maxSpeed = 736;
aileronSensitivity = 0.85;
elevatorSensitivity = 0.75;
rudderInfluence = 0.001;
aileronControlsSensitivityCoef = 3;
elevatorControlsSensitivity = 2;
rudderControlsSensitivityoef = 4;
elevatorCoef[] = {0.7, 0.75, 0.75, 0.65, 0.55, 0.45, 0.35};
aileronCoef[] = {0.6, 0.85, 0.88, 0.92, 0.95, 0.97, 1};
rudderCoef[] = {0.8, 0.75, 0.65, 0.5, 0.4, 0.33, 0.3};
flapsFrictionCoef = 0.35;
angleOfIndicence = 0.0523599;
draconicForceXCoef = 9.5;
draconicForceYCoef = 0.56;
draconicForceZCoef = 0.1;
draconicTorqueXCoef = 0.58;
draconicTorqueYCoef = 0.00013;
envelope[] = {0, 0, 0.75, 2.4, 3.6, 3.8, 3.7, 3.2, 2.2, 1.7, 0.9};
thrustCoef[] = {1, 1.2, 1.3, 1.25, 1.06, 1.01, 1, 0.92, 0.75, 0.65, 0.5, 0.25, 0};
acceleration = 265;
landingSpeed = 220;