65 lines
1.3 KiB
C++
65 lines
1.3 KiB
C++
// GENERAL
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maxSpeed=800;
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enginePower=1.193;
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landingAOA=__EVAL(3*3.1415/180);
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landingSpeed=215;
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stallSpeed=148;
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stallWarningTreshold=0.1;
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wheelSteeringSensitivity=1.5;
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airBrake=1;
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airBrakeFrictionCoef=2.5;
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flaps=1;
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flapsFrictionCoef=0.32;
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gearsUpFrictionCoef=0.6;
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airFrictionCoefs0[]=
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{
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0.0,0.0,0.0
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};
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airFrictionCoefs1[]=
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{
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0.1,0.5,0.0066
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};
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airFrictionCoefs2[]=
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{
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0.001,0.005,0.000068
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};
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angleOfIndicence=__EVAL(-2*3.1415/180);
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envelope[]=
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{
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0.00,0.05,0.60,0.90,1.40,1.80,2.10,2.40,2.88,3.65,4.50,5.45,6.48,7.61,8.10,8.30,8.40,8.30,8.00,7.60,7.00
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};
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altNoForce=11000;
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altFullForce=2500;
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thrustCoef[]=
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{
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1.22,1.28,1.34,1.35,1.35,1.4,1.49,1.01,0.57,0.37,0.26,0.16,0.10,0.00,0.00,0.00,0.00
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};
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aileronSensitivity=0.7;
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aileronCoef[]=
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{
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0,0.11,0.445,0.81,1.0,1.05,1.1,1.15,1.2,1.3,1.3,1.33,1.35,1.34,1.29,1.2,0.800
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};
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elevatorSensitivity=0.85;
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elevatorCoef[]=
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{
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0,0.14,0.54,0.62,0.588,0.56,0.54,0.52,0.489,0.430,0.38,0.35,0.300,0.25,0.2,0.150,0.1
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};
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rudderInfluence=0.95;
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rudderCoef[]=
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{
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0.00,0.89,1.50,2.10,2.50,3.00,3.60,3.90,4.00,3.60,1.80
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};
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aileronControlsSensitivityCoef= 3.6;
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elevatorControlsSensitivityCoef=2.0;
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rudderControlsSensitivityCoef=3.8;
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draconicForceXCoef=12.0;
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draconicForceYCoef=1.0;
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draconicForceZCoef=1.0;
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draconicTorqueXCoef[]=
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{
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4.8,5,5.5,6.2,7,7.7,9.4,11.1,12,14,15
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};
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draconicTorqueYCoef[] =
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{
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12,10,6,2,0.2,0,0,0,0,0,0,0,0,0,0,0,0
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}; |