mirror of
https://github.com/acemod/ACE3.git
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Optimized range card calculations
* Removed dead code
This commit is contained in:
ulteq
ulteq
parent
69cd53de2a
commit
16f3f2ca37
@ -1,5 +1,5 @@
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PREP(calculateSolution);
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PREP(calculateRangeCard);
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PREP(canCopy);
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PREP(canCopy);
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PREP(canShow);
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PREP(canShow);
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PREP(canShowCopy);
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PREP(canShowCopy);
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151
addons/rangecard/functions/fnc_calculateRangeCard.sqf
Normal file
151
addons/rangecard/functions/fnc_calculateRangeCard.sqf
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@ -0,0 +1,151 @@
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/*
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* Author: Ruthberg
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* Calculates the range card data
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*
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* Arguments:
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* 0: Scope base angle <NUMBER>
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* 1: Bore height <NUMBER>
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* 2: air friction <NUMBER>
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* 3: muzzle velocity <NUMBER>
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* 4: temperature <NUMBER>
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* 5: barometric pressure <NUMBER>
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* 6: relative humidity <NUMBER>
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* 7: simulation steps <NUMBER>
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* 8: wind speed <NUMBER>
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* 9: target speed <NUMBER>
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* 10: target range <NUMBER>
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* 11: ballistic coefficient <NUMBER>
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* 12: drag model <NUMBER>
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* 13: atmosphere model <STRING>
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* 14: Range Card Slot <NUMBER>
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* 15: Use advanced ballistics config? <BOOL>
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*
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* Return Value:
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* Nothing
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*
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* Example:
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* call ace_rangecard_fnc_calculateRangeCard
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*
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* Public: No
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*/
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#include "script_component.hpp"
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params [
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"_scopeBaseAngle", "_boreHeight", "_airFriction", "_muzzleVelocity",
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"_temperature", "_barometricPressure", "_relativeHumidity", "_simSteps",
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"_windSpeed", "_targetSpeed", "_targetRange", "_bc", "_dragModel", "_atmosphereModel",
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"_rangeCardSlot", "_useABConfig"
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];
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GVAR(rangeCardDataMVs) set [_rangeCardSlot, format[" %1", round(_muzzleVelocity)]];
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private ["_tx", "_tz", "_lastBulletPos", "_bulletPos", "_bulletVelocity", "_bulletAccel", "_bulletSpeed", "_gravity", "_deltaT", "_speedOfSound"];
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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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_bulletVelocity = [0, 0, 0];
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_bulletAccel = [0, 0, 0];
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_bulletSpeed = 0;
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_gravity = [0, sin(_scopeBaseAngle) * -9.80665, cos(_scopeBaseAngle) * -9.80665];
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_deltaT = 1 / _simSteps;
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_speedOfSound = 0;
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if (missionNamespace getVariable [QEGVAR(advanced_ballistics,enabled), false]) then {
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_speedOfSound = _temperature call EFUNC(weather,calculateSpeedOfSound);
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};
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private ["_elevation", "_windage", "_lead", "_TOF", "_trueVelocity", "_trueSpeed"];
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_elevation = 0;
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_windage = 0;
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_lead = 0;
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_TOF = 0;
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_trueVelocity = [0, 0, 0];
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_trueSpeed = 0;
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private ["_n", "_range"];
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_n = 0;
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_range = 0;
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if (_useABConfig) then {
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_bc = parseNumber(("ace_advanced_ballistics" callExtension format["atmosphericCorrection:%1:%2:%3:%4:%5", _bc, _temperature, _barometricPressure, _relativeHumidity, _atmosphereModel]));
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};
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private ["_airFrictionCoef", "_airDensity"];
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_airFrictionCoef = 1;
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if (!_useABConfig && (missionNamespace getVariable [QEGVAR(advanced_ballistics,enabled), false])) then {
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_airDensity = [_temperature, _barometricPressure, _relativeHumidity] call EFUNC(weather,calculateAirDensity);
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_airFrictionCoef = _airDensity / 1.22498;
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};
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private ["_speedTotal", "_stepsTotal", "_speedAverage"];
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_speedTotal = 0;
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_stepsTotal = 0;
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_speedAverage = 0;
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_bulletPos set [0, 0];
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_bulletPos set [1, 0];
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_bulletPos set [2, -(_boreHeight / 100)];
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_bulletVelocity set [0, 0];
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_bulletVelocity set [1, Cos(_scopeBaseAngle) * _muzzleVelocity];
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_bulletVelocity set [2, Sin(_scopeBaseAngle) * _muzzleVelocity];
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while {_TOF < 6 && (_bulletPos select 1) < _targetRange} do {
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_bulletSpeed = vectorMagnitude _bulletVelocity;
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_speedTotal = _speedTotal + _bulletSpeed;
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_stepsTotal = _stepsTotal + 1;
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_speedAverage = (_speedTotal / _stepsTotal);
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if (_speedAverage > 450 && _bulletSpeed < _speedOfSound) exitWith {};
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if (atan((_bulletPos select 2) / (abs(_bulletPos select 1) + 1)) < -2.254) exitWith {};
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_trueVelocity = _bulletVelocity vectorDiff [-_windSpeed, 0, 0];
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_trueSpeed = vectorMagnitude _trueVelocity;
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if (_useABConfig) then {
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private _drag = parseNumber(("ace_advanced_ballistics" callExtension format["retard:%1:%2:%3", _dragModel, _bc, _trueSpeed]));
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_bulletAccel = (vectorNormalized _trueVelocity) vectorMultiply (-1 * _drag);
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} else {
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_bulletAccel = _trueVelocity vectorMultiply (_trueSpeed * _airFriction * _airFrictionCoef);
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};
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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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_bulletPos = _bulletPos vectorAdd (_bulletVelocity vectorMultiply (_deltaT * 0.5));
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_TOF = _TOF + _deltaT;
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_range = GVAR(rangeCardStartRange) + _n * GVAR(rangeCardIncrement);
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if ((_bulletPos select 1) >= _range && _range <= GVAR(rangeCardEndRange)) then {
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if (_range != 0) then {
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_tx = (_lastBulletPos select 0) + (_range - (_lastBulletPos select 1)) * ((_bulletPos select 0) - (_lastBulletPos select 0)) / ((_bulletPos select 1) - (_lastBulletPos select 1));
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_tz = (_lastBulletPos select 2) + (_range - (_lastBulletPos select 1)) * ((_bulletPos select 2) - (_lastBulletPos select 2)) / ((_bulletPos select 1) - (_lastBulletPos select 1));
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_elevation = - atan(_tz / _range);
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_windage = - atan(_tx / _range);
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_lead = (_targetSpeed * _TOF) / (Tan(3.38 / 60) * _range);
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};
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private ["_elevationString", "_windageString", "_leadString"];
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_elevationString = Str(round(-_elevation * 60 / 3.38 * 10) / 10);
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if (_elevationString == "0") then {
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_elevationString = "-0.0";
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};
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if (_elevationString find "." == -1) then {
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_elevationString = _elevationString + ".0";
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};
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_windageString = Str(round(_windage * 60 / 3.38 * 10) / 10);
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if (_windageString find "." == -1) then {
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_windageString = _windageString + ".0";
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};
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_leadString = Str(round(_lead * 10) / 10);
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if (_leadString find "." == -1) then {
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_leadString = _leadString + ".0";
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};
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(GVAR(rangeCardDataElevation) select _rangeCardSlot) set [_n, _elevationString];
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(GVAR(rangeCardDataWindage) select _rangeCardSlot) set [_n, _windageString];
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(GVAR(rangeCardDataLead) select _rangeCardSlot) set [_n, _leadString];
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_n = _n + 1;
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};
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};
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@ -1,195 +0,0 @@
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/*
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* Author: Ruthberg
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* Calculates the range card data
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*
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* Arguments:
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* 0: Scope base angle <NUMBER>
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* 1: Bullet mass <NUMBER>
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* 2: Bore height <NUMBER>
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* 3: air friction <NUMBER>
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* 4: muzzle velocity <NUMBER>
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* 5: temperature <NUMBER>
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* 6: barometric pressure <NUMBER>
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* 7: relative humidity <NUMBER>
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* 8: simulation steps <NUMBER>
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* 9: wind speed <ARRAY>
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* 10: wind direction <NUMBER>
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* 11: inclination angle <NUMBER>
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* 12: target speed <NUMBER>
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* 13: target range <NUMBER>
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* 14: ballistic coefficient <NUMBER>
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* 15: drag model <NUMBER>
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* 16: atmosphere model <STRING>
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* 17: Store range card data? <BOOL>
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* 18: Stability factor <NUMBER>
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* 19: Twist Direction <NUMBER>
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* 20: Latitude <NUMBER>
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* 21: Direction of Fire <NUMBER>
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* 22: Range Card Slot <NUMBER>
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* 23: Use advanced ballistics config? <BOOL>
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*
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* Return Value:
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* 0: Elevation (MOA) <NUMBER>
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* 1: Windage (MOA) <ARRAY>
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* 2: Lead (MOA) <NUMBER>
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* 3: Time of fligth (SECONDS) <NUMBER>
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* 4: Remaining velocity (m/s) <NUMBER>
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* 5: Remaining kinetic energy (ft·lb) <NUMBER>
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* 6: Vertical coriolis drift (MOA) <NUMBER>
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* 7: Horizontal coriolis drift (MOA) <NUMBER>
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* 8: Spin drift (MOA) <NUMBER>
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*
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* Example:
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* call ace_rangecard_fnc_calculateSolution
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*
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* Public: No
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*/
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#include "script_component.hpp"
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params [
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"_scopeBaseAngle", "_bulletMass", "_boreHeight", "_airFriction", "_muzzleVelocity",
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"_temperature", "_barometricPressure", "_relativeHumidity", "_simSteps", "_windSpeed",
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"_windDirection", "_inclinationAngle", "_targetSpeed", "_targetRange", "_bc", "_dragModel",
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"_atmosphereModel", "_storeRangeCardData", "_stabilityFactor", "_twistDirection", "_latitude",
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"_directionOfFire", "_rangeCardSlot", "_useABConfig"
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];
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_windSpeed params ["_windSpeed1", "_windSpeed2"];
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if (_storeRangeCardData) then {
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GVAR(rangeCardDataMVs) set [_rangeCardSlot, format[" %1", round(_muzzleVelocity)]];
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};
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private ["_bulletPos", "_bulletVelocity", "_bulletAccel", "_bulletSpeed", "_gravity", "_deltaT", "_speedOfSound"];
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_bulletPos = [0, 0, 0];
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_bulletVelocity = [0, 0, 0];
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_bulletAccel = [0, 0, 0];
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_bulletSpeed = 0;
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_gravity = [0, sin(_scopeBaseAngle + _inclinationAngle) * -9.80665, cos(_scopeBaseAngle + _inclinationAngle) * -9.80665];
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_deltaT = 1 / _simSteps;
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_speedOfSound = 0;
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if (missionNamespace getVariable [QEGVAR(advanced_ballistics,enabled), false]) then {
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_speedOfSound = _temperature call EFUNC(weather,calculateSpeedOfSound);
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};
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private ["_elevation", "_windage1", "_windage2", "_lead", "_TOF", "_trueVelocity", "_trueSpeed", "_kineticEnergy", "_verticalCoriolis", "_verticalDeflection", "_horizontalCoriolis", "_horizontalDeflection", "_spinDrift", "_spinDeflection"];
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_elevation = 0;
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_windage1 = 0;
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_windage2 = 0;
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_lead = 0;
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_TOF = 0;
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_trueVelocity = [0, 0, 0];
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_trueSpeed = 0;
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_verticalCoriolis = 0;
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_verticalDeflection = 0;
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_horizontalCoriolis = 0;
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_horizontalDeflection = 0;
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_spinDrift = 0;
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_spinDeflection = 0;
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private ["_n", "_range"];
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_n = 0;
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_range = 0;
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private ["_wind1", "_wind2", "_windDrift"];
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_wind1 = [cos(270 - _windDirection * 30) * _windSpeed1, sin(270 - _windDirection * 30) * _windSpeed1, 0];
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_wind2 = [cos(270 - _windDirection * 30) * _windSpeed2, sin(270 - _windDirection * 30) * _windSpeed2, 0];
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_windDrift = 0;
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if (_useABConfig) then {
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_bc = parseNumber(("ace_advanced_ballistics" callExtension format["atmosphericCorrection:%1:%2:%3:%4:%5", _bc, _temperature, _barometricPressure, _relativeHumidity, _atmosphereModel]));
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};
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private ["_airFrictionCoef", "_airDensity"];
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_airFrictionCoef = 1;
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if (!_useABConfig && (missionNamespace getVariable [QEGVAR(advanced_ballistics,enabled), false])) then {
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_airDensity = [_temperature, _barometricPressure, _relativeHumidity] call EFUNC(weather,calculateAirDensity);
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_airFrictionCoef = _airDensity / 1.22498;
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};
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private ["_speedTotal", "_stepsTotal", "_speedAverage"];
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_speedTotal = 0;
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_stepsTotal = 0;
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_speedAverage = 0;
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_bulletPos set [0, 0];
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_bulletPos set [1, 0];
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_bulletPos set [2, -(_boreHeight / 100)];
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_bulletVelocity set [0, 0];
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_bulletVelocity set [1, Cos(_scopeBaseAngle) * _muzzleVelocity];
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_bulletVelocity set [2, Sin(_scopeBaseAngle) * _muzzleVelocity];
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while {_TOF < 6 && (_bulletPos select 1) < _targetRange} do {
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_bulletSpeed = vectorMagnitude _bulletVelocity;
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_speedTotal = _speedTotal + _bulletSpeed;
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_stepsTotal = _stepsTotal + 1;
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_speedAverage = (_speedTotal / _stepsTotal);
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if (_speedAverage > 450 && _bulletSpeed < _speedOfSound) exitWith {};
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if (atan((_bulletPos select 2) / (abs(_bulletPos select 1) + 1)) < -2.254) exitWith {};
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_trueVelocity = _bulletVelocity vectorDiff _wind1;
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_trueSpeed = vectorMagnitude _trueVelocity;
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if (_useABConfig) then {
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private _drag = parseNumber(("ace_advanced_ballistics" callExtension format["retard:%1:%2:%3", _dragModel, _bc, _trueSpeed]));
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_bulletAccel = (vectorNormalized _trueVelocity) vectorMultiply (-1 * _drag);
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} else {
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_bulletAccel = _trueVelocity vectorMultiply (_trueSpeed * _airFriction * _airFrictionCoef);
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};
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_bulletAccel = _bulletAccel vectorAdd _gravity;
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_bulletVelocity = _bulletVelocity vectorAdd (_bulletAccel vectorMultiply _deltaT);
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_bulletPos = _bulletPos vectorAdd (_bulletVelocity vectorMultiply _deltaT);
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_TOF = _TOF + _deltaT;
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if (_storeRangeCardData) then {
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_range = GVAR(rangeCardStartRange) + _n * GVAR(rangeCardIncrement);
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if ((_bulletPos select 1) >= _range && _range <= GVAR(rangeCardEndRange)) then {
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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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};
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if (_range != 0) then {
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_lead = (_targetSpeed * _TOF) / (Tan(3.38 / 60) * _range);
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};
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private ["_elevationString", "_windageString", "_leadString"];
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_elevationString = Str(round(-_elevation * 60 / 3.38 * 10) / 10);
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if (_elevationString == "0") then {
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_elevationString = "-0.0";
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};
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if (_elevationString find "." == -1) then {
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_elevationString = _elevationString + ".0";
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};
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_windageString = Str(round(_windage1 * 60 / 3.38 * 10) / 10);
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if (_windageString find "." == -1) then {
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_windageString = _windageString + ".0";
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};
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_leadString = Str(round(_lead * 10) / 10);
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if (_leadString find "." == -1) then {
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_leadString = _leadString + ".0";
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};
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(GVAR(rangeCardDataElevation) select _rangeCardSlot) set [_n, _elevationString];
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(GVAR(rangeCardDataWindage) select _rangeCardSlot) set [_n, _windageString];
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(GVAR(rangeCardDataLead) select _rangeCardSlot) set [_n, _leadString];
|
|
||||||
_n = _n + 1;
|
|
||||||
};
|
|
||||||
};
|
|
||||||
};
|
|
||||||
|
|
||||||
if ((_bulletPos select 1) > 0) then {
|
|
||||||
_elevation = - atan((_bulletPos select 2) / (_bulletPos select 1));
|
|
||||||
_windage1 = - atan((_bulletPos select 0) / (_bulletPos select 1));
|
|
||||||
_windDrift = (_wind2 select 0) * (_TOF - _targetRange / _muzzleVelocity);
|
|
||||||
_windage2 = - atan(_windDrift / (_bulletPos select 1));
|
|
||||||
};
|
|
||||||
|
|
||||||
if (_targetRange != 0) then {
|
|
||||||
_lead = (_targetSpeed * _TOF) / (Tan(3.38 / 60) * _targetRange);
|
|
||||||
};
|
|
||||||
|
|
||||||
_kineticEnergy = 0.5 * (_bulletMass / 1000 * (_bulletSpeed ^ 2));
|
|
||||||
_kineticEnergy = _kineticEnergy * 0.737562149;
|
|
||||||
|
|
||||||
[_elevation * 60, [_windage1 * 60, _windage2 * 60], _lead, _TOF, _bulletSpeed, _kineticEnergy, _verticalCoriolis * 60, _horizontalCoriolis * 60, _spinDrift * 60]
|
|
||||||
@ -170,10 +170,10 @@ if (isNil {_cacheEntry}) then {
|
|||||||
private _mvShift = [_ammoConfig select 9, _x] call EFUNC(advanced_ballistics,calculateAmmoTemperatureVelocityShift);
|
private _mvShift = [_ammoConfig select 9, _x] call EFUNC(advanced_ballistics,calculateAmmoTemperatureVelocityShift);
|
||||||
private _mv = _muzzleVelocity + _mvShift;
|
private _mv = _muzzleVelocity + _mvShift;
|
||||||
|
|
||||||
[_scopeBaseAngle,0,_boreHeight,_airFriction,_mv,_x,EGVAR(scopes,zeroReferenceBarometricPressure),EGVAR(scopes,zeroReferenceHumidity),1000,[4,0],3,0,1,GVAR(rangeCardEndRange),_bc,_dragModel,_atmosphereModel,true,1.5,1,46,23,_forEachIndex,_useABConfig] call FUNC(calculateSolution);
|
[_scopeBaseAngle,_boreHeight,_airFriction,_mv,_x,EGVAR(scopes,zeroReferenceBarometricPressure),EGVAR(scopes,zeroReferenceHumidity),100,4,1,GVAR(rangeCardEndRange),_bc,_dragModel,_atmosphereModel,_forEachIndex,_useABConfig] call FUNC(calculateRangeCard);
|
||||||
} forEach [-15, -5, 5, 10, 15, 20, 25, 30, 35];
|
} forEach [-15, -5, 5, 10, 15, 20, 25, 30, 35];
|
||||||
} else {
|
} else {
|
||||||
[_scopeBaseAngle,0,_boreHeight,_airFriction,_muzzleVelocity,15,EGVAR(scopes,zeroReferenceBarometricPressure),EGVAR(scopes,zeroReferenceHumidity),1000,[4,0],3,0,1,GVAR(rangeCardEndRange),_bc,_dragModel,_atmosphereModel,true,1.5,1,46,23,4,_useABConfig] call FUNC(calculateSolution);
|
[_scopeBaseAngle,_boreHeight,_airFriction,_muzzleVelocity,15,EGVAR(scopes,zeroReferenceBarometricPressure),EGVAR(scopes,zeroReferenceHumidity),100,4,1,GVAR(rangeCardEndRange),_bc,_dragModel,_atmosphereModel,4,_useABConfig] call FUNC(calculateRangeCard);
|
||||||
};
|
};
|
||||||
|
|
||||||
for "_i" from 0 to 9 do {
|
for "_i" from 0 to 9 do {
|
||||||
|
|||||||
Loading…
Reference in New Issue
Block a user