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Optimized ATragMX solution calculations
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@ -71,5 +71,5 @@ if (GVAR(currentUnit) == 1) then {
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GVAR(rangeCardData) = [];
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GVAR(rangeCardData) = [];
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private _result = [_scopeBaseAngle, _bulletMass, _boreHeight, _airFriction, _muzzleVelocity, _temperature, _barometricPressure, _relativeHumidity, 1000,
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private _result = [_scopeBaseAngle, _bulletMass, _boreHeight, _airFriction, _muzzleVelocity, _temperature, _barometricPressure, _relativeHumidity, 100,
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[_windSpeed1, _windSpeed2], _windDirection, _inclinationAngle, _targetSpeed, _targetRange, _bc, _dragModel, _atmosphereModel, true, _stabilityFactor, _twistDirection, _latitude, _directionOfFire] call FUNC(calculate_solution);
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[_windSpeed1, _windSpeed2], _windDirection, _inclinationAngle, _targetSpeed, _targetRange, _bc, _dragModel, _atmosphereModel, true, _stabilityFactor, _twistDirection, _latitude, _directionOfFire] call FUNC(calculate_solution);
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@ -51,7 +51,10 @@ params [
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];
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];
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_windSpeed params ["_windSpeed1", "_windSpeed2"];
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_windSpeed params ["_windSpeed1", "_windSpeed2"];
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private ["_bulletPos", "_bulletVelocity", "_bulletAccel", "_bulletSpeed", "_gravity", "_deltaT"];
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private ["_tx", "_tz", "_lastBulletPos", "_bulletPos", "_bulletVelocity", "_bulletAccel", "_bulletSpeed", "_gravity", "_deltaT"];
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_tx = 0;
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_tz = 0;
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_lastBulletPos = [0, 0, 0];
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_bulletPos = [0, 0, 0];
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_bulletPos = [0, 0, 0];
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_bulletVelocity = [0, 0, 0];
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_bulletVelocity = [0, 0, 0];
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_bulletAccel = [0, 0, 0];
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_bulletAccel = [0, 0, 0];
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@ -74,9 +77,10 @@ _horizontalDeflection = 0;
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_spinDrift = 0;
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_spinDrift = 0;
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_spinDeflection = 0;
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_spinDeflection = 0;
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private ["_n", "_range", "_rangeFactor"];
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private ["_n", "_range", "_trueRange", "_rangeFactor"];
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_n = 0;
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_n = 0;
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_range = 0;
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_range = 0;
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_trueRange = 0;
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_rangeFactor = 1;
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_rangeFactor = 1;
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if (_storeRangeCardData) then {
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if (_storeRangeCardData) then {
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if (GVAR(currentUnit) == 1) then {
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if (GVAR(currentUnit) == 1) then {
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@ -133,22 +137,25 @@ while {_TOF < 15 && (_bulletPos select 1) < _targetRange} do {
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_bulletAccel = _bulletAccel vectorAdd _gravity;
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_bulletAccel = _bulletAccel vectorAdd _gravity;
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_lastBulletPos = _bulletPos;
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_bulletPos = _bulletPos vectorAdd (_bulletVelocity vectorMultiply (_deltaT * 0.5));
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_bulletVelocity = _bulletVelocity vectorAdd (_bulletAccel vectorMultiply _deltaT);
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_bulletVelocity = _bulletVelocity vectorAdd (_bulletAccel vectorMultiply _deltaT);
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_bulletPos = _bulletPos vectorAdd (_bulletVelocity vectorMultiply _deltaT);
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_bulletPos = _bulletPos vectorAdd (_bulletVelocity vectorMultiply (_deltaT * 0.5));
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_TOF = _TOF + _deltaT;
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_TOF = _TOF + _deltaT;
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if (_storeRangeCardData) then {
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if (_storeRangeCardData) then {
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_range = GVAR(rangeCardStartRange) + _n * GVAR(rangeCardIncrement);
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_range = GVAR(rangeCardStartRange) + _n * GVAR(rangeCardIncrement);
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if ((_bulletPos select 1) * _rangeFactor >= _range && _range <= GVAR(rangeCardEndRange)) then {
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if ((_bulletPos select 1) * _rangeFactor >= _range && _range <= GVAR(rangeCardEndRange)) then {
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if ((_bulletPos select 1) > 0) then {
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_trueRange = _range / _rangeFactor;
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_elevation = - atan((_bulletPos select 2) / (_bulletPos select 1));
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if (_trueRange != 0) then {
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_windage1 = - atan((_bulletPos select 0) / (_bulletPos select 1));
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_tx = (_lastBulletPos select 0) + (_trueRange - (_lastBulletPos select 1)) * ((_bulletPos select 0) - (_lastBulletPos select 0)) / ((_bulletPos select 1) - (_lastBulletPos select 1));
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_windDrift = (_wind2 select 0) * (_TOF - (_range / _rangeFactor) / _muzzleVelocity);
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_tz = (_lastBulletPos select 2) + (_trueRange - (_lastBulletPos select 1)) * ((_bulletPos select 2) - (_lastBulletPos select 2)) / ((_bulletPos select 1) - (_lastBulletPos select 1));
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_windage2 = - atan(_windDrift / (_bulletPos select 1));
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_elevation = - atan(_tz / _trueRange);
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};
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_windage1 = - atan(_tx / _trueRange);
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if (_range != 0) then {
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_windDrift = (_wind2 select 0) * (_TOF - _trueRange / _muzzleVelocity);
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_lead = (_targetSpeed * _TOF) / (Tan(3.38 / 60) * _range);
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_windage2 = - atan(_windDrift / _trueRange);
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_lead = (_targetSpeed * _TOF) / (Tan(3.38 / 60) * _trueRange);
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};
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};
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_kineticEnergy = 0.5 * (_bulletMass / 1000 * (_bulletSpeed ^ 2));
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_kineticEnergy = 0.5 * (_bulletMass / 1000 * (_bulletSpeed ^ 2));
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_kineticEnergy = _kineticEnergy * 0.737562149;
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_kineticEnergy = _kineticEnergy * 0.737562149;
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@ -176,14 +183,13 @@ while {_TOF < 15 && (_bulletPos select 1) < _targetRange} do {
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};
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};
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};
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};
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if ((_bulletPos select 1) > 0) then {
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_elevation = - atan((_bulletPos select 2) / (_bulletPos select 1));
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_windage1 = - atan((_bulletPos select 0) / (_bulletPos select 1));
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_windDrift = (_wind2 select 0) * (_TOF - _targetRange / _muzzleVelocity);
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_windage2 = - atan(_windDrift / (_bulletPos select 1));
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};
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if (_targetRange != 0) then {
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if (_targetRange != 0) then {
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_tx = (_lastBulletPos select 0) + (_targetRange - (_lastBulletPos select 1)) * ((_bulletPos select 0) - (_lastBulletPos select 0)) / ((_bulletPos select 1) - (_lastBulletPos select 1));
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_tz = (_lastBulletPos select 2) + (_targetRange - (_lastBulletPos select 1)) * ((_bulletPos select 2) - (_lastBulletPos select 2)) / ((_bulletPos select 1) - (_lastBulletPos select 1));
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_elevation = - atan(_tz / _targetRange);
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_windage1 = - atan(_tx / _targetRange);
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_windDrift = (_wind2 select 0) * (_TOF - _targetRange / _muzzleVelocity);
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_windage2 = - atan(_windDrift / _targetRange);
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_lead = (_targetSpeed * _TOF) / (Tan(3.38 / 60) * _targetRange);
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_lead = (_targetSpeed * _TOF) / (Tan(3.38 / 60) * _targetRange);
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};
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};
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@ -70,7 +70,7 @@ _inclinationAngle = GVAR(inclinationAngle) select GVAR(currentTarget);
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_targetSpeed = GVAR(targetSpeed) select GVAR(currentTarget);
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_targetSpeed = GVAR(targetSpeed) select GVAR(currentTarget);
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_targetRange = GVAR(targetRange) select GVAR(currentTarget);
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_targetRange = GVAR(targetRange) select GVAR(currentTarget);
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GVAR(targetSolutionInput) = [_scopeBaseAngle, _bulletMass, _boreHeight, _airFriction, _muzzleVelocity, _temperature, _barometricPressure, _relativeHumidity, 1000,
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GVAR(targetSolutionInput) = [_scopeBaseAngle, _bulletMass, _boreHeight, _airFriction, _muzzleVelocity, _temperature, _barometricPressure, _relativeHumidity, 100,
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[_windSpeed1, _windSpeed2], _windDirection, _inclinationAngle, _targetSpeed, _targetRange, _bc, _dragModel, _atmosphereModel, false, _stabilityFactor, _twistDirection, _latitude, _directionOfFire];
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[_windSpeed1, _windSpeed2], _windDirection, _inclinationAngle, _targetSpeed, _targetRange, _bc, _dragModel, _atmosphereModel, false, _stabilityFactor, _twistDirection, _latitude, _directionOfFire];
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private _result = GVAR(targetSolutionInput) call FUNC(calculate_solution);
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private _result = GVAR(targetSolutionInput) call FUNC(calculate_solution);
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