This commit is the equivalent of a atomic bomb

source/braf_air2/braf_casa/flightModel.hpp

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+// GENERAL
+maxSpeed					= 450; // flight behavior arrays are dependable on this value
+acceleration 				= 300;
+
+landingAoa					= 6*3.1415/180; // landing angle of attack in radians, for AI
+landingSpeed				= 215; // for AI to approach the runawy, the plane should be stable at this speed
+
+stallSpeed					= 190;
+stallWarningTreshold		= 0.1;
+
+wheelSteeringSensitivity	= 2.0; // steering authority of the nose wheel
+
+airBrake 					= 1;
+airBrakeFrictionCoef 		= 2.2;
+flaps						= 1;
+flapsFrictionCoef 			= 0.32;
+gearsUpFrictionCoef 		= 0.6;
+
+airFrictionCoefs0[] 		= { 0.0, 0.0, 0.0 };
+airFrictionCoefs1[] 		= { 0.1, 0.5, 0.0066 };
+airFrictionCoefs2[] 		= { 0.001, 0.005, 0.000068};
+
+angleOfIndicence			= -2*3.1415/180; // difference between forward and airfold chord line in radians
+envelope[] =
+{
+	0.0,	// 0
+	0.05,	// 50
+	0.2,	// 100
+	0.46,	// 150
+	0.82,	// 200
+	1.28,	// 250
+	1.84,	// 300
+	2.4,	// 350
+	2.88,	// 400
+	3.65,	// 450
+	4.5,	// 500
+	5.45,	// 550
+	6.48,	// 600
+	7.61,	// 650
+	8.1,	// 700
+	8.3,	// 750
+	8.4,	// 800
+	8.3,	// 850
+	8.0,	// 900
+	7.6,	// 950
+	7.0		// 1000
+};
+
+// THRUST
+altNoForce				= 13000;
+altFullForce			= 2000;
+thrustCoef[]			=
+{	//		 fSpeed = maxI * speedRel; speedRel = speed / (maxSpeed * 1.5f); maxI = _thrustCoef.Size() - 1;
+	1.42,	// 0
+	1.38,	// 75
+	1.34,	// 150
+	1.30,	// 225
+	1.25,	// 300
+	1.20,	// 375
+	1.19,	// 450
+	1.18,	// 525
+	1.17,	// 600
+	1.17,	// 675
+	1.16,	// 750
+	1.16,	// 825
+	0.1,	// 900
+	0.0,	// 975
+	0.0,	// 1050
+	0.0,	// 1125
+	0.0		// 1200
+};
+
+// CONTROL SURFACES
+aileronSensitivity		= 0.5;
+/* ---------------------------------
+aileronCoef[]			=
+{
+	0.0,	// 0
+	0.11,	// 75
+	0.45,	// 150
+	0.81,	// 225
+	1.1,	// 300
+	1.15,	// 375
+	1.2,	// 450
+	1.25,	// 525
+	1.3,	// 600
+	1.35,	// 675
+	1.4,	// 750
+	1.43,	// 825
+	1.45,	// 900
+	1.47,	// 975
+	1.4,	// 1050
+	1.2,	// 1125
+	0.8		// 1200
+};
+----------------------------- */
+aileronCoef[]={0,0.5,0.89999998,1,1.05,1.1,1.12};
+
+elevatorSensitivity		= 1.6;
+elevatorCoef[]			=
+{
+	0.0,	// 0
+	0.14,	// 75
+	0.54,	// 150
+	0.62,	// 225
+	0.58,	// 300
+	0.56,	// 375
+	0.54,	// 450
+	0.52,	// 525
+	0.48,	// 600
+	0.43,	// 675
+	0.38,	// 750
+	0.35,	// 825
+	0.3,	// 900
+	0.25,	// 975
+	0.2,	// 1050
+	0.15,	// 1125
+	0.1		// 1200
+};
+
+
+rudderInfluence			= 0.8660; 	// Basic angle (cos angle) of the rudder extent
+rudderCoef[]			=	 		// default value is fabs(speed.Z())*InvSqrt(Square(speed.X())+Square(speed.Z()));
+{
+	0.0,	// 0
+	0.8,	// 120
+	2.0,	// 240
+	2.2,	// 360
+	2.3,	// 480
+	2.4,	// 600
+	2.3,	// 720
+	2.2,	// 840
+	2.1,	// 960
+	2.0,	// 1080
+	1.2	// 1200
+};
+
+// CONTROLS - sensitivity/speed in which control surface reaches its maximum extent
+aileronControlsSensitivityCoef		= 3.6;	// default value is 4
+elevatorControlsSensitivityCoef	 = 3.4;	// default value is 4
+rudderControlsSensitivityCoef		= 3.8;	// default value is 4
+
+// FORCES - how good the airplane changes the flight vector or alignes with it
+draconicForceXCoef	  = 8.0; //7.5
+draconicForceYCoef	  = 1.4; //1
+draconicForceZCoef	  = 1.0; //1
+draconicTorqueXCoef[] =
+{
+	4.8,	// 0
+	5.0,	// 120
+	5.5,	// 240
+	6.2,	// 360
+	7.0,	// 480
+	7.7,	// 600
+	9.4,	// 720
+	11.1,	// 840
+	12.0,	// 960
+	14.0,	// 1080
+	15.0	// 1200
+};
+draconicTorqueYCoef[] =
+{
+	12.0,	// 0
+	10.0,	// 75
+	6.0,	// 150
+	2.0,	// 225
+	0.2,	// 300
+	0.0,	// 375
+	0.0,	// 450
+	0.0,	// 525
+	0.0,	// 600
+	0.0,	// 675
+	0.0,	// 750
+	0.0,	// 825
+	0.0,	// 900
+	0.0,	// 975
+	0.0,	// 1050
+	0.0,	// 1125
+	0.0		// 1200
+};
+
+// VTOL - behavior while vectoring
+// VTOLYawInfluence = 1.0;
+// VTOLPitchInfluence = 1.0;
+// VTOLRollInfluence = 1.0;