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;