000 -1.2303

6.0000 -1.8454

8.0000 -2.4606

10.0000 -3.0757

12.0000 -3.6908

14.0000 -4.3060

16.0000 -4.9211

18.0000 -5.5362

20.0000 -6.1514

25.5069 -7.5029

32.1429 -8.7500

38.7788 -9.1447

45.0907 -8.9779

53.8004 -7.5302

66.5668 -5.0658

78.5945 -2.1930

88.9631 1.1184

100.2520 4.8291

111.8649 7.9491

123.1149 9.6113

133.8206 9.8794

145.2520 9.5845

159.9496 6.8499

170.0000 4.0856

180.0000 0

</YawingMomentDueToSideslip>

</Fuselage>

<Engines>

<Engine type="ConstantRPMEngine">

<DebugInfo printDebugInfo="false" />

<General inertia="5" />

<Performance maxPower="270" maxTorque="1000" rotationResistance="0.000009"/>

<ControllerParams P="0.5" I="1.5" D="0.0" offset="150" targetRPM="5000" />

</Engine>

</Engines>

<DriveTrains>

<DriveTrain type="GenericDriveTrain">

<GearBox gearRatios="1" reverseGearRatio="1" />

<Clutch maxClutchTorque="5000" />

<Engine index="0" />

<Load name="MainRotor" gearRatio="10.7" />

<Load name="TailRotor" gearRatio="1.739" />

</DriveTrain>

</DriveTrains>

<ControlSystem>

<FCSComponent type="FCSAutoHoverTOH">

<YawController P="0.0" D="0"/>

<PitchController P="0.15" D="0.05"/>

<RollController P="0.15" D="0.05"/>

</FCSComponent>

<FCSComponent type="FCSHelicopterAutoTrim100" >

<YawRateAndSideslipController printDebugInfo="false">

<YawRatePID P="0.18" I="0.02" D="0.0" offset="0.0" integralMin="-50" integralMax="50" />

<SideslipPID P="0.1" I="0.02" D="0.002" offset="0.0" integralMin="-50" integralMax="50" />

<Transition speedLow="10" speedHigh="20" />

<Maximums maxYawRate="30" maxSideslip="30" />

<InputMapping nonlinearity="1" />

</YawRateAndSideslipController>

<PitchRateController printDebugInfo="false">

<PID P="0.02" I="0.04" D="0.001" offset="0.0" integralMin="-25" integralMax="25" />

<MaxPitchRate maxPitchRate="35" />

<InputMapping nonlinearity="1.5" />

</PitchRateController>

<RollRateController printDebugInfo="false">

<PID P="0.02" I="0.04" D="0.001" offset="0.0" integralMin="-25" integralMax="25" />

<MaxRollRate maxRollRate="70" />

<InputMapping nonlinearity="1.5" />

</RollRateController>

</FCSComponent>

<FCSComponent type="FCSRotationDamper">

<YawController P="1" D="0"/>

<PitchController P="1.0" D="0"/>

<RollController P="0.2" D="0.00"/>

</FCSComponent>

</ControlSystem>

<Rotors>

<Rotor type="FGRotorBladeElementTheory">

<ModelConfiguration updateSubstepCount="360" />

<InfoPrint printControlInputs="false" printFlappingInfo="false" printOmega="false" />

<Geometry>

<Position x="0.0" y="0.260" z="0.8720" />

<Tilt lateralTilt="0.0" longitudinalTilt="0" />

<Blades radius="4.165" chord="0.171" count="5" hingeOffset="0.128" flappingHingeLowerLimit="-5" flappingHingeHigherLimit="10" />

<Rotation clockwise="false" />

</Geometry>

<MechanicalFeatures Ir="355" Ib="71" maxBrakeTorque="500" />

<AerodynamicFeatures>

<DesignRPM rpm="467"/>

<Blades twist="-9">

<LiftCoefficient>

0 0.4 0.6 0.8 1.0 5.0

-180 0.0 0.0 0.0 0.0 0.0 0.0

-176 0.5133 0.5133 0.5133 0.5133 0.5133 0.5133

-168 0.725 0.725 0.725 0.725 0.725 0.725

-160 0.665 0.665 0.665 0.665 0.665 0.665

-152 0.875 0.875 0.875 0.875 0.875 0.875

-144 0.8525 0.8525 0.8525 0.8525 0.8525 0.8525

-136 0.7225 0.7225 0.7225 0.7225 0.7225 0.7225

-128 0.5925 0.5925 0.5925 0.5925 0.5925 0.5925

-120 0.4625 0.4625 0.4625 0.4625 0.4625 0.4625

-112 0.3325 0.3325 0.3325 0.3325 0.3325 0.3325

-104 0.2025 0.2025 0.2025 0.2025 0.2025 0.2025

-96 0.0725 0.0725 0.0725 0.0725 0.0725 0.0725

-88 -0.0575 -0.0575 -0.0575 -0.0575 -0.0575 -0.0575

-80 -0.1875 -0.1875 -0.1875 -0.1875 -0.1875 -0.1875

-72 -0.3175 -0.3175 -0.3175 -0.3175 -0.3175 -0.3175

-64 -0.4475 -0.4475 -0.4475 -0.4475 -0.4475 -0.4475

-56 -0.5775 -0.5775 -0.5775 -0.5775 -0.5775 -0.5775

-48 -0.7075 -0.7075 -0.7075 -0.7075 -0.7075 -0.7075

-40 -0.8375 -0.8375 -0.8375 -0.8375 -0.8375 -0.8375

-32 -0.9675 -0.9675 -0.9675 -0.9675 -0.9675 -0.9675

-28 -0.996 -0.955 -0.946 -0.93 -0.918 -0.918

-24 -0.988 -0.962 -0.938 -0.89 -0.854 -0.854

-20 -0.98 -0.966 -0.93 -0.85 -0.79 -0.79

-16 -0.972 -0.970 -0.922 -0.81 -0.726 -0.726

-12 -0.724 -0.535 -0.66 -0.79 -0.662 -0.662

-8 -0.19 -0.3 -0.55 -0.75 -0.62 -0.62

-4 -0.45 -0.42 -0.47 -0.47 -0.425 -0.425

0 0.03 0.05 0.075 0.08 -0.05 -0.05

4 0.46 0.510 0.613 0.56 0.45 0.45

8 0.89 0.98 0.915 0.810 0.8 0.8

12 1.25 1.13 1.0 0.845 0.865 0.865

16 0.98 0.96 1.08 0.86 0.895 0.895

20 0.9856 0.9714 1.053 0.9 0.925 0.925

24 0.9912 0.9828 1.031 0.94 0.955 0.955

28 0.997 0.9942 1.01 0.98 0.985 0.985

32 0.9675 0.9675 0.9675 0.9675 0.9675 0.9675

40 0.8375 0.8375 0.8375 0.8375 0.8375 0.8375

48 0.7075 0.7075 0.7075 0.7075 0.7075 0.7075

56 0.5775 0.5775 0.5775 0.5775 0.5775 0.5775

64 0.4475 0.4475 0.4475 0.4475 0.4475 0.4475

72 0.3175 0.3175 0.3175 0.3175 0.3175 0.3175

80 0.1875 0.1875 0.1875 0.1875 0.1875 0.1875

88 0.0575 0.0575 0.0575 0.0575 0.0575 0.0575

96 -0.0725 -0.0725 -0.0725 -0.0725 -0.0725 -0.0725

104 -0.2025 -0.2025 -0.2025 -0.2025 -0.2025 -0.2025

112 -0.3325 -0.3325 -0.3325 -0.3325 -0.3325 -0.3325

120 -0.4625 -0.4625 -0.4625 -0.4625 -0.4625 -0.4625

128 -0.5925 -0.5925 -0.5925 -0.5925 -0.5925 -0.5925

136 -0.7225 -0.7225 -0.7225 -0.7225 -0.7225 -0.7225

144 -0.8525 -0.8525 -0.8525 -0.8525 -0.8525 -0.8525

152 -0.875 -0.875 -0.875 -0.875 -0.875 -0.875

160 -0.665 -0.665 -0.665 -0.665 -0.665 -0.665

168 -0.725 -0.725 -0.725 -0.725 -0.725 -0.725

176 -0.5133 -0.5133 -0.5133 -0.5133 -0.5133 -0.5133

180 0.0 0.0 0.0 0.0 0.0 0.0

</LiftCoefficient>

<DragCoefficient >

0.0 0.4 0.6 0.8 1.0 5.0

-180 0 0 0 0 0 0

-176 0.733 0.733 0.733 0.733 0.733 0.733

-168 0.995 0.995 0.995 0.995 0.995 0.995

-160 0.84 0.84 0.84 0.84 0.84 0.84

-152 0.68 0.68 0.68 0.68 0.68 0.68

-144 0.7825 0.7825 0.7825 0.7825 0.7825 0.7825

-136 0.9762 0.9762 0.9762 0.9762 0.9762 0.9762

-128 1.1712 1.1712 1.1712 1.1712 1.1712 1.1712

-120 1.3662 1.3662 1.3662 1.3662 1.3662 1.3662

-112 1.561 1.561 1.561 1.561 1.561 1.561

-104 1.76 1.76 1.76 1.76 1.76 1.76

-96 1.952 1.952 1.952 1.952 1.952 1.952

-88 2.079 2.079 2.079 2.079 2.079 2.079

-80 2.086 2.086 2.086 2.086 2.086 2.086

-72 2.005 2.005 2.005 2.005 2.005 2.005

-64 1.826 1.826 1.826 1.826 1.826 1.826

-56 1.554 1.554 1.554 1.554 1.554 1.554

-48 1.262 1.262 1.262 1.262 1.262 1.262

-40 0.9725 0.9725 0.9725 0.9725 0.9725 0.9725

-32 0.6975 0.6975 0.6975 0.6975 0.6975 0.6975

-28 0.562 0.57 0.578 0.593 0.601 0.601

-24 0.417 0.448 0.469 0.52 0.543 0.543

-20 0.267 0.33 0.361 0.44 0.486 0.486

-16 0.12 0.208 0.285 0.364 0.428 0.428

-12 0.018 0.022 0.191 0.29 0.37 0.37

-8 0.008 0.009 0.07 0.16 0.248 0.248

-4 0.0075 0.008 0.0125 0.065 0.152 0.152

0 0.0075 0.008 0.008 0.017 0.09 0.09

4 0.0085 0.0085 0.011 0.09 0.1525 0.1525

8 0.011 0.014 0.073 0.17 0.249 0.249

12 0.026 0.098 0.179 0.285 0.37 0.37

16 0.23 0.23 0.283 0.361 0.428 0.428

20 0.345 0.345 0.358 0.435 0.486 0.486

24 0.455 0.455 0.467 0.508 0.543 0.543

28 0.56 0.56 0.576 0.583 0.601 0.601

32 0.6975 0.6975 0.6975 0.6975 0.6975 0.6975

40 0.9725 0.9725 0.9725 0.9725 0.9725 0.9725

48 1.2625 1.2625 1.2625 1.2625 1.2625 1.2625

56 1.554 1.554 1.554 1.554 1.554 1.554

64 1.826 1.826 1.826 1.826 1.826 1.826

72 2.005 2.005 2.005 2.005 2.005 2.005

80 2.086 2.086 2.086 2.086 2.086 2.086

88 2.079 2.079 2.079 2.079 2.079 2.079

96 1.9525 1.9525 1.9525 1.9525 1.9525 1.9525

104 1.76 1.76 1.76 1.76 1.76 1.76

112 1.5612 1.5612 1.5612 1.5612 1.5612 1.5612

120 1.366 1.366 1.366 1.366 1.366 1.366

128 1.171 1.171 1.171 1.171 1.171 1.171

136 0.976 0.976 0.976 0.976 0.976 0.976

144 0.7825 0.7825 0.7825 0.7825 0.7825 0.7825

152 0.68 0.68 0.68 0.68 0.68 0.68

160 0.84 0.84 0.84 0.84 0.84 0.84

168 0.996 0.996 0.996 0.996 0.996 0.996

176 0.733 0.733 0.733 0.733 0.733 0.733

180 0.0 0.0 0.0 0.0 0.0 0.0

</DragCoefficient>

</Blades>

<Controls A1UL="6.5" A1LL="-6.5" B1UL="13" B1LL="-13.0" thetaLL="8" thetaUL="17.3" useExtendedCollectiveRange="false" />

</AerodynamicFeatures>

</Rotor>

<Rotor type="FGRotorMomentumTheory">

<Geometry>

<Position x="-0.1" y="-4.9460" z="-0.0080"/>

<Tilt lateralTilt="-90.0" longitudinalTilt="0.0" />

<Blades radius="0.71" chord="0.050" count="2" hingeOffset="0.0" />

<Delta3 angle="0" />

</Geometry>

<MechanicalFeatures Ir="0.35" Ib="0.027"/>

<AerodynamicFeatures>

<GroundEffect magnitude="0.1" />

<DesignRPM rpm="2874"/>

<Blades liftCurveSlope="0.11" zeroLiftDragCoefficient="0.007" twist="-9.4" />

<Controls A1UL="0" A1LL="0" B1UL="0" B1LL="0" thetaLL="37" thetaUL="-37" useExtendedCollectiveRange="true"/>

<Power inducedPowerCorrectionFactor="1.05" />

<DynamicPressureRatio>

<Sideslip>

-1000 0.91

-30 0.91

-25 0.80

-20 0.72

-15 0.65

-10 0.60

-5 0.58

0 0.56

5 0.58

10 0.60

15 0.65

20 0.72

25 0.80

30 0.91

1000 0.91

</Sideslip>

</DynamicPressureRatio>

<Inplanewash>

<Low_a1 a1 ="-6">

-1000 0

0 0

10 -0.17

20 0.043

30 0.26

40 0.464

50 0.69

60 0.89

70 1.12

80 1.33

90 0.69

100 0

1000 0.86

</Low_a1>

<Medium_a1 a1 ="0">

-1000 0

0 -0.34

10 -0.52

20 -0.17

30 0.10

40 0.31

50 0.52

60 0.71

70 0.91

80 1.12

90 0.57

100 0

1000 0

</Medium_a1>

<High_a1 a1 ="6">

-1000 -0.48

0 -0.48

10 -0.69

20 -0.64

30 -0.27

40 0.03

50 0.27

60 0.52

70 0.74

80 0.96

90 0.46

100 0

</High_a1>

</Inplanewash>

<Downwash>

<Low_a1 a1 ="-6">

-1000 -0.12

0 -0.12

10 0.71

20 1.60

30 1.62

40 1.66

50 1.67

60 1.67

70 1.73

80 1.50

90 1.26

100 1.01

1000 1.01

</Low_a1>

<Medium_a1 a1 ="0">

-1000 0.36

0 0.36

10 0.84

20 1.64

30 1.70

40 1.76

50 1.82

60 1.85

70 1.90

80 1.68

90 1.44

100 1.20

1000 1.20

</Medium_a1>

<High_a1 a1 ="6">

-1000 0.69

0 0.69

10 1.21

20 1.70

30 1.76

40 1.83

50 1.90

60 1.97

70 2.03

80 1.92

90 1.74

100 1.39

1000 1.39

</High_a1>

</Downwash>

</AerodynamicFeatures>

</Rotor>

</Rotors>

<StabilizersAndWings>

<HorizontalStabilizerRight>

<Geometry>

<Position x="1.8140" y="-4.9460" z="0.9800"/>

<Up x="0.0" y="0.03489" z="0.9993908"/>

<Front x="0" y="0.9993908" z="-0.03489"/>

<SurfaceArea area="0.291028"/>

</Geometry>

<ControlResponse controlSurfaceLiftCoeffDerivative="0.0" controlSurfaceForceArmPos="0.0" />

<AerodynamicFeatures>

<DynamicPressureRatio>

<AoA>

-1000 0.93

-30 0.93

-25 0.93

-20 0.88

-15 0.71

-10 0.71

-5 0.71

0 0.71

5 0.71

10 0.71

15 0.76

20 0.85

25 0.93

30 0.93

1000 0.93

</AoA>

</DynamicPressureRatio>

<MainRotorInplanewash>

<Low_a1 a1 ="-6">

-1000 0

0 0

10 -0.18

20 0.04

30 0.26

40 0.47

50 0.70

60 0.91

70 1.14

80 1.36

90 0.70

100 0

1000 0

</Low_a1>

<Medium_a1 a1 ="0">

-1000 -0.35

0 -0.35

10 -0.53

20 -0.18

30 0.11

40 0.32

50 0.53

60 0.73

70 0.93

80 1.14

90 0.58

100 0

1000 0

</Medium_a1>

<High_a1 a1 ="6">

-1000 -0.49

0 -0.49

10 -0.70

20 -0.65

30 -0.28

40 0.03

50 0.28

60 0.53

70 0.76

80 0.99

90 0.47

100 0

1000 0

</High_a1>

</MainRotorInplanewash>

<MainRotorDownwash>

<Low_a1 a1 ="-6">

-1000 -0.12

0 -0.12

10 0.74

20 1.66

30 1.67

40 1.71

50 1.73

60 1.76

70 1.78

80 1.55

90 1.30

100 1.05

1000 1.05

</Low_a1>

<Medium_a1 a1 ="0">

-1000 0.37

0 0.37

10 0.86

20 1.69

30 1.76

40 1.82

50 1.88

60 1.91

70 1.97

80 1.74

90 1.49

100 1.24

1000 1.24

</Medium_a1>

<High_a1 a1 ="6">

-1000 0.72

0 0.72

10 1.25

20 1.76

30 1.82

40 1.89

50 1.97

60 2.03

70 2.10

80 1.99

90 1.80

100 1.43

1000 1.43

</High_a1>

</MainRotorDownwash>

<GroundEffect startDistance="1.6" strength="0.0"/>

<LiftCurve>

-1000 0

-180 0

-150 0.61

-140 0.69

-130 0.69

-120 0.61

-110 0.46

-100 0.24

-90 0

-80 -0.24

-70 -0.46

-60 -0.61

-50 -0.69

-40 -0.69

-30 -0.61

0 0

30 0.61

40 0.69

50 0.69

60 0.61

70 0.46

80 0.24

90 0

100 -0.24

110 -0.46

120 -0.61

130 -0.69

140 -0.69

150 -0.61

180 0

1000 0

</LiftCurve>

<DragCurve >

-1000 0.0

-180 0.0

-140 0.42

-130 0.56

-120 0.71

-110 0.84

-100 0.93

-90 0.96

-80 0.93

-70 0.84

-60 0.71

-50 0.56

-40 0.42

0 0.008

40 0.42

50 0.56

60 0.71

70 0.84

80 0.93

90 0.96

100 0.93

110 0.84

120 0.71

130 0.56

140 0.42

180 0.0

1000 0.0

</DragCurve>

</AerodynamicFeatures>

</HorizontalStabilizerRight>

<HorizontalStabilizerLeft copy="HorizontalStabilizerRight">

<Geometry>

<Position x="-1.8140" />

</Geometry>

</HorizontalStabilizerLeft>

<VerticalStabilizer>

<Geometry>

<Position x="0" y="-4.778" z="0.1340"/>

<Up x="-1.0" y="0.0" z="0"/>

<Front x="0" y="1.0" z="0"/>

<SurfaceArea area="0.59"/>

</Geometry>

<ControlResponse controlSurfaceLiftCoeffDerivative="0.0" controlSurfaceForceArmPos="0.0" />

<AerodynamicFeatures>

<DynamicPressureRatio>

<Sideslip>

-1000 0.95

-30 0.95

-25 0.84

-20 0.75

-15 0.68

-10 0.63

-5 0.61

0 0.59

5 0.61

10 0.63

15 0.68

20 0.75

25 0.84

30 0.95

1000 0.95

</Sideslip>

</DynamicPressureRatio>

<MainRotorInplanewash>

<Low_a1 a1 ="-6">

-1000 0

0 0

10 -0.18

20 0.04

30 0.27

40 0.49

50 0.73

60 0.95

70 1.18

80 1.41

90 0.73

100 0

1000 0

</Low_a1>

<Medium_a1 a1 ="0">

-1000 -0.36

0 -0.36

10 -0.55

20 -0.18

30 0.11

40 0.33

50 0.55

60 0.75

70 0.96

80 1.18

90 0.60

100 0

</Medium_a1>

<High_a1 a1 ="6">

-1000 -0.51

0 -0.51

10 -0.73

20 -0.67

30 -0.29

40 0.04

50 0.29

60 0.55

70 0.78

80 1.02

90 0.49

100 0

1000 0

</High_a1>

</MainRotorInplanewash>

<MainRotorDownwash>

<Low_a1 a1 ="-6">

-1000 -0.12

0 -0.12

10 0.74

20 1.67

30 1.69

40 1.73

50 1.75

60 1.78

70 1.80

80 1.57

90 1.32

100 1.06

1000 1.06

</Low_a1>

<Medium_a1 a1 ="0">

-1000 0.37

0 0.37

10 0.87

20 1.71

30 1.78

40 1.84

50 1.90

60 1.93

70 1.99

80 1.76

90 1.51

100 1.26

1000 1.26

</Medium_a1>

<High_a1 a1 ="6">

-1000 0.72

0 0.72

10 1.26

20 1.78

30 1.84

40 1.92

50 1.99

60 2.05

70 2.12

80 2.01

90 1.82

100 1.45

1000 1.45

</High_a1>

</MainRotorDownwash>

<GroundEffect startDistance="0" strength="0.0"/>

<LiftCurve >

-180 0

-170 0.34

-160 0.74

-150 0.80

-140 0.72

-130 0.57

-120 0.43

-110 0.29

-100 0.15

-90 0

-80 -0.15

-70 -0.29

-60 -0.43

-50 -0.57

-40 -0.72

-30 -0.80

-25 -0.80

-20 -0.74

0 0

20 0.74

25 0.80

30 0.80

40 0.72

50 0.57

60 0.43

70 0.29

80 0.15

90 0

100 -0.15

110 -0.29

120 -0.43

130 -0.57

140 -0.72

150 -0.80

160 -0.74

170 -0.34

180 0

</LiftCurve>

<DragCurve>

-1000 0.0

-180 0.0

-140 0.42

-130 0.56

-120 0.71

-110 0.84

-100 0.93

-90 0.96

-80 0.93

-70 0.84

-60 0.71

-50 0.56

-40 0.42

0 0.008

40 0.42

50 0.56

60 0.71

70 0.84

80 0.93

90 0.96

100 0.93

110 0.84

120 0.71

130 0.56

140 0.42

180 0.0

1000 0.0

</DragCurve>

</AerodynamicFeatures>

</VerticalStabilizer>

</StabilizersAndWings>

<GroundContacts>

<GeneralConfiguration gearExtensionTime="3" gearDragCoefficient="0" gearReferenceArea="0"

maxSteerableGearDeflection="80" steerableGearSpeedCorrectionFactor="0.0"/>

<GroundContact type="FGGroundContact200" >

<Features isBrakable="false" isRetractable="false" isSteerable="false" />

<Aerodynamics equivalentFlatPlateArea ="0.0" />

<Suspension>

<MountStation x="-1.052" y="1.6933" z="-1.6717"/>

<SliderAxis x="0" y="0" z="1" />

<SuspensionLength length="0.2" />

<SpringParameters springConstant="420000" damperConstant="50000" maxCompression="0.18" />

</Suspension>

<Wheel mass="1" radius="0.1" >

<RollAxis x="1" y="0" z="0" />

<Friction slidingFriction="0.8" resistanceTorqueNoBrake="1000" resistanceTorqueFullBrake="1000" />

</Wheel>

<Damage thresholdLoad="20000000" />

</GroundContact>

<GroundContact type="FGGroundContact200" >

<Features isBrakable="false" isRetractable="false" isSteerable="false" />

<Aerodynamics equivalentFlatPlateArea ="0.0" />

<Suspension>

<MountStation x="1.052" y="1.6933" z="-1.6717"/>

<SliderAxis x="0" y="0" z="1" />

<SuspensionLength length="0.2" />

<SpringParameters springConstant="420000" damperConstant="50000" maxCompression="0.18" />

</Suspension>

<Wheel mass="1" radius="0.1" >

<RollAxis x="1" y="0" z="0" />

<Friction slidingFriction="0.8" resistanceTorqueNoBrake="1000" resistanceTorqueFullBrake="1000" />

</Wheel>

<Damage thresholdLoad="20000000" />

</GroundContact>

<GroundContact type="FGGroundContact200" >

<Features isBrakable="false" isRetractable="false" isSteerable="false" />

<Aerodynamics equivalentFlatPlateArea ="0.0" />

<Suspension>

<MountStation x="0.944" y="-0.6387" z="-1.5650"/>

<SliderAxis x="0" y="0" z="1" />

<SuspensionLength length="0.2" />

<SpringParameters springConstant="420000" damperConstant="50000" maxCompression="0.18" />

</Suspension>

<Wheel mass="1" radius="0.1" >

<RollAxis x="1" y="0" z="0" />

<Friction slidingFriction="0.8" resistanceTorqueNoBrake="1000" resistanceTorqueFullBrake="1000" />

</Wheel>

<Damage thresholdLoad="20000000" />

</GroundContact>

<GroundContact type="FGGroundContact200" >

<Features isBrakable="false" isRetractable="false" isSteerable="false" />

<Aerodynamics equivalentFlatPlateArea ="0.0" />

<Suspension>

<MountStation x="-0.944" y="-0.6387" z="-1.5650"/>

<SliderAxis x="0" y="0" z="1" />

<SuspensionLength length="0.2" />

<SpringParameters springConstant="420000" damperConstant="50000" maxCompression="0.18" />

</Suspension>

<Wheel mass="1" radius="0.1" >

<RollAxis x="1" y="0" z="0" />

<Friction slidingFriction="0.8" resistanceTorqueNoBrake="1000" resistanceTorqueFullBrake="1000" />

</Wheel>

<Damage thresholdLoad="20000000" />

</GroundContact>

<GroundContact type="FGGroundContact200" >

<Features isBrakable="false" isRetractable="false" isSteerable="false" />

<Aerodynamics equivalentFlatPlateArea ="0.0" />

<Suspension>

<MountStation x="0" y="-4.341" z="-0.65"/>

<SliderAxis x="0" y="0" z="1" />

<SuspensionLength length="0" />

<SpringParameters springConstant="420000" damperConstant="50000" maxCompression="0" />

</Suspension>

<Wheel mass="0.1" radius="0.1" >

<RollAxis x="1" y="0" z="0" />

<Friction slidingFriction="0.8" resistanceTorqueNoBrake="1000" resistanceTorqueFullBrake="1000" />

</Wheel>

<Damage thresholdLoad="20000000" />

</GroundContact>

</GroundContacts>

</GenHeli600>

Edited by Foxhound
Please put long configs etc like this between spoiler tags preventing the topic from becoming a mile long.

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many thanks ;) i can edit this file but eliteness dont let me reconvert the pbo file just show the message "No sqm or config detected pbo" when i try to convert the folder air_us_h :(

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Hmm I'm not sure, I haven't tried to create a pbo yet, I've only extracted them. Have you tried any of the other PBO tools?

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I used the eliteness and I think I had to download a depbo.dll and stick in the same folder as eliteness. With eliteness, you will get errors if you don't run the exe as administrator in Windows 7. I got the files on one of those overly complicated dev-heaven sites where you have to read the page 4 times over to find the DL link.

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i tried with pboview but no extract nothing just say "no arma pbo", i find collective maximum and minimum values, the minimum value is to high 8 degrees this is the reason this one is almost unable to auto rotate and no decent faster when the collective is in full down position, normal values in a real helicopter are around zero o even negatives values in asymmetrical foil blades but in the other hand if with 8 degrees you just need add weight and this is able to auto rotate mean the rotors flight dynamics are amazing!!

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Hello,

i need repack to see the changes? i am totally new with this game thanks ;)

Yes, you need to repack the files as pbo to get them running ingame.

To repack PBO files I recommend either kegeteys CPBO (scroll down to the section ArmA tools), which actually is just packing all the files in a bag and gives it the filetype PBO, or the more professional one, which is by that binarizing the Configs (so recommended for a final release packing). This tool is called BinPBO and is part of the BITools2.

To extract pbo´s I recommend Micero´s ExtractPbp application, to find on dev-heaven.net You´ll find a detailed information about how extract them by following this link. Just scroll down to the option: Extract BI addons to P: .

Good luck

Edited by MemphisBelle

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this appears to be lift vs angle of attack but why in columns? what mean this columns? 0, 0.4, 0.6.... :rolleyes:reynolds number:confused:

<AerodynamicFeatures>

<DesignRPM rpm="467"/>

<Blades twist="-9">

<LiftCoefficient>

0 0.4 0.6 0.8 1.0 5.0

-180 0.0 0.0 0.0 0.0 0.0 0.0

-176 0.5133 0.5133 0.5133 0.5133 0.5133 0.5133

-168 0.725 0.725 0.725 0.725 0.725 0.725

-160 0.665 0.665 0.665 0.665 0.665 0.665

-152 0.875 0.875 0.875 0.875 0.875 0.875

-144 0.8525 0.8525 0.8525 0.8525 0.8525 0.8525

-136 0.7225 0.7225 0.7225 0.7225 0.7225 0.7225

-128 0.5925 0.5925 0.5925 0.5925 0.5925 0.5925

-120 0.4625 0.4625 0.4625 0.4625 0.4625 0.4625

-112 0.3325 0.3325 0.3325 0.3325 0.3325 0.3325

-104 0.2025 0.2025 0.2025 0.2025 0.2025 0.2025

-96 0.0725 0.0725 0.0725 0.0725 0.0725 0.0725

-88 -0.0575 -0.0575 -0.0575 -0.0575 -0.0575 -0.0575

-80 -0.1875 -0.1875 -0.1875 -0.1875 -0.1875 -0.1875

-72 -0.3175 -0.3175 -0.3175 -0.3175 -0.3175 -0.3175

-64 -0.4475 -0.4475 -0.4475 -0.4475 -0.4475 -0.4475

-56 -0.5775 -0.5775 -0.5775 -0.5775 -0.5775 -0.5775

-48 -0.7075 -0.7075 -0.7075 -0.7075 -0.7075 -0.7075

-40 -0.8375 -0.8375 -0.8375 -0.8375 -0.8375 -0.8375

-32 -0.9675 -0.9675 -0.9675 -0.9675 -0.9675 -0.9675

-28 -0.996 -0.955 -0.946 -0.93 -0.918 -0.918

-24 -0.988 -0.962 -0.938 -0.89 -0.854 -0.854

-20 -0.98 -0.966 -0.93 -0.85 -0.79 -0.79

-16 -0.972 -0.970 -0.922 -0.81 -0.726 -0.726

-12 -0.724 -0.535 -0.66 -0.79 -0.662 -0.662

-8 -0.19 -0.3 -0.55 -0.75 -0.62 -0.62

-4 -0.45 -0.42 -0.47 -0.47 -0.425 -0.425

0 0.03 0.05 0.075 0.08 -0.05 -0.05

4 0.46 0.510 0.613 0.56 0.45 0.45

8 0.89 0.98 0.915 0.810 0.8 0.8

12 1.25 1.13 1.0 0.845 0.865 0.865

16 0.98 0.96 1.08 0.86 0.895 0.895

20 0.9856 0.9714 1.053 0.9 0.925 0.925

24 0.9912 0.9828 1.031 0.94 0.955 0.955

28 0.997 0.9942 1.01 0.98 0.985 0.985

32 0.9675 0.9675 0.9675 0.9675 0.9675 0.9675

40 0.8375 0.8375 0.8375 0.8375 0.8375 0.8375

48 0.7075 0.7075 0.7075 0.7075 0.7075 0.7075

56 0.5775 0.5775 0.5775 0.5775 0.5775 0.5775

64 0.4475 0.4475 0.4475 0.4475 0.4475 0.4475

72 0.3175 0.3175 0.3175 0.3175 0.3175 0.3175

80 0.1875 0.1875 0.1875 0.1875 0.1875 0.1875

88 0.0575 0.0575 0.0575 0.0575 0.0575 0.0575

96 -0.0725 -0.0725 -0.0725 -0.0725 -0.0725 -0.0725

104 -0.2025 -0.2025 -0.2025 -0.2025 -0.2025 -0.2025

112 -0.3325 -0.3325 -0.3325 -0.3325 -0.3325 -0.3325

120 -0.4625 -0.4625 -0.4625 -0.4625 -0.4625 -0.4625

128 -0.5925 -0.5925 -0.5925 -0.5925 -0.5925 -0.5925

136 -0.7225 -0.7225 -0.7225 -0.7225 -0.7225 -0.7225

144 -0.8525 -0.8525 -0.8525 -0.8525 -0.8525 -0.8525

152 -0.875 -0.875 -0.875 -0.875 -0.875 -0.875

160 -0.665 -0.665 -0.665 -0.665 -0.665 -0.665

168 -0.725 -0.725 -0.725 -0.725 -0.725 -0.725

176 -0.5133 -0.5133 -0.5133 -0.5133 -0.5133 -0.5133

180 0.0 0.0 0.0 0.0 0.0 0.0

Edited by heli_flying

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I have something that might help real pilots to disable what they probably call "lag on joystick". As there is actualy no real pilot available in BI, pls try this and provide your feedback:

Remove or replace such entry in your testing XML.

If my findings are good, this should remove all stability agumentation build in RLib:

<FCSComponent type="FCSRotationDamper">

<YawController P="0" D="0"/>

<PitchController P="0" D="0"/>

<RollController P="0" D="0"/>

</FCSComponent>

From my personal tests, values for this "Damper" do slow responses simillar way as stability agumentation slider in X-Plane or stability "autopilot" chanels in Black Shark.

Edited by Armored_Sheep

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Anyone who want to test settings with removed FCSRotationDamper values can try thise XML file. Just unpack it in your TKOH folder on root next to the exe.

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what is the difference with Light-GenHeli600-DesktopSim.xml and Light-GenHeli400-DesktopSim.xml ?

is that armed and unarmed heli ?

Just unpack it in your TKOH folder on root next to the exe.

oh? so am I to understand that placing this addon in the root folder overrides the data in the Addons folder? that would help play testing changes and reduce the chance of corrupting the original addon.

Edited by [DirTyDeeDs]-Ziggy-

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-Ziggy-;2054788']what is the difference with Light-GenHeli600-DesktopSim.xml and Light-GenHeli400-DesktopSim.xml ?

400 is training helicopter that has less powerfull engine

-Ziggy-;2054788'] placing this addon in the root folder overrides the data in the Addons folder?

yes, exactly

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Attached complete pack of XML files for all helicopters.

Dampeners at least for yaw control cannot be set to 0 as it brakes autotrim.

More investigation is needed at the controlers part of the XML.

Edited by Armored_Sheep

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I noticed that with this change and auto-trim on (in the light heli), it takes a few seconds for auto-trim to kick-in. You get about 4-5 seconds of occillation before it bites.

Other than that, I need to test a bit more to see if handling is affected - unfortunately I have a big problem controlling my heli without auto trim on and I guess the biggest benefit of the change is in that mode.

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i think this one can do the job for the light in expert without auto trim but push your left pedal starting in freeflight mode!!

REFERENCES

[1] Technical Description.pdf

[2] Wikipedia

[3] Field manual

[4] Technical manual

[5] Blueprints

-->

<?xml version="1.0"?>

<GenHeli600 version="1.0">

<!-- Estimation

Calculated after the ration R_mass = (empty weight of dauphin) / (empty weight of MD500) ratio = (2271)/(722) = 3.1454293629.

Ixx = 11000/R_Mass = 3497

Iyy = 2704/R_Mass = 859

Ixx = 9900/R_Mass = 3147

-->

<MomentsOfInertia Ixx="3497" Iyy="859" Izz="3147"/>

<!--[2]

Empty Weight=722 kg

Max Takeoff Weight=1610 kg

Any value between empty weight and max takeoff weight is valid.

-->

<Mass mass="722"/>

<Fuselage rotationalResistance="100" >

<MainRotorDownwash scale="0.5">

<Low_a1 a1 ="-6">

0 1.4958

10.0000 1.4955

20.0000 1.4939

30.0000 1.4881

40.0000 1.4694

50.0000 1.4149

60.0000 1.2801

70.0000 1.0072

80.0000 0.5652

90.0000 0.0000

</Low_a1>

<Medium_a1 a1 ="0" scale="0.5">

0 1.4958

10.0000 1.4955

20.0000 1.4939

30.0000 1.4881

40.0000 1.4694

50.0000 1.4149

60.0000 1.2801

70.0000 1.0072

80.0000 0.5652

90.0000 0.0000

</Medium_a1>

<High_a1 a1 ="6" scale="0.5">

0 1.4958

10.0000 1.4955

20.0000 1.4939

30.0000 1.4881

40.0000 1.4694

50.0000 1.4149

60.0000 1.2801

70.0000 1.0072

80.0000 0.5652

90.0000 0.0000

</High_a1>

</MainRotorDownwash>

<MainRotorInplanewash scale="0.5">

<Low_a1 a1 ="-6">

0 0.1124

10.0000 0.1125

20.0000 0.1127

30.0000 0.1138

40.0000 0.1176

50.0000 0.1333

60.0000 0.2000

70.0000 0.4472

80.0000 1.0415

90.0000 1.5000

</Low_a1>

<Medium_a1 a1 ="0" scale="0.5">

0 0.1124

10.0000 0.1125

20.0000 0.1127

30.0000 0.1138

40.0000 0.1176

50.0000 0.1333

60.0000 0.2000

70.0000 0.4472

80.0000 1.0415

90.0000 1.5000

</Medium_a1>

<High_a1 a1 ="6" scale="0.5">

0 0.1124

10.0000 0.1125

20.0000 0.1127

30.0000 0.1138

40.0000 0.1176

50.0000 0.1333

60.0000 0.2000

70.0000 0.4472

80.0000 1.0415

90.0000 1.5000

</High_a1>

</MainRotorInplanewash>

<LiftDueToAoA scale="0.1">

-180.0000 -0.0001

-170.0000 0.4658

-160.0000 0.9087

-150.0000 2.7566

-140.0000 4.1489

-130.0000 4.9260

-120.0000 4.9619

-110.0000 3.3846

-100.0000 1.7154

-90.0000 -0.0005

-80.0000 -1.7144

-70.0000 -3.3820

-60.0000 -4.9578

-50.0000 -4.9208

-40.0000 -4.1432

-30.0000 -2.7511

-20.0000 -0.5829

-18.0000 -0.5107

-16.0000 -0.4336

-14.0000 -0.3544

-12.0000 -0.2757

-10.0000 -0.1996

-8.0000 -0.1278

-6.0000 -0.0620

-4.0000 -0.0034

-2.0000 0.0474

0 0.0898

2.0000 0.1237

4.0000 0.1492

6.0000 0.1671

8.0000 0.1781

10.0000 0.1835

12.0000 0.1848

14.0000 0.1839

16.0000 0.1829

18.0000 0.1843

20.0000 0.1907

30.0000 -0.0001

40.0000 0.4658

50.0000 0.9087

60.0000 2.7566

70.0000 4.1489

80.0000 4.9260

90.0000 4.9619

100.0000 3.3846

110.0000 1.7154

120.0000 -0.0005

130.0000 -1.7144

140.0000 -3.3820

150.0000 -4.9578

160.0000 -4.9208

170.0000 -4.1432

180.0000 -2.7511

</LiftDueToAoA>

<SideForceDueToSideslip scale="0.1">

-180.0000 0

-171.4977 0.3326

-154.4931 0.8516

-130.4378 1.4803

-100.5760 1.9598

-79.4240 2.0621

-63.6636 2.0724

-48.7327 2.0314

-30.4839 1.7361

-20.0000 1.3702

-18.0000 1.2471

-16.0000 1.1193

-14.0000 0.9873

-12.0000 0.8515

-10.0000 0.7125

-8.0000 0.5708

-6.0000 0.4269

-4.0000 0.2815

-2.0000 0.1349

0 -0.0121

2.0000 -0.1592

4.0000 -0.3057

6.0000 -0.4511

8.0000 -0.5949

10.0000 -0.7365

12.0000 -0.8755

14.0000 -1.0111

16.0000 -1.1431

18.0000 -1.2708

20.0000 -1.3937

30.4839 -1.7361

48.7327 -2.0314

63.6636 -2.0724

79.4240 -2.0621

100.5760 -1.9598

130.4378 -1.4803

154.4931 -0.8516

171.4977 -0.3326

180.0000 0

</SideForceDueToSideslip>

<DragDueToAoA scale="0.1">

-180.0000 0.8000

-170.0000 0.8133

-160.0000 1.0119

-150.0000 2.2253

-140.0000 4.0787

-130.0000 6.4404

-120.0000 9.1441

-110.0000 9.8355

-100.0000 10.2580

-90.0000 10.4000

-80.0000 10.2581

-70.0000 9.8365

-60.0000 9.1465

-50.0000 6.4448

-40.0000 4.0856

-30.0000 2.2349

-20.0000 1.3727

-18.0000 1.2424

-16.0000 1.1396

-14.0000 1.0621

-12.0000 1.0077

-10.0000 0.9740

-8.0000 0.9582

-6.0000 0.9578

-4.0000 0.9700

-2.0000 0.9918

0 1.0203

2.0000 1.0528

4.0000 1.0862

6.0000 1.1179

8.0000 1.1450

10.0000 1.1650

12.0000 1.1754

14.0000 1.1739

16.0000 1.1583

18.0000 1.1268

20.0000 1.0776

30.0000 0.8000

40.0000 0.8133

50.0000 1.0119

60.0000 2.2253

70.0000 4.0787

80.0000 6.4404

90.0000 9.1441

100.0000 9.8355

110.0000 10.2580

120.0000 10.4000

130.0000 10.2581

140.0000 9.8365

150.0000 9.1465

160.0000 6.4448

170.0000 4.0856

180.0000 2.2349

</DragDueToAoA>

<PitchingMomentDueToAoA scale="0.1" >

-180.0000 -7.9390

-170.7661 -7.7714

-162.7016 -6.7996

-158.2661 -5.7272

-138.5081 6.8733

-130.4435 10.3251

-126.0081 11.0958

-118.7500 11.5315

-109.4758 11.7661

-99.7984 11.5315

-94.5565 10.8613

-65.5242 -6.6655

-60.0000 -7.7275

-51.8145 -8.2071

-39.7177 -8.3412

-30.8468 -8.1401

-20.0000 -7.7275

-18.0000 -7.3963

-16.0000 -7.0066

-14.0000 -6.5610

-12.0000 -6.0621

-10.0000 -5.5124

-8.0000 -4.9147

-6.0000 -4.2714

-4.0000 -3.5852

-2.0000 -2.8587

0 -2.0944

2.0000 -1.2951

4.0000 -0.4632

6.0000 0.3986

8.0000 1.2877

10.0000 2.2016

12.0000 3.1376

14.0000 4.0931

16.0000 5.0655

18.0000 6.0522

20.0000 7.0507

23.9919 8.5824

31.2500 9.8559

42.9435 11.0958

56.2500 11.4645

70.7661 11.6320

85.2823 11.5650

102.6210 11.0288

116.7339 9.8224

126.8145 7.9792

141.3306 4.4269

150.6048 1.3773

157.8629 -1.3036

163.1048 -3.6830

168.7500 -6.5650

172.3790 -7.6709

180.0000 -7.9390

</PitchingMomentDueToAoA>

<YawingMomentDueToSideslip scale="0.1" >

-180.0000 0

-170.0000 -4.0856

-159.9496 -6.8499

-145.2520 -9.5845

-133.8206 -9.8794

-123.1149 -9.6113

-111.8649 -7.9491

-100.2520 -4.8291

-88.9631 -1.1184

-78.5945 2.1930

-66.5668 5.0658

-53.8004 7.5302

-45.0907 8.9779

-38.7788 9.1447

-32.1429 8.7500

-25.5069 7.5029

-20.0000 6.1514

-18.0000 5.5362

-16.0000 4.9211

-14.0000 4.3060

-12.0000 3.6908

-10.0000 3.0757

-8.0000 2.4606

-6.0000 1.8454

-4.0000 1.2303

-2.0000 0.6151

0 0

2.0000 -0.6151

4.0000 -1.2303

6.0000 -1.8454

8.0000 -2.4606

10.0000 -3.0757

12.0000 -3.6908

14.0000 -4.3060

16.0000 -4.9211

18.0000 -5.5362

20.0000 -6.1514

25.5069 -7.5029

32.1429 -8.7500

38.7788 -9.1447

45.0907 -8.9779

53.8004 -7.5302

66.5668 -5.0658

78.5945 -2.1930

88.9631 1.1184

100.2520 4.8291

111.8649 7.9491

123.1149 9.6113

133.8206 9.8794

145.2520 9.5845

159.9496 6.8499

170.0000 4.0856

180.0000 0

</YawingMomentDueToSideslip>

</Fuselage>

<Engines>

<Engine type="ConstantRPMEngine">

<DebugInfo printDebugInfo="false" />

<General inertia="6" />

<Performance maxPower="375" maxTorque="1000" rotationResistance="0.000000009"/>

<ControllerParams P="0.5" I="1.5" D="0.0" offset="150" targetRPM="5000" />

</Engine>

</Engines>

<DriveTrains>

<DriveTrain type="GenericDriveTrain">

<GearBox gearRatios="1" reverseGearRatio="1" />

<Clutch maxClutchTorque="5000" />

<Engine index="0" />

<Load name="MainRotor" gearRatio="10.0" />

<Load name="TailRotor" gearRatio="1.739" />

</DriveTrain>

</DriveTrains>

<ControlSystem>

<FCSComponent type="FCSAutoHoverTOH">

<YawController P="0.0" D="0"/>

<PitchController P="0.15" D="0.05"/>

<RollController P="0.15" D="0.05"/>

</FCSComponent>

<FCSComponent type="FCSHelicopterAutoTrim100" >

<YawRateAndSideslipController printDebugInfo="false">

<YawRatePID P="0.18" I="0.02" D="0.0" offset="0.0" integralMin="-50" integralMax="50" />

<SideslipPID P="0.1" I="0.02" D="0.002" offset="0.0" integralMin="-50" integralMax="50" />

<Transition speedLow="10" speedHigh="20" />

<Maximums maxYawRate="30" maxSideslip="30" />

<InputMapping nonlinearity="1" />

</YawRateAndSideslipController>

<PitchRateController printDebugInfo="false">

<PID P="0.02" I="0.04" D="0.001" offset="0.0" integralMin="-25" integralMax="25" />

<MaxPitchRate maxPitchRate="35" />

<InputMapping nonlinearity="1.5" />

</PitchRateController>

<RollRateController printDebugInfo="false">

<PID P="0.02" I="0.04" D="0.001" offset="0.0" integralMin="-25" integralMax="25" />

<MaxRollRate maxRollRate="70" />

<InputMapping nonlinearity="1.5" />

</RollRateController>

</FCSComponent>

<FCSComponent type="FCSRotationDamper">

<YawController P="0" D="0"/>

<PitchController P="0.0" D="0"/>

<RollController P="0.0" D="0.00"/>

</FCSComponent>

</ControlSystem>

<Rotors>

<Rotor type="FGRotorBladeElementTheory">

<ModelConfiguration updateSubstepCount="360" />

<InfoPrint printControlInputs="false" printFlappingInfo="false" printOmega="false" />

<Geometry>

<Position x="0.0" y="0.260" z="0.8720" />

<Tilt lateralTilt="0.0" longitudinalTilt="0" />

<Blades radius="4.165" chord="0.171" count="5" hingeOffset="0.128" flappingHingeLowerLimit="-2" flappingHingeHigherLimit="20" />

<Rotation clockwise="false" />

</Geometry>

<MechanicalFeatures Ir="155" Ib="220" maxBrakeTorque="500" />

<AerodynamicFeatures>

<DesignRPM rpm="503"/>

<Blades twist="-7">

<LiftCoefficient>

0 0.4 0.6 0.8 1.0 5.0

-180 0.0 0.0 0.0 0.0 0.0 0.0

-176 0.5133 0.5133 0.5133 0.5133 0.5133 0.5133

-168 0.725 0.725 0.725 0.725 0.725 0.725

-160 0.665 0.665 0.665 0.665 0.665 0.665

-152 0.875 0.875 0.875 0.875 0.875 0.875

-144 0.8525 0.8525 0.8525 0.8525 0.8525 0.8525

-136 0.7225 0.7225 0.7225 0.7225 0.7225 0.7225

-128 0.5925 0.5925 0.5925 0.5925 0.5925 0.5925

-120 0.4625 0.4625 0.4625 0.4625 0.4625 0.4625

-112 0.3325 0.3325 0.3325 0.3325 0.3325 0.3325

-104 0.2025 0.2025 0.2025 0.2025 0.2025 0.2025

-96 0.0725 0.0725 0.0725 0.0725 0.0725 0.0725

-88 -0.0575 -0.0575 -0.0575 -0.0575 -0.0575 -0.0575

-80 -0.1875 -0.1875 -0.1875 -0.1875 -0.1875 -0.1875

-72 -0.3175 -0.3175 -0.3175 -0.3175 -0.3175 -0.3175

-64 -0.4475 -0.4475 -0.4475 -0.4475 -0.4475 -0.4475

-56 -0.5775 -0.5775 -0.5775 -0.5775 -0.5775 -0.5775

-48 -0.7075 -0.7075 -0.7075 -0.7075 -0.7075 -0.7075

-40 -0.8375 -0.8375 -0.8375 -0.8375 -0.8375 -0.8375

-32 -0.9675 -0.9675 -0.9675 -0.9675 -0.9675 -0.9675

-28 -0.996 -0.955 -0.946 -0.93 -0.918 -0.918

-24 -0.988 -0.962 -0.938 -0.89 -0.854 -0.854

-20 -0.98 -0.966 -0.93 -0.85 -0.79 -0.79

-16 -0.982 -0.970 -0.922 -0.81 -0.726 -0.726

-12 -0.95 -1.235 -0.66 -0.79 -0.662 -0.662

-8 -0.89 -0.8 -0.55 -0.75 -0.62 -0.62

-4 -0.46 -0.46 -0.47 -0.47 -0.425 -0.425

0 0.00 0.05 0.075 0.08 -0.05 -0.05

4 0.46 0.510 0.613 0.56 0.45 0.45

8 0.89 0.98 0.915 0.810 0.8 0.8

12 1.25 1.23 1.0 0.845 0.865 0.865

16 0.98 0.96 1.08 0.86 0.895 0.895

20 0.9856 0.9714 1.053 0.9 0.925 0.925

24 0.9912 0.9828 1.031 0.94 0.955 0.955

28 0.997 0.9942 1.01 0.98 0.985 0.985

32 0.9675 0.9675 0.9675 0.9675 0.9675 0.9675

40 0.8375 0.8375 0.8375 0.8375 0.8375 0.8375

48 0.7075 0.7075 0.7075 0.7075 0.7075 0.7075

56 0.5775 0.5775 0.5775 0.5775 0.5775 0.5775

64 0.4475 0.4475 0.4475 0.4475 0.4475 0.4475

72 0.3175 0.3175 0.3175 0.3175 0.3175 0.3175

80 0.1875 0.1875 0.1875 0.1875 0.1875 0.1875

88 0.0575 0.0575 0.0575 0.0575 0.0575 0.0575

96 -0.0725 -0.0725 -0.0725 -0.0725 -0.0725 -0.0725

104 -0.2025 -0.2025 -0.2025 -0.2025 -0.2025 -0.2025

112 -0.3325 -0.3325 -0.3325 -0.3325 -0.3325 -0.3325

120 -0.4625 -0.4625 -0.4625 -0.4625 -0.4625 -0.4625

128 -0.5925 -0.5925 -0.5925 -0.5925 -0.5925 -0.5925

136 -0.7225 -0.7225 -0.7225 -0.7225 -0.7225 -0.7225

144 -0.8525 -0.8525 -0.8525 -0.8525 -0.8525 -0.8525

152 -0.875 -0.875 -0.875 -0.875 -0.875 -0.875

160 -0.665 -0.665 -0.665 -0.665 -0.665 -0.665

168 -0.725 -0.725 -0.725 -0.725 -0.725 -0.725

176 -0.5133 -0.5133 -0.5133 -0.5133 -0.5133 -0.5133

180 0.0 0.0 0.0 0.0 0.0 0.0

</LiftCoefficient>

<DragCoefficient >

0.0 0.4 0.6 0.8 1.0 5.0

-180 0 0 0 0 0 0

-176 0.733 0.733 0.733 0.733 0.733 0.733

-168 0.995 0.995 0.995 0.995 0.995 0.995

-160 0.84 0.84 0.84 0.84 0.84 0.84

-152 0.68 0.68 0.68 0.68 0.68 0.68

-144 0.7825 0.7825 0.7825 0.7825 0.7825 0.7825

-136 0.9762 0.9762 0.9762 0.9762 0.9762 0.9762

-128 1.1712 1.1712 1.1712 1.1712 1.1712 1.1712

-120 1.3662 1.3662 1.3662 1.3662 1.3662 1.3662

-112 1.561 1.561 1.561 1.561 1.561 1.561

-104 1.76 1.76 1.76 1.76 1.76 1.76

-96 1.952 1.952 1.952 1.952 1.952 1.952

-88 2.079 2.079 2.079 2.079 2.079 2.079

-80 2.086 2.086 2.086 2.086 2.086 2.086

-72 2.005 2.005 2.005 2.005 2.005 2.005

-64 1.826 1.826 1.826 1.826 1.826 1.826

-56 1.554 1.554 1.554 1.554 1.554 1.554

-48 1.262 1.262 1.262 1.262 1.262 1.262

-40 0.9725 0.9725 0.9725 0.9725 0.9725 0.9725

-32 0.6975 0.6975 0.6975 0.6975 0.6975 0.6975

-28 0.562 0.57 0.578 0.593 0.601 0.601

-24 0.417 0.448 0.469 0.52 0.543 0.543

-20 0.267 0.33 0.361 0.44 0.486 0.486

-16 0.12 0.208 0.285 0.364 0.428 0.428

-12 0.018 0.022 0.191 0.29 0.37 0.37

-8 0.008 0.009 0.07 0.16 0.248 0.248

-4 0.0055 0.008 0.0125 0.065 0.152 0.152

0 0.0035 0.008 0.008 0.017 0.09 0.09

4 0.0055 0.0085 0.011 0.09 0.1525 0.1525

8 0.008 0.014 0.073 0.17 0.249 0.249

12 0.018 0.028 0.179 0.285 0.37 0.37

16 0.12 0.13 0.283 0.361 0.428 0.428

20 0.265 0.345 0.358 0.435 0.486 0.486

24 0.455 0.455 0.467 0.508 0.543 0.543

28 0.56 0.56 0.576 0.583 0.601 0.601

32 0.6975 0.6975 0.6975 0.6975 0.6975 0.6975

40 0.9725 0.9725 0.9725 0.9725 0.9725 0.9725

48 1.2625 1.2625 1.2625 1.2625 1.2625 1.2625

56 1.554 1.554 1.554 1.554 1.554 1.554

64 1.826 1.826 1.826 1.826 1.826 1.826

72 2.005 2.005 2.005 2.005 2.005 2.005

80 2.086 2.086 2.086 2.086 2.086 2.086

88 2.079 2.079 2.079 2.079 2.079 2.079

96 1.9525 1.9525 1.9525 1.9525 1.9525 1.9525

104 1.76 1.76 1.76 1.76 1.76 1.76

112 1.5612 1.5612 1.5612 1.5612 1.5612 1.5612

120 1.366 1.366 1.366 1.366 1.366 1.366

128 1.171 1.171 1.171 1.171 1.171 1.171

136 0.976 0.976 0.976 0.976 0.976 0.976

144 0.7825 0.7825 0.7825 0.7825 0.7825 0.7825

152 0.68 0.68 0.68 0.68 0.68 0.68

160 0.84 0.84 0.84 0.84 0.84 0.84

168 0.996 0.996 0.996 0.996 0.996 0.996

176 0.733 0.733 0.733 0.733 0.733 0.733

180 0.0 0.0 0.0 0.0 0.0 0.0

</DragCoefficient>

</Blades>

<Controls A1UL="6.5" A1LL="-6.5" B1UL="10" B1LL="-10.0" thetaLL="4.5" thetaUL="17.3" useExtendedCollectiveRange="false" />

</AerodynamicFeatures>

</Rotor>

<Rotor type="FGRotorMomentumTheory">

<Geometry>

<Position x="-0.1" y="-4.9460" z="-0.0080"/>

<Tilt lateralTilt="-90.0" longitudinalTilt="0.0" />

<Blades radius="0.71" chord="0.050" count="2" hingeOffset="0.0" />

<Delta3 angle="0" />

</Geometry>

<MechanicalFeatures Ir="0.35" Ib="0.027"/>

<AerodynamicFeatures>

<GroundEffect magnitude="0.05" />

<DesignRPM rpm="2874"/>

<Blades liftCurveSlope="0.11" zeroLiftDragCoefficient="0.007" twist="0.0" />

<Controls A1UL="0" A1LL="0" B1UL="0" B1LL="0" thetaLL="17" thetaUL="-27" useExtendedCollectiveRange="true"/>

<Power inducedPowerCorrectionFactor="1.05" />

<DynamicPressureRatio>

<Sideslip>

-1000 0.91

-30 0.91

-25 0.80

-20 0.72

-15 0.65

-10 0.60

-5 0.58

0 0.56

5 0.58

10 0.60

15 0.65

20 0.72

25 0.80

30 0.91

1000 0.91

</Sideslip>

</DynamicPressureRatio>

<Inplanewash>

<Low_a1 a1 ="-6">

-1000 0

0 0

10 -0.17

20 0.043

30 0.26

40 0.464

50 0.69

60 0.89

70 1.12

80 1.33

90 0.69

100 0

1000 0.86

</Low_a1>

<Medium_a1 a1 ="0">

-1000 0

0 -0.34

10 -0.52

20 -0.17

30 0.10

40 0.31

50 0.52

60 0.71

70 0.91

80 1.12

90 0.57

100 0

1000 0

</Medium_a1>

<High_a1 a1 ="6">

-1000 -0.48

0 -0.48

10 -0.69

20 -0.64

30 -0.27

40 0.03

50 0.27

60 0.52

70 0.74

80 0.96

90 0.46

100 0

</High_a1>

</Inplanewash>

<Downwash>

<Low_a1 a1 ="-6">

-1000 -0.12

0 -0.12

10 0.71

20 1.60

30 1.62

40 1.66

50 1.67

60 1.67

70 1.73

80 1.50

90 1.26

100 1.01

1000 1.01

</Low_a1>

<Medium_a1 a1 ="0">

-1000 0.36

0 0.36

10 0.84

20 1.64

30 1.70

40 1.76

50 1.82

60 1.85

70 1.90

80 1.68

90 1.44

100 1.20

1000 1.20

</Medium_a1>

<High_a1 a1 ="6">

-1000 0.69

0 0.69

10 1.21

20 1.70

30 1.76

40 1.83

50 1.90

60 1.97

70 2.03

80 1.92

90 1.74

100 1.39

1000 1.39

</High_a1>

</Downwash>

</AerodynamicFeatures>

</Rotor>

</Rotors>

<StabilizersAndWings>

<HorizontalStabilizerRight>

<Geometry>

<Position x="1.8140" y="-4.9460" z="0.9800"/>

<Up x="0.0" y="0.03489" z="0.9993908"/>

<Front x="0" y="0.9993908" z="-0.03489"/>

<SurfaceArea area="0.291028"/>

</Geometry>

<ControlResponse controlSurfaceLiftCoeffDerivative="0.0" controlSurfaceForceArmPos="0.0" />

<AerodynamicFeatures>

<DynamicPressureRatio>

<AoA>

-1000 0.93

-30 0.93

-25 0.93

-20 0.88

-15 0.71

-10 0.71

-5 0.71

0 0.71

5 0.71

10 0.71

15 0.76

20 0.85

25 0.93

30 0.93

1000 0.93

</AoA>

</DynamicPressureRatio>

<MainRotorInplanewash>

<Low_a1 a1 ="-6">

-1000 0

0 0

10 -0.18

20 0.04

30 0.26

40 0.47

50 0.70

60 0.91

70 1.14

80 1.36

90 0.70

100 0

1000 0

</Low_a1>

<Medium_a1 a1 ="0">

-1000 -0.35

0 -0.35

10 -0.53

20 -0.18

30 0.11

40 0.32

50 0.53

60 0.73

70 0.93

80 1.14

90 0.58

100 0

1000 0

</Medium_a1>

<High_a1 a1 ="6">

-1000 -0.49

0 -0.49

10 -0.70

20 -0.65

30 -0.28

40 0.03

50 0.28

60 0.53

70 0.76

80 0.99

90 0.47

100 0

1000 0

</High_a1>

</MainRotorInplanewash>

<MainRotorDownwash>

<Low_a1 a1 ="-6">

-1000 -0.12

0 -0.12

10 0.74

20 1.66

30 1.67

40 1.71

50 1.73

60 1.76

70 1.78

80 1.55

90 1.30

100 1.05

1000 1.05

</Low_a1>

<Medium_a1 a1 ="0">

-1000 0.37

0 0.37

10 0.86

20 1.69

30 1.76

40 1.82

50 1.88

60 1.91

70 1.97

80 1.74

90 1.49

100 1.24

1000 1.24

</Medium_a1>

<High_a1 a1 ="6">

-1000 0.72

0 0.72

10 1.25

20 1.76

30 1.82

40 1.89

50 1.97

60 2.03

70 2.10

80 1.99

90 1.80

100 1.43

1000 1.43

</High_a1>

</MainRotorDownwash>

<GroundEffect startDistance="1.6" strength="0.0"/>

<LiftCurve>

-1000 0

-180 0

-150 0.61

-140 0.69

-130 0.69

-120 0.61

-110 0.46

-100 0.24

-90 0

-80 -0.24

-70 -0.46

-60 -0.61

-50 -0.69

-40 -0.79

-30 -0.91

0 -0.2

30 0.41

40 0.79

50 0.69

60 0.61

70 0.46

80 0.24

90 0

100 -0.24

110 -0.46

120 -0.61

130 -0.69

140 -0.69

150 -0.61

180 0

1000 0

</LiftCurve>

<DragCurve >

-1000 0.0

-180 0.0

-140 0.42

-130 0.56

-120 0.71

-110 0.84

-100 0.93

-90 0.96

-80 0.93

-70 0.84

-60 0.71

-50 0.56

-40 0.42

0 0.008

40 0.42

50 0.56

60 0.71

70 0.84

80 0.93

90 0.96

100 0.93

110 0.84

120 0.71

130 0.56

140 0.42

180 0.0

1000 0.0

</DragCurve>

</AerodynamicFeatures>

</HorizontalStabilizerRight>

<HorizontalStabilizerLeft copy="HorizontalStabilizerRight">

<Geometry>

<Position x="-1.8140" />

</Geometry>

</HorizontalStabilizerLeft>

<VerticalStabilizer>

<Geometry>

<Position x="0" y="-4.778" z="0.1340"/>

<Up x="-1.0" y="0.0" z="0"/>

<Front x="0" y="1.0" z="0"/>

<SurfaceArea area="0.59"/>

</Geometry>

<ControlResponse controlSurfaceLiftCoeffDerivative="0.0" controlSurfaceForceArmPos="0.0" />

<AerodynamicFeatures>

<DynamicPressureRatio>

<Sideslip>

-1000 0.95

-30 0.95

-25 0.84

-20 0.75

-15 0.68

-10 0.63

-5 0.61

0 0.59

5 0.61

10 0.63

15 0.68

20 0.75

25 0.84

30 0.95

1000 0.95

</Sideslip>

</DynamicPressureRatio>

<MainRotorInplanewash>

<Low_a1 a1 ="-6">

-1000 0

0 0

10 -0.18

20 0.04

30 0.27

40 0.49

50 0.73

60 0.95

70 1.18

80 1.41

90 0.73

100 0

1000 0

</Low_a1>

<Medium_a1 a1 ="0">

-1000 -0.36

0 -0.36

10 -0.55

20 -0.18

30 0.11

40 0.33

50 0.55

60 0.75

70 0.96

80 1.18

90 0.60

100 0

</Medium_a1>

<High_a1 a1 ="6">

-1000 -0.51

0 -0.51

10 -0.73

20 -0.67

30 -0.29

40 0.04

50 0.29

60 0.55

70 0.78

80 1.02

90 0.49

100 0

1000 0

</High_a1>

</MainRotorInplanewash>

<MainRotorDownwash>

<Low_a1 a1 ="-6">

-1000 -0.12

0 -0.12

10 0.74

20 1.67

30 1.69

40 1.73

50 1.75

60 1.78

70 1.80

80 1.57

90 1.32

100 1.06

1000 1.06

</Low_a1>

<Medium_a1 a1 ="0">

-1000 0.37

0 0.37

10 0.87

20 1.71

30 1.78

40 1.84

50 1.90

60 1.93

70 1.99

80 1.76

90 1.51

100 1.26

1000 1.26

</Medium_a1>

<High_a1 a1 ="6">

-1000 0.72

0 0.72

10 1.26

20 1.78

30 1.84

40 1.92

50 1.99

60 2.05

70 2.12

80 2.01

90 1.82

100 1.45

1000 1.45

</High_a1>

</MainRotorDownwash>

<GroundEffect startDistance="0" strength="0.0"/>

<LiftCurve >

-180 0

-170 0.34

-160 0.74

-150 0.80

-140 0.72

-130 0.57

-120 0.43

-110 0.29

-100 0.15

-90 0

-80 -0.15

-70 -0.29

-60 -0.43

-50 -0.57

-40 -0.72

-30 -0.80

-25 -1.00

-20 -1.34

0 0

20 1.34

25 1.00

30 0.80

40 0.72

50 0.57

60 0.43

70 0.29

80 0.15

90 0

100 -0.15

110 -0.29

120 -0.43

130 -0.57

140 -0.72

150 -0.80

160 -0.74

170 -0.34

180 0

</LiftCurve>

<DragCurve>

-1000 0.0

-180 0.0

-140 0.42

-130 0.56

-120 0.71

-110 0.84

-100 0.93

-90 0.96

-80 0.93

-70 0.84

-60 0.71

-50 0.56

-40 0.42

0 0.008

40 0.42

50 0.56

60 0.71

70 0.84

80 0.93

90 0.96

100 0.93

110 0.84

120 0.71

130 0.56

140 0.42

180 0.0

1000 0.0

</DragCurve>

</AerodynamicFeatures>

</VerticalStabilizer>

</StabilizersAndWings>

<GroundContacts>

<GeneralConfiguration gearExtensionTime="3" gearDragCoefficient="0" gearReferenceArea="0"

maxSteerableGearDeflection="80" steerableGearSpeedCorrectionFactor="0.0"/>

<GroundContact type="FGGroundContact200" >

<Features isBrakable="false" isRetractable="false" isSteerable="false" />

<Aerodynamics equivalentFlatPlateArea ="0.0" />

<Suspension>

<MountStation x="-1.052" y="1.6933" z="-1.6717"/>

<SliderAxis x="0" y="0" z="1" />

<SuspensionLength length="0.2" />

<SpringParameters springConstant="420000" damperConstant="50000" maxCompression="0.18" />

</Suspension>

<Wheel mass="1" radius="0.1" >

<RollAxis x="1" y="0" z="0" />

<Friction slidingFriction="0.8" resistanceTorqueNoBrake="1000" resistanceTorqueFullBrake="1000" />

</Wheel>

<Damage thresholdLoad="20000000" />

</GroundContact>

<GroundContact type="FGGroundContact200" >

<Features isBrakable="false" isRetractable="false" isSteerable="false" />

<Aerodynamics equivalentFlatPlateArea ="0.0" />

<Suspension>

<MountStation x="1.052" y="1.6933" z="-1.6717"/>

<SliderAxis x="0" y="0" z="1" />

<SuspensionLength length="0.2" />

<SpringParameters springConstant="420000" damperConstant="50000" maxCompression="0.18" />

</Suspension>

<Wheel mass="1" radius="0.1" >

<RollAxis x="1" y="0" z="0" />

<Friction slidingFriction="0.8" resistanceTorqueNoBrake="1000" resistanceTorqueFullBrake="1000" />

</Wheel>

<Damage thresholdLoad="20000000" />

</GroundContact>

<GroundContact type="FGGroundContact200" >

<Features isBrakable="false" isRetractable="false" isSteerable="false" />

<Aerodynamics equivalentFlatPlateArea ="0.0" />

<Suspension>

<MountStation x="0.944" y="-0.6387" z="-1.5650"/>

<SliderAxis x="0" y="0" z="1" />

<SuspensionLength length="0.2" />

<SpringParameters springConstant="420000" damperConstant="50000" maxCompression="0.18" />

</Suspension>

<Wheel mass="1" radius="0.1" >

<RollAxis x="1" y="0" z="0" />

<Friction slidingFriction="0.8" resistanceTorqueNoBrake="1000" resistanceTorqueFullBrake="1000" />

</Wheel>

<Damage thresholdLoad="20000000" />

</GroundContact>

<GroundContact type="FGGroundContact200" >

<Features isBrakable="false" isRetractable="false" isSteerable="false" />

<Aerodynamics equivalentFlatPlateArea ="0.0" />

<Suspension>

<MountStation x="-0.944" y="-0.6387" z="-1.5650"/>

<SliderAxis x="0" y="0" z="1" />

<SuspensionLength length="0.2" />

<SpringParameters springConstant="420000" damperConstant="50000" maxCompression="0.18" />

</Suspension>

<Wheel mass="1" radius="0.1" >

<RollAxis x="1" y="0" z="0" />

<Friction slidingFriction="0.8" resistanceTorqueNoBrake="1000" resistanceTorqueFullBrake="1000" />

</Wheel>

<Damage thresholdLoad="20000000" />

</GroundContact>

<GroundContact type="FGGroundContact200" >

<Features isBrakable="false" isRetractable="false" isSteerable="false" />

<Aerodynamics equivalentFlatPlateArea ="0.0" />

<Suspension>

<MountStation x="0" y="-4.341" z="-0.65"/>

<SliderAxis x="0" y="0" z="1" />

<SuspensionLength length="0" />

<SpringParameters springConstant="420000" damperConstant="50000" maxCompression="0" />

</Suspension>

<Wheel mass="0.1" radius="0.1" >

<RollAxis x="1" y="0" z="0" />

<Friction slidingFriction="0.8" resistanceTorqueNoBrake="1000" resistanceTorqueFullBrake="1000" />

</Wheel>

<Damage thresholdLoad="20000000" />

</GroundContact>

</GroundContacts>

</GenHeli600>

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You can also try to alter InputMapping nonlinearity="1.5" in both pitch and bank RateController (ControlSystem block in XML). Removing any nonlinearity may help users to adjust the controler imput better in game controler options.

Real pilots, who prefer no centering force on stick and hold it with just fingertips may prefer linear response. Gamers with normal joystick who hold the stick with whole wirst, will most likely prefer smoother response curve (gamma 1.5 and more which is 1/4 or less on sensitivity slider)

Thank you, i'm sure this can help a lot!! i have found some problems at high speed with pitch i attached this to the horizontal stabilizer, the real helicopters are more leveled in cruise the h stabilizer need to be more powerful with speed.

Another bug is the main rotor rpm gauge in the medium, this one show the engines rpms instead the main rotor rpms, is there some way to get the main rotor rpms in the game? via script or something..:rolleyes:

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Heli flying... what program are you using to repack your .pbo and where in your TOH folder are you placing everything? I am totally confused by this process and everything I am reading on the forums and in Dev-heaven is just confusing me even more.

Thanks in advance.

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i use cpbo.exe when you run this for first time the program create a registry association to every folder and later to repack the folder just right click and select "create a pbo", in win7 run as administrator

download it from this link:

http://www.kegetys.net/dl.php/tools07072010.zip

the folder to repack need config and prefix files in other words the last air_us_h folder

air_us_h/h_sim/air_us_h and this is your new air_us_h.pbo work in the same way like the original put this one in the addons folder

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