// aerofly professional --------------------------------------------------------
//
// file:    SkyLady.tmd
// version: 1.11.0
//
// type:    97
// lock:    0
//
// -----------------------------------------------------------------------------


Append tmdjoint00 JointFuselageEngine
Append tmdjoint00 JointFuselageStabilizer
Append tmdjoint00 JointStabilizerLeftStabilizer
Append tmdjoint00 JointStabilizerRightStabilizer
Append tmdjoint00 JointFuselageLeftWing
Append tmdjoint00 JointFuselageRightWing
Append tmdjoint00 JointGearLeftWheel
Append tmdjoint00 JointGearRightWheel
Append tmdjoint00 JointFuselageGear
Append tmdfuselage00 Fuselage
Append tmdwing00 LeftWing
Append tmdwing00 RightWing
Append tmdwing11 Stabilizer
Append tmdwing10 LeftStabilizer
Append tmdwing10 RightStabilizer
Append tmdgear00 Gear
Append tmdwheel00 LeftWheel
Append tmdwheel00 RightWheel
Append tmdengine10 Engine
Append tmdpropeller00 Propeller
Append tmdservo00 ServoRudder
Append tmdservo00 ServoElevator
Append tmdservo00 ServoThrottle
Append tmdreceiver00 Receiver
cd JointFuselageEngine/
X    = tmvector4r(   1.0000,   0.0000,   0.0000, 0 )
Y    = tmvector4r(   0.0000,   1.0000,   0.0000, 0 )
Z    = tmvector4r(   0.0000,   0.0000,   1.0000, 0 )
R    = tmvector4r(   0.0000,   0.0000,   0.0000, 1 )
Mass = 0
RangeMassMax = 0
RangeMassMin = 0
Inertia = {   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000 }
Kn = 1000
Dn = 20
Dv = 5
Dbxy = 1
Body0 = ../Fuselage/
Body1 = ../Engine/
Kf = 10000
Df = 100
Kfx = 0
Dfx = 0
Kfy = 0
Dfy = 0
Kfz = 0
Dfz = 0
Ktx = 1000
Dtx = 10
Kty = 1000
Dty = 10
Ktz = 1000
Dtz = 10
MaxForce = 0
MaxTorque = 0
Rigid = 1
Essential = 1
Angle = 0
AngleZ = 0
Axis = tmvector4r(   0.0000,   0.0000,   0.0000, 0 )
Displacement = tmvector4r(   0.0000,   0.0000,   0.0000, 0 )
cd ../

cd JointFuselageStabilizer/
X    = tmvector4r(   1.0000,   0.0000,   0.0000, 0 )
Y    = tmvector4r(   0.0000,   1.0000,   0.0000, 0 )
Z    = tmvector4r(   0.0000,   0.0000,   1.0000, 0 )
R    = tmvector4r(  -0.5108,   0.0000,   0.0157, 1 )
Mass = 0
RangeMassMax = 0
RangeMassMin = 0
Inertia = {   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000 }
Kn = 1000
Dn = 20
Dv = 5
Dbxy = 1
Body0 = ../Fuselage/
Body1 = ../Stabilizer/
Kf = 2000
Df = 2
Kfx = 0
Dfx = 0
Kfy = 0
Dfy = 0
Kfz = 0
Dfz = 0
Ktx = 10
Dtx = 0.01
Kty = 10
Dty = 0.01
Ktz = 10
Dtz = 0.01
MaxForce = 200
MaxTorque = 1
Rigid = 1
Essential = 1
Angle = 0
AngleZ = 0
Axis = tmvector4r(   0.0000,   0.0000,   0.0000, 0 )
Displacement = tmvector4r(   0.0000,   0.0000,   0.0000, 0 )
cd ../

cd JointStabilizerLeftStabilizer/
X    = tmvector4r(   1.0000,   0.0000,   0.0000, 0 )
Y    = tmvector4r(   0.0000,   1.0000,   0.0000, 0 )
Z    = tmvector4r(   0.0000,   0.0000,   1.0000, 0 )
R    = tmvector4r(  -0.5132,   0.0000,   0.1312, 1 )
Mass = 0
RangeMassMax = 0
RangeMassMin = 0
Inertia = {   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000 }
Kn = 1000
Dn = 20
Dv = 5
Dbxy = 1
Body0 = ../Stabilizer/
Body1 = ../LeftStabilizer/
Kf = 5000
Df = 5
Kfx = 0
Dfx = 0
Kfy = 0
Dfy = 0
Kfz = 0
Dfz = 0
Ktx = 10
Dtx = 0.01
Kty = 10
Dty = 0.01
Ktz = 10
Dtz = 0.01
MaxForce = 1000
MaxTorque = 4
Rigid = 1
Essential = 1
Angle = 0
AngleZ = 0
Axis = tmvector4r(   0.0000,   0.0000,   0.0000, 0 )
Displacement = tmvector4r(   0.0000,   0.0000,   0.0000, 0 )
cd ../

cd JointStabilizerRightStabilizer/
X    = tmvector4r(   1.0000,   0.0000,   0.0000, 0 )
Y    = tmvector4r(   0.0000,   1.0000,   0.0000, 0 )
Z    = tmvector4r(   0.0000,   0.0000,   1.0000, 0 )
R    = tmvector4r(  -0.5132,   0.0000,   0.1312, 1 )
Mass = 0
RangeMassMax = 0
RangeMassMin = 0
Inertia = {   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000 }
Kn = 1000
Dn = 20
Dv = 5
Dbxy = 1
Body0 = ../Stabilizer/
Body1 = ../RightStabilizer/
Kf = 5000
Df = 5
Kfx = 0
Dfx = 0
Kfy = 0
Dfy = 0
Kfz = 0
Dfz = 0
Ktx = 10
Dtx = 0.01
Kty = 10
Dty = 0.01
Ktz = 10
Dtz = 0.01
MaxForce = 1000
MaxTorque = 4
Rigid = 1
Essential = 1
Angle = 0
AngleZ = 0
Axis = tmvector4r(   0.0000,   0.0000,   0.0000, 0 )
Displacement = tmvector4r(   0.0000,   0.0000,   0.0000, 0 )
cd ../

cd JointFuselageLeftWing/
X    = tmvector4r(   1.0000,   0.0000,   0.0000, 0 )
Y    = tmvector4r(   0.0000,   1.0000,   0.0000, 0 )
Z    = tmvector4r(   0.0000,   0.0000,   1.0000, 0 )
R    = tmvector4r(  -0.0053,   0.0000,   0.0235, 1 )
Mass = 0
RangeMassMax = 0
RangeMassMin = 0
Inertia = {   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000 }
Kn = 1000
Dn = 20
Dv = 5
Dbxy = 1
Body0 = ../Fuselage/
Body1 = ../LeftWing/
Kf = 400
Df = 1
Kfx = 0
Dfx = 0
Kfy = 0
Dfy = 0
Kfz = 0
Dfz = 0
Ktx = 12
Dtx = 0.15
Kty = 12
Dty = 0.15
Ktz = 12
Dtz = 0.15
MaxForce = 20
MaxTorque = 5
Rigid = 1
Essential = 1
Angle = 0
AngleZ = 0
Axis = tmvector4r(   0.0000,   0.0000,   0.0000, 0 )
Displacement = tmvector4r(   0.0000,   0.0000,   0.0000, 0 )
cd ../

cd JointFuselageRightWing/
X    = tmvector4r(   1.0000,   0.0000,   0.0000, 0 )
Y    = tmvector4r(   0.0000,   1.0000,   0.0000, 0 )
Z    = tmvector4r(   0.0000,   0.0000,   1.0000, 0 )
R    = tmvector4r(  -0.0053,   0.0000,   0.0235, 1 )
Mass = 0
RangeMassMax = 0
RangeMassMin = 0
Inertia = {   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000 }
Kn = 1000
Dn = 20
Dv = 5
Dbxy = 1
Body0 = ../Fuselage/
Body1 = ../RightWing/
Kf = 400
Df = 1
Kfx = 0
Dfx = 0
Kfy = 0
Dfy = 0
Kfz = 0
Dfz = 0
Ktx = 12
Dtx = 0.15
Kty = 12
Dty = 0.15
Ktz = 12
Dtz = 0.15
MaxForce = 20
MaxTorque = 5
Rigid = 1
Essential = 1
Angle = 0
AngleZ = 0
Axis = tmvector4r(   0.0000,   0.0000,   0.0000, 0 )
Displacement = tmvector4r(   0.0000,   0.0000,   0.0000, 0 )
cd ../

cd JointGearLeftWheel/
X    = tmvector4r(   1.0000,   0.0000,   0.0000, 0 )
Y    = tmvector4r(   0.0000,   1.0000,   0.0000, 0 )
Z    = tmvector4r(   0.0000,   0.0000,   1.0000, 0 )
R    = tmvector4r(   0.1161,   0.0129,  -0.0520, 1 )
Mass = 0
RangeMassMax = 0
RangeMassMin = 0
Inertia = {   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000 }
Kn = 1000
Dn = 20
Dv = 5
Dbxy = 1
Body0 = ../Gear/
Body1 = ../LeftWheel/
Kf = 4000
Df = 15
Kfx = 0
Dfx = 0
Kfy = 0
Dfy = 0
Kfz = 0
Dfz = 0
Ktx = 200
Dtx = 0.4
Kty = 200
Dty = 0.4
Ktz = 200
Dtz = 0.4
MaxForce = 800
MaxTorque = 20
Rigid = 1
Essential = 1
Angle = 0
AngleZ = 0
Axis = tmvector4r(   0.0000,   0.0000,   0.0000, 0 )
Displacement = tmvector4r(   0.0000,   0.0000,   0.0000, 0 )
cd ../

cd JointGearRightWheel/
X    = tmvector4r(   1.0000,   0.0000,   0.0000, 0 )
Y    = tmvector4r(   0.0000,   1.0000,   0.0000, 0 )
Z    = tmvector4r(   0.0000,   0.0000,   1.0000, 0 )
R    = tmvector4r(   0.1161,  -0.0129,  -0.0520, 1 )
Mass = 0
RangeMassMax = 0
RangeMassMin = 0
Inertia = {   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000 }
Kn = 1000
Dn = 20
Dv = 5
Dbxy = 1
Body0 = ../Gear/
Body1 = ../RightWheel/
Kf = 4000
Df = 15
Kfx = 0
Dfx = 0
Kfy = 0
Dfy = 0
Kfz = 0
Dfz = 0
Ktx = 200
Dtx = 0.4
Kty = 200
Dty = 0.4
Ktz = 200
Dtz = 0.4
MaxForce = 800
MaxTorque = 20
Rigid = 1
Essential = 1
Angle = 0
AngleZ = 0
Axis = tmvector4r(   0.0000,   0.0000,   0.0000, 0 )
Displacement = tmvector4r(   0.0000,   0.0000,   0.0000, 0 )
cd ../

cd JointFuselageGear/
X    = tmvector4r(   1.0000,   0.0000,   0.0000, 0 )
Y    = tmvector4r(   0.0000,   1.0000,   0.0000, 0 )
Z    = tmvector4r(   0.0000,   0.0000,   1.0000, 0 )
R    = tmvector4r(   0.1161,   0.0000,  -0.0520, 1 )
Mass = 0
RangeMassMax = 0
RangeMassMin = 0
Inertia = {   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000 }
Kn = 1000
Dn = 20
Dv = 5
Dbxy = 1
Body0 = ../Fuselage/
Body1 = ../Gear/
Kf = 4000
Df = 15
Kfx = 0
Dfx = 0
Kfy = 0
Dfy = 0
Kfz = 0
Dfz = 0
Ktx = 200
Dtx = 0.4
Kty = 200
Dty = 0.4
Ktz = 200
Dtz = 0.4
MaxForce = 800
MaxTorque = 20
Rigid = 0
Essential = 1
Angle = 0
AngleZ = 0
Axis = tmvector4r(   0.0000,   0.0000,   0.0000, 0 )
Displacement = tmvector4r(   0.0000,   0.0000,   0.0000, 0 )
cd ../

cd Fuselage/
X    = tmvector4r(   1.0000,   0.0000,   0.0000, 0 )
Y    = tmvector4r(   0.0000,   1.0000,   0.0000, 0 )
Z    = tmvector4r(   0.0000,   0.0000,   1.0000, 0 )
R    = tmvector4r(   0.1049,   0.0000,  -0.0321, 1 )
Geometry( "~Geometry/Fuselage/" )
Mass = 0.2
RangeMassMax = 0.3
RangeMassMin = 0.1
Inertia = {   0.0001,   0.0000,   0.0002,   0.0000,   0.0000,   0.0037,   0.0000,   0.0000,   0.0002,   0.0000,   0.0036,   0.0000,   0.0000,   0.0000,   0.0000, 3590.0051 }
Kn = 1000
Dn = 20
Dv = 0.2
Dbxy = 1
AreaCenter = tmvector4r(   0.0000,   0.0000,   0.0490, 1 )
CG = tmvector4r(   0.0100,   0.0000,  -0.0000, 1 )
SmokeNum = 1
SmokeR = tmvector4r(  -0.1600,  -0.0400,  -0.1000, 1 )
SmokeR1 = tmvector4r(   0.0000,   0.0000,   0.0000, 1 )
SmokeR2 = tmvector4r(   0.0000,   0.0000,   0.0000, 1 )
SmokeR3 = tmvector4r(   0.0000,   0.0000,   0.0000, 1 )
Cdx = 0.3
Cly = 0.4
Cdy = 0.8
Clz = 0.8
Cdz = 1
InertiaScale = 0
cd ../

cd LeftWing/
Sections = 2
RootR = tmvector4f(  -0.0053,   0.0000,   0.0235,   1.0000 )
RootN = tmvector4f(   0.0000,   1.0000,   0.0000,   0.0000 )
PropWashFactor = 0
FuselageInterference = 1
Cly = 0.7
RangeSpanMax = 0.8
RangeSpanMin = 0.6
IncidenceOffset = 0
FlapEffect = 1
FlapEffectArea = 0
AileronOffset = tmvector4f(   0.0000,   0.0000,   0.0000,   0.0000 )
FlapDisplacement = tmvector4f(   0.0000,   0.0000,   0.0000,   0.0000 )
Flap1Displacement = tmvector4f(   0.0000,   0.0000,   0.0000,   0.0000 )
AirbrakeDisplacement = 0
AirbrakeCl = 1
AirbrakeCd = 1
// start section 0
SectionR(0)     = tmvector4f(   0.0412,  -0.1436,  -0.0027,   1.0000 )
SectionArea(0)  =   0.0551
SectionChord(0) =   0.1685
SectionAirfoil(0) = "BLERIOT"
// start section 1
SectionR(1)     = tmvector4f(   0.0368,   0.1811,   0.0001,   1.0000 )
SectionArea(1)  =   0.0483
SectionChord(1) =   0.1512
SectionAirfoil(1) = "BLERIOT"
X    = tmvector4r(   0.9990,  -0.0229,   0.0383, 0 )
Y    = tmvector4r(   0.0201,   0.9972,   0.0723, 0 )
Z    = tmvector4r(  -0.0398,  -0.0714,   0.9967, 0 )
R    = tmvector4r(  -0.0194,   0.3066,   0.0375, 1 )
Geometry( "~Geometry/LeftWing/" )
Mass = 0.05
RangeMassMax = 0.15
RangeMassMin = 0.05
Inertia = {   0.0017,  -0.0000,  -0.0000,   0.0000,  -0.0000,   0.0001,  -0.0000,   0.0000,  -0.0000,  -0.0000,   0.0018,   0.0000,   0.0000,   0.0000,   0.0000, 627.4336 }
Kn = 1000
Dn = 10
Dv = 0.2
Dbxy = 1
cd ../

cd RightWing/
Sections = 2
RootR = tmvector4f(  -0.0053,   0.0000,   0.0235,   1.0000 )
RootN = tmvector4f(   0.0000,  -1.0000,   0.0000,   0.0000 )
PropWashFactor = 0
FuselageInterference = 1
Cly = 0.7
RangeSpanMax = 0.8
RangeSpanMin = 0.6
IncidenceOffset = 0
FlapEffect = 1
FlapEffectArea = 0
AileronOffset = tmvector4f(   0.0000,   0.0000,   0.0000,   0.0000 )
FlapDisplacement = tmvector4f(   0.0000,   0.0000,   0.0000,   0.0000 )
Flap1Displacement = tmvector4f(   0.0000,   0.0000,   0.0000,   0.0000 )
AirbrakeDisplacement = 0
AirbrakeCl = 1
AirbrakeCd = 1
// start section 0
SectionR(0)     = tmvector4f(   0.0412,   0.1436,  -0.0027,   1.0000 )
SectionArea(0)  =   0.0551
SectionChord(0) =   0.1685
SectionAirfoil(0) = "BLERIOT"
// start section 1
SectionR(1)     = tmvector4f(   0.0368,  -0.1811,   0.0001,   1.0000 )
SectionArea(1)  =   0.0483
SectionChord(1) =   0.1512
SectionAirfoil(1) = "BLERIOT"
X    = tmvector4r(   0.9990,   0.0229,   0.0383, 0 )
Y    = tmvector4r(  -0.0201,   0.9972,  -0.0723, 0 )
Z    = tmvector4r(  -0.0398,   0.0714,   0.9967, 0 )
R    = tmvector4r(  -0.0194,  -0.3066,   0.0375, 1 )
Geometry( "~Geometry/RightWing/" )
Mass = 0.05
RangeMassMax = 0.15
RangeMassMin = 0.05
Inertia = {   0.0017,   0.0000,  -0.0000,   0.0000,   0.0000,   0.0001,   0.0000,   0.0000,  -0.0000,   0.0000,   0.0018,   0.0000,   0.0000,   0.0000,   0.0000, 627.4349 }
Kn = 1000
Dn = 10
Dv = 0.2
Dbxy = 1
cd ../

cd Stabilizer/
Sections = 1
RootR = tmvector4f(  -0.5108,   0.0000,   0.0157,   1.0000 )
RootN = tmvector4f(   0.0000,   0.0000,   1.0000,   0.0000 )
Flap = ~Geometry/Stabilizer/Rudder/
FlapLink = ~Aircraft/ServoRudder/MechLink
FlapRotation = 0.8
PropWashFactor = 0.5
Dwf = 0
RangeSpanMax = 0.15
RangeSpanMin = 0.1
// start section 0
SectionR(0)     = tmvector4f(   0.0247,  -0.0112,  -0.0000,   1.0000 )
SectionArea(0)  =   0.0118
SectionChord(0) =   0.0964
SectionAirfoil(0) = "NACA 0009"
X    = tmvector4r(   1.0000,   0.0001,  -0.0000, 0 )
Y    = tmvector4r(   0.0000,  -0.0000,  -1.0000, 0 )
Z    = tmvector4r(  -0.0001,   1.0000,  -0.0000, 0 )
R    = tmvector4r(  -0.5056,  -0.0000,   0.0652, 1 )
Geometry( "~Geometry/Stabilizer/" )
Mass = 0.015
RangeMassMax = 0.02
RangeMassMin = 0.01
Inertia = {   0.0000,   0.0000,  -0.0000,   0.0000,   0.0000,   0.0000,  -0.0000,   0.0000,  -0.0000,  -0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000, 280.1297 }
Kn = 10000
Dn = 40
Dv = 0.2
Dbxy = 1
cd ../

cd LeftStabilizer/
Sections = 1
RootR = tmvector4f(  -0.5132,   0.0000,   0.1312,   1.0000 )
RootN = tmvector4f(   0.0000,   0.0000,   0.0000,   0.0000 )
Flap = ~Geometry/LeftStabilizer/LeftElevator/
FlapLink = ~Aircraft/ServoElevator/MechLink
FlapRotation = 0.8
PropWashFactor = 0.1
Dwf = 0
RangeSpanMax = 0.2
RangeSpanMin = 0.16
// start section 0
SectionR(0)     = tmvector4f(   0.0206,   0.0052,  -0.0000,   1.0000 )
SectionArea(0)  =   0.0132
SectionChord(0) =   0.0791
SectionAirfoil(0) = "FLAT"
X    = tmvector4r(   1.0000,   0.0000,   0.0003, 0 )
Y    = tmvector4r(   0.0000,   1.0000,  -0.0000, 0 )
Z    = tmvector4r(  -0.0003,   0.0000,   1.0000, 0 )
R    = tmvector4r(  -0.5067,   0.0819,   0.1386, 1 )
Geometry( "~Geometry/LeftStabilizer/" )
Mass = 0.01
RangeMassMax = 0.02
RangeMassMin = 0.01
Inertia = {   0.0000,   0.0000,  -0.0000,   0.0000,   0.0000,   0.0000,  -0.0000,   0.0000,  -0.0000,  -0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000, 124.0612 }
Kn = 10000
Dn = 40
Dv = 0.2
Dbxy = 1
cd ../

cd RightStabilizer/
Sections = 1
RootR = tmvector4f(  -0.5132,   0.0000,   0.1312,   1.0000 )
RootN = tmvector4f(   0.0000,   0.0000,   0.0000,   0.0000 )
Flap = ~Geometry/RightStabilizer/RightElevator/
FlapLink = ~Aircraft/ServoElevator/MechLink
FlapRotation = 0.8
PropWashFactor = 0.1
Dwf = 0
RangeSpanMax = 0.2
RangeSpanMin = 0.16
// start section 0
SectionR(0)     = tmvector4f(   0.0206,  -0.0052,  -0.0000,   1.0000 )
SectionArea(0)  =   0.0132
SectionChord(0) =   0.0791
SectionAirfoil(0) = "FLAT"
X    = tmvector4r(   1.0000,   0.0000,   0.0003, 0 )
Y    = tmvector4r(   0.0000,   1.0000,  -0.0000, 0 )
Z    = tmvector4r(  -0.0003,   0.0000,   1.0000, 0 )
R    = tmvector4r(  -0.5067,  -0.0819,   0.1386, 1 )
Geometry( "~Geometry/RightStabilizer/" )
Mass = 0.01
RangeMassMax = 0.02
RangeMassMin = 0.01
Inertia = {   0.0000,  -0.0000,  -0.0000,   0.0000,  -0.0000,   0.0000,   0.0000,   0.0000,  -0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000, 124.7559 }
Kn = 10000
Dn = 40
Dv = 0.2
Dbxy = 1
cd ../

cd Gear/
MountingR = tmvector4f(   0.1161,   0.0000,  -0.0520,   1.0000 )
MountingZ = tmvector4f(   1.0000,   0.0000,   0.0000,   0.0000 )
Retractable = 0
RetractZ = tmvector4f(   1.0000,   0.0000,   0.0000,   0.0000 )
RetractAngle = 0
RetractAngleZ = 0
Cdx = 0
X    = tmvector4r(   1.0000,   0.0000,   0.0000, 0 )
Y    = tmvector4r(  -0.0000,   1.0000,   0.0000, 0 )
Z    = tmvector4r(   0.0000,  -0.0000,   1.0000, 0 )
R    = tmvector4r(   0.1161,  -0.0000,  -0.0520, 1 )
Geometry( "~Geometry/Gear/" )
Mass = 0.005
RangeMassMax = 0
RangeMassMin = 0
Inertia = {   0.0000,  -0.0000,   0.0000,   0.0000,  -0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000, 811.4858 }
Kn = 0
Dn = 0
Dv = 0
Dbxy = 1
cd ../

cd LeftWheel/
X    = tmvector4r(   1.0000,   0.0000,   0.0000, 0 )
Y    = tmvector4r(   0.0000,   1.0000,   0.0000, 0 )
Z    = tmvector4r(   0.0000,   0.0000,   1.0000, 0 )
R    = tmvector4r(   0.1161,   0.0106,  -0.0520, 1 )
Geometry( "~Geometry/LeftWheel/" )
Mass = 0.005
RangeMassMax = 0
RangeMassMin = 0
Inertia = {   0.0020,   0.0000,   0.0000,   0.0000,   0.0000,   0.0020,   0.0000,   0.0000,   0.0000,   0.0000,   0.0020,   0.0000,   0.0000,   0.0000,   0.0000,   1.0000 }
Kn = 0
Dn = 0
Dv = 0
Dbxy = 1
Kxr = 0.7
Kyr = 0.8
Kr  = 10000
Dr  = 0
Kbrake = 0.4
RotationEnable = 1
cd ../

cd RightWheel/
X    = tmvector4r(   1.0000,   0.0000,   0.0000, 0 )
Y    = tmvector4r(   0.0000,   1.0000,   0.0000, 0 )
Z    = tmvector4r(   0.0000,   0.0000,   1.0000, 0 )
R    = tmvector4r(   0.1161,  -0.0106,  -0.0520, 1 )
Geometry( "~Geometry/RightWheel/" )
Mass = 0.005
RangeMassMax = 0
RangeMassMin = 0
Inertia = {   0.0020,   0.0000,   0.0000,   0.0000,   0.0000,   0.0020,   0.0000,   0.0000,   0.0000,   0.0000,   0.0020,   0.0000,   0.0000,   0.0000,   0.0000,   1.0000 }
Kn = 0
Dn = 0
Dv = 0
Dbxy = 1
Kxr = 0.7
Kyr = 0.8
Kr  = 10000
Dr  = 0
Kbrake = 0.4
RotationEnable = 1
cd ../

cd Engine/
X    = tmvector4r(   1.0000,   0.0000,   0.0000, 0 )
Y    = tmvector4r(   0.0000,   1.0000,   0.0000, 0 )
Z    = tmvector4r(   0.0000,   0.0000,   1.0000, 0 )
R    = tmvector4r(   0.0000,   0.0000,   0.0000, 1 )
Mass = 0.267
RangeMassMax = 0.288
RangeMassMin = 0.072
Inertia = {   0.0000,  -0.0000,  -0.0000,   0.0000,  -0.0000,   0.0000,  -0.0000,   0.0000,  -0.0000,  -0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.1911 }
Kn = 4000
Dn = 10
Dv = 5
Dbxy = 1
ThrottleControl = ~Aircraft/ServoThrottle/MechLink
Sound0File = "beryll0"
Sound1File = "beryll1"
Sound0RPM = 7000.000000
Sound0RPMLow = 500.000000
Sound1RPM = 1000.000000
Sound01RPM = 4500.000000
SoundRange = 2000.0
TorqueFactor = 0.010000
ConstantRPM = 0
MotorNs = 2000.000000
MotorRi = 0.047000
MotorI0 = 1.000000
MotorMass = 0.092000
MotorR = tmvector4r(   0.0000,   0.0000,   0.0000, 1 )
CellNum = 7
CellVoltage = 1.200000
CellMass = 0.025000
CellRi = 0.000100
CellR = tmvector4r(   0.0000,   0.0000,   0.0000, 1 )
GearRatio = 1.000000
GearMass = 0.000000
GearEta = 1.000000
Brake = 0.000000
cd ../

cd Propeller/
X    = tmvector4r(   0.0000,   1.0000,   0.0000, 0 )
Y    = tmvector4r(   0.0000,   0.0000,   1.0000, 0 )
Z    = tmvector4r(   1.0000,   0.0000,   0.0000, 0 )
R    = tmvector4r(   0.2172,   0.0000,  -0.0190, 1 )
Geometry( "~Geometry/Propeller/" )
Mass = 0.015
RangeMassMax = 0.25
RangeMassMin = 0.01
Inertia = {   0.0004,   0.0000,   0.0000,   0.0000,   0.0000,   0.0004,   0.0000,   0.0000,   0.0000,   0.0000,   0.0004,   0.0000,   0.0000,   0.0000,   0.0000,   1.0000 }
Kn = 4000
Dn = 10
Dv = 5
Dbxy = 1
Radius = 0.0762
RangeRadiusMax = 0.0889
RangeRadiusMin = 0.0635
Pitch  = 0.0761995
DragLateral  = 0.005
StopNumber = 0
StopPosition = 0
Folding = 0.0000
FoldingR = tmvector4r(   0.0000,   0.0000,   0.0000, 1 )
Engine = ~Aircraft/Engine/
cd ../

cd ServoRudder/
SignalIn = ~Aircraft/Receiver/Out(8)
P0 = 0
P1 = 0.610865
P2 = 0
P3 = 0
PFirst = 0
Vmax = 10
Vmaxdown = 0
X    = tmvector4r(   1.0000,   0.0000,   0.0000, 0 )
Y    = tmvector4r(   0.0000,   1.0000,   0.0000, 0 )
Z    = tmvector4r(   0.0000,   0.0000,   1.0000, 0 )
R    = tmvector4r(   0.0000,   0.0000,   0.0000, 1 )
Mass = 0
RangeMassMax = 0
RangeMassMin = 0
Inertia = {   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000 }
Kn = 1000
Dn = 20
Dv = 5
Dbxy = 1
cd ../

cd ServoElevator/
SignalIn = ~Aircraft/Receiver/Out(4)
P0 = 0
P1 = 0.349066
P2 = 0
P3 = 0
PFirst = 0
Vmax = 10
Vmaxdown = 0
X    = tmvector4r(   1.0000,   0.0000,   0.0000, 0 )
Y    = tmvector4r(   0.0000,   1.0000,   0.0000, 0 )
Z    = tmvector4r(   0.0000,   0.0000,   1.0000, 0 )
R    = tmvector4r(   0.0000,   0.0000,   0.0000, 1 )
Mass = 0
RangeMassMax = 0
RangeMassMin = 0
Inertia = {   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000 }
Kn = 1000
Dn = 20
Dv = 5
Dbxy = 1
cd ../

cd ServoThrottle/
SignalIn = ~Aircraft/Receiver/Out(0)
P0 = 0
P1 = 1
P2 = 0
P3 = 0
PFirst = -1
Vmax = 2
Vmaxdown = 0
X    = tmvector4r(   1.0000,   0.0000,   0.0000, 0 )
Y    = tmvector4r(   0.0000,   1.0000,   0.0000, 0 )
Z    = tmvector4r(   0.0000,   0.0000,   1.0000, 0 )
R    = tmvector4r(   0.0000,   0.0000,   0.0000, 1 )
Mass = 0
RangeMassMax = 0
RangeMassMin = 0
Inertia = {   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000 }
Kn = 1000
Dn = 20
Dv = 5
Dbxy = 1
cd ../

cd Receiver/
X    = tmvector4r(   1.0000,   0.0000,   0.0000, 0 )
Y    = tmvector4r(   0.0000,   1.0000,   0.0000, 0 )
Z    = tmvector4r(   0.0000,   0.0000,   1.0000, 0 )
R    = tmvector4r(   0.0000,   0.0000,   0.0000, 1 )
Mass = 0
RangeMassMax = 0
RangeMassMin = 0
Inertia = {   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000,   0.0000 }
Kn = 1000
Dn = 20
Dv = 5
Dbxy = 1
VTailMixElevator = 0.77
VTailMixRudder   = 0.42
MixButterflyAileron = 0
MixButterflyFlap = 0
MixButterflyElevator = 0
MixPowerElevator = 0
MixAileronFlap = 0
MixFlapReduction = 1
cd ../