maxSpeed = 1059;
acceleration = 300;
aileronSensitivity = 0.635;
elevatorSensitivity = 0.814;
rudderInfluence = 0.001;
aileronControlsSensitivityCoef = 3;
elevatorControlsSensitivity = 2;
rudderControlsSensitivityoef = 4;
elevatorCoef[] = {0.6,0.76,0.7,0.65,0.58,0.47,0.43};
aileronCoef[] = {0.5,0.85,0.87,0.89,0.92,0.95,1};
rudderCoef[] = {0.8,0.7,0.6,0.5,0.4,0.32,0.27};
angleOfIndicence = 0.0523599;
draconicForceXCoef = 7.6;
draconicForceYCoef = 0.75;
draconicForceZCoef = 0.085;
draconicTorqueXCoef = 0.815;
draconicTorqueYCoef = 0.000152;
envelope[] = {0,0.446,1.5,3.9,5.2,4.8,4.2,3.5,2,1,0.5};
thrustCoef[] = {1,1.2,1.7,1.7,1.65,1.54,1.32,1.1,0.95,0.75,0.5,0.35,0};
flapsFrictionCoef = 0.32;