ACE3/addons/missileguidance/functions/fnc_guidancePFH.sqf
2021-03-31 17:16:00 -06:00

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#include "script_component.hpp"
/*
* Author: jaynus / nou
* Guidance Per Frame Handler
*
* Arguments:
* 0: Guidance Arg Array <ARRAY>
* 1: PFID <NUMBER>
*
* Return Value:
* None
*
* Example:
* [[], 0] call ace_missileguidance_fnc_guidancePFH;
*
* Public: No
*/
BEGIN_COUNTER(guidancePFH);
#define TIMESTEP_FACTOR 0.01
params ["_args", "_pfID"];
_args params ["_firedEH", "_launchParams", "_flightParams", "_seekerParams", "_stateParams"];
_firedEH params ["_shooter","","","","_ammo","","_projectile"];
_launchParams params ["","_targetLaunchParams"];
_stateParams params ["_lastRunTime", "_seekerStateParams", "_attackProfileStateParams", "_lastKnownPosState", "_pidData"];
if (!alive _projectile || isNull _projectile || isNull _shooter) exitWith {
[_pfID] call CBA_fnc_removePerFrameHandler;
END_COUNTER(guidancePFH);
};
private _runtimeDelta = diag_tickTime - _lastRunTime;
private _adjustTime = 1;
if (accTime > 0) then {
_adjustTime = 1/accTime;
_adjustTime = _adjustTime * (_runtimeDelta / TIMESTEP_FACTOR);
TRACE_4("Adjust timing", 1/accTime, _adjustTime, _runtimeDelta, (_runtimeDelta / TIMESTEP_FACTOR) );
} else {
_adjustTime = 0;
};
private _minDeflection = ((_flightParams select 0) - ((_flightParams select 0) * _adjustTime)) max 0;
private _maxDeflection = (_flightParams select 1) * _adjustTime;
// private _incDeflection = _flightParams select 2; // todo
private _projectilePos = getPosASLVisual _projectile;
// Run seeker function:
private _seekerTargetPos = [[0,0,0], _args, _seekerStateParams, _lastKnownPosState] call FUNC(doSeekerSearch);
// Run attack profile function:
private _profileAdjustedTargetPos = [_seekerTargetPos, _args, _attackProfileStateParams] call FUNC(doAttackProfile);
// If we have no seeker target, then do not change anything
// If there is no deflection on the missile, this cannot change and therefore is redundant. Avoid calculations for missiles without any deflection
if ((_minDeflection != 0 || {_maxDeflection != 0}) && {_profileAdjustedTargetPos isNotEqualTo [0,0,0]}) then {
// Get a commanded acceleration via proportional navigation (https://youtu.be/Osb7anMm1AY)
// Use a simple PID controller to get the desired pitch, yaw, and roll
// Simulate moving servos by moving in each DOF by a fixed amount per frame
// Then setVectorDirAndUp to allow ARMA to translate the velocity to whatever PhysX says
private _rollDegreesPerSecond = 30;
private _yawDegreesPerSecond = 30;
private _pitchDegreesPerSecond = 30;
private _proportionalGain = 1;
private _integralGain = 0;
private _derivativeGain = 0;
_pidData params ["_pid", "_lastMissileFrame", "_currentPitchYawRoll"];
_currentPitchYawRoll params ["_pitch", "_yaw", "_roll"];
_lastMissileFrame params ["_lastTargetPosition", "_lastTargetVelocity", "_lastAngle"];
private _navigationGain = 3;
// integrate target velocity for realistic inference of velocity
private _targetVelocity = (_seekerTargetPos vectorDiff _lastTargetPosition) vectorMultiply (1 / diag_deltaTime);
private _targetAcceleration = (_targetVelocity vectorDiff _lastTargetVelocity) vectorMultiply (1 / diag_deltaTime);
private _currentLineOfSight = vectorNormalized (_profileAdjustedTargetPos vectorDiff _projectilePos);
private _targetVelocityAtPositon = _profileAdjustedTargetPos vectorAdd _targetVelocity;
private _lineOfSightAtPosition = _projectilePos vectorAdd _currentLineOfSight;
// get angle between LOS's
private _angleNow = acos (_targetVelocityAtPositon vectorCos _lineOfSightAtPosition);
private _losChange = (_angleNow - _lastAngle) / diag_deltaTime;
private _closingVelocity = (velocity _projectile) vectorDiff _targetVelocity;
private _commandedAcceleration = _closingVelocity vectorMultiply (_navigationGain * _losChange);
_commandedAcceleration = _projectile vectorWorldToModelVisual _commandedAcceleration;
private _relativeLOS = _projectile vectorWorldToModelVisual (_currentLineOfSight vectorCrossProduct velocity _projectile);
_commandedAcceleration = _relativeLOS vectorMultiply (vectorMagnitude _commandedAcceleration);
#ifdef DRAW_GUIDANCE_INFO
TRACE_1("",_commandedAcceleration);
private _projectilePosAGL = ASLToAGL _projectilePos;
drawLine3D [_projectilePosAGL, _projectilePosAGL vectorAdd ((_projectile vectorModelToWorldVisual _relativeLOS) vectorMultiply 15), [1, 0, 0, 1]];
#endif
if (!isGamePaused && accTime > 0) then {
_commandedAcceleration params ["_pitchChange", "_yawChange"];
private _clampedPitch = (-_pitchChange min _pitchDegreesPerSecond) max -_pitchDegreesPerSecond;
private _clampedYaw = (_yawChange min _yawDegreesPerSecond) max -_yawDegreesPerSecond;
_pitch = _pitch + _clampedPitch * diag_deltaTime;
_yaw = _yaw + _clampedYaw * diag_deltaTime;
[_projectile, _pitch, _yaw, 0] call FUNC(changeMissileDirection);
_currentPitchYawRoll set [0, _pitch];
_currentPitchYawRoll set [1, _yaw];
};
_pidData set [0, _pid];
if (accTime > 0) then {
_pidData set [1, [_seekerTargetPos, _targetVelocity, _angleNow]];
};
_pidData set [2, _currentPitchYawRoll];
_stateParams set [4, _pidData];
_args set [4, _stateParams];
};
#ifdef DRAW_GUIDANCE_INFO
TRACE_3("",_projectilePos,_seekerTargetPos,_profileAdjustedTargetPos);
drawIcon3D ["\a3\ui_f\data\IGUI\Cfg\Cursors\selectover_ca.paa", [1,0,0,1], ASLtoAGL _projectilePos, 0.75, 0.75, 0, _ammo, 1, 0.025, "TahomaB"];
if (!isGamePaused && accTime > 0) then {
private _ps = "#particlesource" createVehicleLocal (ASLtoAGL _projectilePos);
_PS setParticleParams [["\A3\Data_f\cl_basic", 8, 3, 1], "", "Billboard", 1, 3.0141, [0, 0, 2], [0, 0, 0], 1, 1.275, 1, 0, [1, 1], [[1, 0, 0, 1], [1, 0, 0, 1], [1, 0, 0, 1]], [1], 1, 0, "", "", nil];
_PS setDropInterval 1.0;
};
#endif
_stateParams set [0, diag_tickTime];
END_COUNTER(guidancePFH);