| Verzögertes Einfahren der Fahrwerksklappen Durch richtiges Einstellen in der tmd-Datei kann man erreichen, dass die Fahrwerksklappen sich erst nach dem Einziehen des Fahrwerks schliessen bzw. sich erst die Klappen öffnen und dann das Fahrwerk ausgefahren wird!Append tmdjoint00 JointFuselageFrontdoor1L
Append tmdjoint00 JointFuselageFrontdoor1R
Append tmdjoint00 JointFuselageFrontdoor2L
Append tmdjoint00 JointFuselageFrontdoor2R
Append tmdbody Frontdoor1L
Append tmdbody Frontdoor1R
Append tmdbody Frontdoor2L
Append tmdbody Frontdoor2R
Append tmdservo01 ServoGearDoor
cd JointFuselageFrontdoor1L/
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( 0.5209, 0.0309, -0.1038, 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
Body0 = ../Fuselage/
Body1 = ../Frontdoor1L/
Kf = 2000
Df = 10
Ktx = 400
Dtx = 0.2
Kty = 400
Dty = 0.2
Ktz = 400
Dtz = 0.2
MaxForce = 1000
MaxTorque = 10
Rigid = 0
Essential = 0
Link = ~Aircraft/ServoGearDoor/MechLink
Angle = 1.5
AngleZ = 0
Axis = tmvector4r( 0.5000, 0.0000, 0.5000, 0 )
Displacement = tmvector4r( 0.0000, 0.0000, 0.0000, 0 )
cd ../
cd JointFuselageFrontdoor1R/
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( 0.5209, -0.0309, -0.1038, 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
Body0 = ../Fuselage/
Body1 = ../Frontdoor1R/
Kf = 2000
Df = 10
Ktx = 400
Dtx = 0.2
Kty = 400
Dty = 0.2
Ktz = 400
Dtz = 0.2
MaxForce = 1000
MaxTorque = 10
Rigid = 0
Essential = 0
Link = ~Aircraft/ServoGearDoor/MechLink
Angle = -1.5
AngleZ = 0
Axis = tmvector4r( 0.5000, 0.0000, 0.5000, 0 )
Displacement = tmvector4r( 0.0000, 0.0000, 0.0000, 0 )
cd ../
cd JointFuselageFrontdoor2L/
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( 0.4883, 0.0309, -0.1073, 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
Body0 = ../Fuselage/
Body1 = ../Frontdoor2L/
Kf = 2000
Df = 10
Ktx = 400
Dtx = 0.2
Kty = 400
Dty = 0.2
Ktz = 400
Dtz = 0.2
MaxForce = 1000
MaxTorque = 10
Rigid = 0
Essential = 0
Link = ~Aircraft/ServoGearDoor/MechLink
Angle = 1.5
AngleZ = 0
Axis = tmvector4r( 1.0000, 0.0000, 0.0000, 0 )
Displacement = tmvector4r( 0.0000, 0.0000, 0.0000, 0 )
cd ../
cd JointFuselageFrontdoor2R/
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( 0.4883, -0.0309, -0.1073, 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
Body0 = ../Fuselage/
Body1 = ../Frontdoor2R/
Kf = 2000
Df = 10
Ktx = 400
Dtx = 0.2
Kty = 400
Dty = 0.2
Ktz = 400
Dtz = 0.2
MaxForce = 1000
MaxTorque = 10
Rigid = 0
Essential = 0
Link = ~Aircraft/ServoGearDoor/MechLink
Angle = -1.5
AngleZ = 0
Axis = tmvector4r( 1.0000, 0.0000, 0.0000, 0 )
Displacement = tmvector4r( 0.0000, 0.0000, 0.0000, 0 )
cd ../
cd Frontdoor1L/
X = tmvector4r( -0.8278, 0.0040, -0.5610, 0 )
Y = tmvector4r( -0.5610, 0.0003, 0.8278, 0 )
Z = tmvector4r( 0.0034, 1.0000, 0.0020, 0 )
R = tmvector4r( 0.5523, 0.0294, -0.1023, 1 )
Geometry( "~Geometry/Frontdoor1L/" )
Mass = 0.2
RangeMassMax = 0.2
RangeMassMin = 0.05
Inertia = { 0.0010, -0.0000, 0.0000, 0.0000, -0.0000, 0.0010, -0.0000, 0.0000, 0.0000, -0.0000, 0.0010, 0.0000, 0.0000, 0.0000, 0.0000, 494.5399 }
Kn = 1000
Dn = 20
Dv = 0.02
cd ../
cd Frontdoor1R/
X = tmvector4r( -0.8278, -0.0040, -0.5610, 0 )
Y = tmvector4r( 0.5610, 0.0003, -0.8278, 0 )
Z = tmvector4r( 0.0034, -1.0000, 0.0020, 0 )
R = tmvector4r( 0.5523, -0.0294, -0.1023, 1 )
Geometry( "~Geometry/Frontdoor1R/" )
Mass = 0.2
RangeMassMax = 0.2
RangeMassMin = 0.05
Inertia = { 0.0010, 0.0000, -0.0000, 0.0000, 0.0000, 0.0010, 0.0000, 0.0000, -0.0000, 0.0000, 0.0010, 0.0000, 0.0000, 0.0000, 0.0000, 494.5399 }
Kn = 1000
Dn = 20
Dv = 0.02
cd ../
cd Frontdoor2L/
X = tmvector4r( 0.9994, -0.0009, 0.0353, 0 )
Y = tmvector4r( 0.0009, 1.0000, -0.0000, 0 )
Z = tmvector4r( -0.0353, 0.0000, 0.9994, 0 )
R = tmvector4r( 0.4216, 0.0294, -0.1250, 1 )
Geometry( "~Geometry/Frontdoor2L/" )
Mass = 0.2
RangeMassMax = 0.2
RangeMassMin = 0.05
Inertia = { 0.0010, 0.0000, -0.0000, 0.0000, 0.0000, 0.0010, 0.0000, 0.0000, -0.0000, 0.0000, 0.0010, 0.0000, 0.0000, 0.0000, 0.0000, 143.8128 }
Kn = 1000
Dn = 20
Dv = 0.02
cd ../
cd Frontdoor2R/
X = tmvector4r( 0.9994, 0.0009, 0.0353, 0 )
Y = tmvector4r( -0.0009, 1.0000, 0.0000, 0 )
Z = tmvector4r( -0.0353, -0.0000, 0.9994, 0 )
R = tmvector4r( 0.4216, -0.0294, -0.1250, 1 )
Geometry( "~Geometry/Frontdoor2R/" )
Mass = 0.2
RangeMassMax = 0.2
RangeMassMin = 0.05
Inertia = { 0.0010, -0.0000, -0.0000, 0.0000, -0.0000, 0.0010, -0.0000, 0.0000, -0.0000, -0.0000, 0.0010, 0.0000, 0.0000, 0.0000, 0.0000, 143.8128 }
Kn = 1000
Dn = 20
Dv = 0.02
cd ../
cd ServoGearDoor/
SignalIn = ~Aircraft/Receiver/Out(24)
VelocityIn = 0.8
VelocityOut = 5
ValueNumber = 3
ValueIn(0) = -1
ValueOut(0) = 0
ValueIn(1) = 0.9
ValueOut(1) = 0
ValueIn(2) = 1
ValueOut(2) = 1
PositionFirst = -1
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
cd ../ |
