// Written by David Culp, started November 2003.
// - davidculp2@comcast.net
//
-// With major additions by Mathias Froehlich & Vivian Meazza 2004-2007
+// With major additions by Mathias Froehlich & Vivian Meazza 2004-2008
//
// This program is free software; you can redistribute it and/or
// modify it under the terms of the GNU General Public License as
# include <config.h>
#endif
-#include <simgear/math/point3d.hxx>
#include <simgear/math/sg_random.h>
-#include <simgear/scene/material/mat.hxx>
-#include <math.h>
-#include <vector>
+#include <simgear/math/sg_geodesy.hxx>
+#include <simgear/scene/model/modellib.hxx>
#include <Scenery/scenery.hxx>
#include "AIBallistic.hxx"
-SG_USING_STD(vector);
+#include <Main/util.hxx>
+#include <Environment/gravity.hxx>
+
+using namespace simgear;
+using std::string;
const double FGAIBallistic::slugs_to_kgs = 14.5939029372;
+const double FGAIBallistic::slugs_to_lbs = 32.1740485564;
+
+FGAIBallistic::FGAIBallistic(object_type ot) :
+FGAIBase(ot, false),
+_height(0.0),
+_speed(0),
+_ht_agl_ft(0.0),
+_azimuth(0.0),
+_elevation(0.0),
+_rotation(0.0),
+hs(0),
+_elapsed_time(0),
+_az_random_error(0.0),
+_el_random_error(0.0),
+_aero_stabilised(false),
+_drag_area(0.007),
+_cd(0.029),
+_init_cd(0.029),
+_cd_randomness(0.0),
+_buoyancy(0),
+_life_timer(0.0),
+_wind(true),
+_mass(0),
+_random(false),
+_life_randomness(0.0),
+_load_resistance(0),
+_solid(false),
+_force_stabilised(false),
+_slave_to_ac(false),
+_slave_load_to_ac(false),
+_contents_lb(0),
+_report_collision(false),
+_report_impact(false),
+_external_force(false),
+_report_expiry(false),
+_impact_report_node(fgGetNode("/ai/models/model-impact", true))
-FGAIBallistic::FGAIBallistic() :
- FGAIBase(otBallistic),
- _aero_stabilised(false),
- _drag_area(0.007),
- _life_timer(0.0),
- _gravity(32),
- // _buoyancy(64),
- _ht_agl_ft(0),
- _load_resistance(0),
- _solid(false),
- _impact_data(false),
- _impact_report_node(0),
- _impact_energy(0),
- _impact_speed(0),
- _impact_lat(0),
- _impact_lon(0),
- _impact_elev(0),
- _mat_name("")
{
no_roll = false;
}
}
void FGAIBallistic::readFromScenario(SGPropertyNode* scFileNode) {
- if (!scFileNode)
+ if (!scFileNode){
return;
+ }
FGAIBase::readFromScenario(scFileNode);
+ //setPath(scFileNode->getStringValue("model", "Models/Geometry/rocket.ac"));
+ setRandom(scFileNode->getBoolValue("random", false));
setAzimuth(scFileNode->getDoubleValue("azimuth", 0.0));
- setElevation(scFileNode->getDoubleValue("elevation", 0.0));
+ setElevation(scFileNode->getDoubleValue("elevation", 0));
setDragArea(scFileNode->getDoubleValue("eda", 0.007));
setLife(scFileNode->getDoubleValue("life", 900.0));
setBuoyancy(scFileNode->getDoubleValue("buoyancy", 0));
- setWind_from_east(scFileNode->getDoubleValue("wind_from_east", 0));
- setWind_from_north(scFileNode->getDoubleValue("wind_from_north", 0));
+ //setWind_from_east(scFileNode->getDoubleValue("wind_from_east", 0));
+ //setWind_from_north(scFileNode->getDoubleValue("wind_from_north", 0));
setWind(scFileNode->getBoolValue("wind", false));
setRoll(scFileNode->getDoubleValue("roll", 0.0));
setCd(scFileNode->getDoubleValue("cd", 0.029));
- setMass(scFileNode->getDoubleValue("mass", 0.007));
- setStabilisation(scFileNode->getBoolValue("aero_stabilized", false));
+ //setMass(scFileNode->getDoubleValue("mass", 0.007));
+ setWeight(scFileNode->getDoubleValue("weight", 0.25));
+ setStabilisation(scFileNode->getBoolValue("aero-stabilised", false));
setNoRoll(scFileNode->getBoolValue("no-roll", false));
- setRandom(scFileNode->getBoolValue("random", false));
setImpact(scFileNode->getBoolValue("impact", false));
+ setExpiry(scFileNode->getBoolValue("expiry", false));
+ setCollision(scFileNode->getBoolValue("collision", false));
setImpactReportNode(scFileNode->getStringValue("impact-reports"));
- setName(scFileNode->getStringValue("name", "Bomb"));
+ setName(scFileNode->getStringValue("name", "Rocket"));
+ setFuseRange(scFileNode->getDoubleValue("fuse-range", 0.0));
+ setSMPath(scFileNode->getStringValue("submodel-path", ""));
+ setSubID(scFileNode->getIntValue("SubID", 0));
+ setExternalForce(scFileNode->getBoolValue("external-force", false));
+ setForcePath(scFileNode->getStringValue("force-path", ""));
+ setForceStabilisation(scFileNode->getBoolValue("force-stabilised", false));
+ setXoffset(scFileNode->getDoubleValue("x-offset", 0.0));
+ setYoffset(scFileNode->getDoubleValue("y-offset", 0.0));
+ setZoffset(scFileNode->getDoubleValue("z-offset", 0.0));
+ setPitchoffset(scFileNode->getDoubleValue("pitch-offset", 0.0));
+ setRolloffset(scFileNode->getDoubleValue("roll-offset", 0.0));
+ setYawoffset(scFileNode->getDoubleValue("yaw-offset", 0.0));
+ setGroundOffset(scFileNode->getDoubleValue("ground-offset", 0.0));
+ setLoadOffset(scFileNode->getDoubleValue("load-offset", 0.0));
+ setSlaved(scFileNode->getBoolValue("slaved", false));
+ setSlavedLoad(scFileNode->getBoolValue("slaved-load", false));
+ setContentsPath(scFileNode->getStringValue("contents"));
+ setParentName(scFileNode->getStringValue("parent"));
}
bool FGAIBallistic::init(bool search_in_AI_path) {
FGAIBase::init(search_in_AI_path);
+ reinit();
+ return true;
+}
+
+void FGAIBallistic::reinit() {
+ _impact_reported = false;
+ _collision_reported = false;
+ _expiry_reported = false;
+
+ _impact_lat = 0;
+ _impact_lon = 0;
+ _impact_elev = 0;
+ _impact_hdg = 0;
+ _impact_pitch = 0;
+ _impact_roll = 0;
+ _impact_speed = 0;
- props->setStringValue("material/name", _mat_name.c_str());
+ invisible = false;
+
+ _elapsed_time += (sg_random() * 100);
+
+ _life_timer = 0;
+
+ props->setStringValue("material/name", "");
props->setStringValue("name", _name.c_str());
+ props->setStringValue("submodels/path", _path.c_str());
+
+ if (_slave_to_ac) {
+ props->setStringValue("force/path", _force_path.c_str());
+ props->setStringValue("contents/path", _contents_path.c_str());
+ }
+
+ //cout << "init: name " << _name.c_str() << " _life_timer " << _life_timer
+ // << endl;
+
+ //if(_parent != ""){
+ // setParentNode();
+ //}
+
+ //setParentNodes(_selected_ac);
+
+ //props->setStringValue("vector/path", _vector_path.c_str());
// start with high value so that animations don't trigger yet
- _ht_agl_ft = 10000000;
+ _ht_agl_ft = 1e10;
hdg = _azimuth;
pitch = _elevation;
roll = _rotation;
+
Transform();
- return true;
+
+ if (_parent != "") {
+ setParentNode();
+ }
+
+ setParentNodes(_selected_ac);
+
+ FGAIBase::reinit();
}
void FGAIBallistic::bind() {
// FGAIBase::bind();
- props->tie("sim/time/elapsed-sec",
+
+ _tiedProperties.setRoot(props);
+ tie("sim/time/elapsed-sec",
SGRawValueMethods<FGAIBallistic,double>(*this,
- &FGAIBallistic::_getTime));
- props->tie("material/load-resistance",
- SGRawValuePointer<double>(&_load_resistance));
- props->tie("material/solid",
- SGRawValuePointer<bool>(&_solid));
- props->tie("altitude-agl-ft",
- SGRawValuePointer<double>(&_ht_agl_ft));
- props->tie("impact/latitude-deg",
- SGRawValuePointer<double>(&_impact_lat));
- props->tie("impact/longitude-deg",
- SGRawValuePointer<double>(&_impact_lon));
- props->tie("impact/elevation-m",
- SGRawValuePointer<double>(&_impact_elev));
- props->tie("impact/speed-mps",
- SGRawValuePointer<double>(&_impact_speed));
- props->tie("impact/energy-kJ",
- SGRawValuePointer<double>(&_impact_energy));
-}
-
-void FGAIBallistic::unbind() {
- // FGAIBase::unbind();
- props->untie("sim/time/elapsed-sec");
- props->untie("material/load-resistance");
- props->untie("material/solid");
- props->untie("altitude-agl-ft");
- props->untie("impact/latitude-deg");
- props->untie("impact/longitude-deg");
- props->untie("impact/elevation-m");
- props->untie("impact/speed-mps");
- props->untie("impact/energy-kJ");
-}
-
-void FGAIBallistic::update(double dt) {
+ &FGAIBallistic::_getTime, &FGAIBallistic::setTime));
+ //tie("mass-slug",
+ // SGRawValueMethods<FGAIBallistic,double>(*this,
+ // &FGAIBallistic::getMass));
+
+ tie("material/solid",
+ SGRawValuePointer<bool>(&_solid));
+ tie("altitude-agl-ft",
+ SGRawValuePointer<double>(&_ht_agl_ft));
+ tie("controls/slave-to-ac",
+ SGRawValueMethods<FGAIBallistic,bool>
+ (*this, &FGAIBallistic::getSlaved, &FGAIBallistic::setSlaved));
+ tie("controls/invisible",
+ SGRawValuePointer<bool>(&invisible));
+
+ if (_external_force || _slave_to_ac) {
+ tie("controls/force_stabilized",
+ SGRawValuePointer<bool>(&_force_stabilised));
+ tie("position/global-x",
+ SGRawValueMethods<FGAIBase,double>(*this, &FGAIBase::_getCartPosX, 0));
+ tie("position/global-y",
+ SGRawValueMethods<FGAIBase,double>(*this, &FGAIBase::_getCartPosY, 0));
+ tie("position/global-z",
+ SGRawValueMethods<FGAIBase,double>(*this, &FGAIBase::_getCartPosZ, 0));
+ tie("velocities/vertical-speed-fps",
+ SGRawValuePointer<double>(&vs));
+ tie("velocities/true-airspeed-kt",
+ SGRawValuePointer<double>(&speed));
+ tie("velocities/horizontal-speed-fps",
+ SGRawValuePointer<double>(&hs));
+ tie("position/altitude-ft",
+ SGRawValueMethods<FGAIBase,double>(*this, &FGAIBase::_getElevationFt, &FGAIBase::_setAltitude));
+ tie("position/latitude-deg",
+ SGRawValueMethods<FGAIBase,double>(*this, &FGAIBase::_getLatitude, &FGAIBase::_setLatitude));
+ tie("position/longitude-deg",
+ SGRawValueMethods<FGAIBase,double>(*this, &FGAIBase::_getLongitude, &FGAIBase::_setLongitude));
+ tie("orientation/hdg-deg",
+ SGRawValuePointer<double>(&hdg));
+ tie("orientation/pitch-deg",
+ SGRawValuePointer<double>(&pitch));
+ tie("orientation/roll-deg",
+ SGRawValuePointer<double>(&roll));
+ tie("controls/slave-load-to-ac",
+ SGRawValueMethods<FGAIBallistic,bool>
+ (*this, &FGAIBallistic::getSlavedLoad, &FGAIBallistic::setSlavedLoad));
+ tie("position/load-offset",
+ SGRawValueMethods<FGAIBallistic,double>
+ (*this, &FGAIBallistic::getLoadOffset, &FGAIBallistic::setLoadOffset));
+ tie("load/distance-to-hitch-ft",
+ SGRawValueMethods<FGAIBallistic,double>
+ (*this, &FGAIBallistic::getDistanceToHitch));
+ tie("load/elevation-to-hitch-deg",
+ SGRawValueMethods<FGAIBallistic,double>
+ (*this, &FGAIBallistic::getElevToHitch));
+ tie("load/bearing-to-hitch-deg",
+ SGRawValueMethods<FGAIBallistic,double>
+ (*this, &FGAIBallistic::getBearingToHitch));
+ tie("material/load-resistance",
+ SGRawValuePointer<double>(&_load_resistance));
+ }
+}
+
+void FGAIBallistic::update(double dt)
+{
FGAIBase::update(dt);
- Run(dt);
- Transform();
+
+ if (_slave_to_ac) {
+ slaveToAC(dt);
+ Transform();
+ }
+ else if (!invisible) {
+ Run(dt);
+ Transform();
+ }
+
}
void FGAIBallistic::setAzimuth(double az) {
- hdg = _azimuth = az;
+ if (_random)
+ hdg = _azimuth = az - _az_random_error + 2 * _az_random_error * sg_random();
+ else
+ hdg = _azimuth = az;
+}
+
+void FGAIBallistic::setAzimuthRandomError(double error) {
+ _az_random_error = error;
+}
+
+void FGAIBallistic::setElevationRandomError(double error) {
+ _el_random_error = error;
}
void FGAIBallistic::setElevation(double el) {
- pitch = _elevation = el;
+ if (_random)
+ pitch = _elevation = el - _el_random_error + 2 * _el_random_error * sg_random();
+ else
+ pitch = _elevation = el;
}
void FGAIBallistic::setRoll(double rl) {
- _rotation = rl;
+ roll = _rotation = rl;
}
void FGAIBallistic::setStabilisation(bool val) {
_aero_stabilised = val;
}
+void FGAIBallistic::setForceStabilisation(bool val) {
+ _force_stabilised = val;
+}
+
void FGAIBallistic::setNoRoll(bool nr) {
no_roll = nr;
}
}
void FGAIBallistic::setLife(double seconds) {
- life = seconds;
+ if (_random)
+ life = seconds * _life_randomness + (seconds * (1 -_life_randomness) * sg_random());
+ else
+ life = seconds;
}
void FGAIBallistic::setBuoyancy(double fpss) {
_wind = val;
}
-void FGAIBallistic::setCd(double c) {
- _Cd = c;
+void FGAIBallistic::setCd(double cd) {
+ _cd = cd;
+ _init_cd = cd;
+}
+
+void FGAIBallistic::setCdRandomness(double randomness) {
+ _cd_randomness = randomness;
}
void FGAIBallistic::setMass(double m) {
_mass = m;
}
+void FGAIBallistic::setWeight(double w) {
+ _weight_lb = w;
+}
+
+void FGAIBallistic::setLifeRandomness(double randomness) {
+ _life_randomness = randomness;
+}
+
void FGAIBallistic::setRandom(bool r) {
_random = r;
}
void FGAIBallistic::setImpact(bool i) {
- _impact = i;
+ _report_impact = i;
+}
+
+void FGAIBallistic::setCollision(bool c) {
+ _report_collision = c;
+}
+
+void FGAIBallistic::setExpiry(bool e) {
+ _report_expiry = e;
+}
+
+void FGAIBallistic::setExternalForce(bool f) {
+ _external_force = f;
}
void FGAIBallistic::setImpactReportNode(const string& path) {
- if (path.empty())
- _impact_report_node = 0;
- else
+ if (!path.empty())
_impact_report_node = fgGetNode(path.c_str(), true);
}
-void FGAIBallistic::setName(const string& n) {
- _name = n;
+void FGAIBallistic::setSMPath(const string& s) {
+ _path = s;
+ //cout << "submodel path " << _path << endl;
+}
+
+void FGAIBallistic::setFuseRange(double f) {
+ _fuse_range = f;
+}
+
+void FGAIBallistic::setSubID(int i) {
+ _subID = i;
+}
+
+void FGAIBallistic::setSubmodel(const string& s) {
+ _submodel = s;
+}
+
+void FGAIBallistic::setGroundOffset(double g) {
+ _ground_offset = g;
+}
+
+void FGAIBallistic::setLoadOffset(double l) {
+ _load_offset = l;
+}
+
+double FGAIBallistic::getLoadOffset() const {
+ return _load_offset;
+}
+
+void FGAIBallistic::setSlaved(bool s) {
+ _slave_to_ac = s;
+}
+
+void FGAIBallistic::setContentsPath(const string& path) {
+ _contents_path = path;
+
+ if (!path.empty()) {
+ _contents_node = fgGetNode(path.c_str(), true);
+ }
+}
+
+void FGAIBallistic::setContentsNode(SGPropertyNode_ptr node) {
+ if (node != 0) {
+ _contents_node = node;
+ _contents_path = _contents_node->getDisplayName();
+ }
+}
+
+void FGAIBallistic::setParentNodes(SGPropertyNode_ptr node) {
+ if (node != 0) {
+ _pnode = node;
+ _p_pos_node = _pnode->getChild("position", 0, true);
+ _p_lat_node = _p_pos_node->getChild("latitude-deg", 0, true);
+ _p_lon_node = _p_pos_node->getChild("longitude-deg", 0, true);
+ _p_alt_node = _p_pos_node->getChild("altitude-ft", 0, true);
+ _p_agl_node = _p_pos_node->getChild("altitude-agl-ft", 0, true);
+
+
+ _p_ori_node = _pnode->getChild("orientation", 0, true);
+ _p_pch_node = _p_ori_node->getChild("pitch-deg", 0, true);
+ _p_rll_node = _p_ori_node->getChild("roll-deg", 0, true);
+ _p_hdg_node = _p_ori_node->getChild("true-heading-deg",0, true);
+
+ _p_vel_node = _pnode->getChild("velocities", 0, true);
+ _p_spd_node = _p_vel_node->getChild("true-airspeed-kt", 0, true);
+ }
+}
+
+void FGAIBallistic::setParentPos() {
+ if (_pnode != 0) {
+ double lat = _p_lat_node->getDoubleValue();
+ double lon = _p_lon_node->getDoubleValue();
+ double alt = _p_alt_node->getDoubleValue();
+
+ _parentpos.setLongitudeDeg(lon);
+ _parentpos.setLatitudeDeg(lat);
+ _parentpos.setElevationFt(alt);
+ }
+}
+
+bool FGAIBallistic::getSlaved() const {
+ return _slave_to_ac;
+}
+
+double FGAIBallistic::getMass() const {
+ return _mass;
+}
+
+double FGAIBallistic::getContents() {
+ if (_contents_node) {
+ _contents_lb = _contents_node->getChild("level-lbs", 0, 1)->getDoubleValue();
+ }
+ return _contents_lb;
+}
+
+void FGAIBallistic::setContents(double c) {
+ if (_contents_node)
+ _contents_lb = _contents_node->getChild("level-gal_us", 0, 1)->setDoubleValue(c);
+}
+
+void FGAIBallistic::setSlavedLoad(bool l) {
+ _slave_load_to_ac = l;
+}
+
+bool FGAIBallistic::getSlavedLoad() const {
+ return _slave_load_to_ac;
+}
+
+void FGAIBallistic::setForcePath(const string& p) {
+ _force_path = p;
+ if (!_force_path.empty()) {
+ SGPropertyNode *fnode = fgGetNode(_force_path.c_str(), 0, true );
+ _force_node = fnode->getChild("force-lb", 0, true);
+ _force_azimuth_node = fnode->getChild("force-azimuth-deg", 0, true);
+ _force_elevation_node = fnode->getChild("force-elevation-deg", 0, true);
+ }
+}
+
+bool FGAIBallistic::getHtAGL(double start) {
+ const simgear::BVHMaterial* mat = 0;
+ if (getGroundElevationM(SGGeod::fromGeodM(pos, start),
+ _elevation_m, &mat)) {
+ const SGMaterial* material = dynamic_cast<const SGMaterial*>(mat);
+ _ht_agl_ft = pos.getElevationFt() - _elevation_m * SG_METER_TO_FEET;
+
+ if (material) {
+ const std::vector<string>& names = material->get_names();
+ _solid = material->get_solid();
+ _load_resistance = material->get_load_resistance();
+ _frictionFactor = material->get_friction_factor();
+
+ if (!names.empty())
+ props->setStringValue("material/name", names[0].c_str());
+ else
+ props->setStringValue("material/name", "");
+
+ _mat_name = names[0];
+
+ //cout << "material " << _mat_name
+ //<< " solid " << _solid
+ //<< " load " << _load_resistance
+ //<< " frictionFactor " << _frictionFactor
+ //<< endl;
+ }
+
+ return true;
+ }
+ else {
+ return false;
+ }
+}
+
+double FGAIBallistic::getRecip(double az) {
+ // calculate the reciprocal of the input azimuth
+ if (az - 180 < 0) {
+ return az + 180;
+ }
+ else {
+ return az - 180;
+ }
+}
+
+void FGAIBallistic::setPch(double e, double dt, double coeff) {
+ double c = dt / (coeff + dt);
+ pitch = (e * c) + (pitch * (1 - c));
+}
+
+void FGAIBallistic::setBnk(double r, double dt, double coeff) {
+ double c = dt / (coeff + dt);
+ roll = (r * c) + (roll * (1 - c));
+}
+
+void FGAIBallistic::setSpd(double s, double dt, double coeff) {
+ double c = dt / (coeff + dt);
+ _speed = (s * c) + (_speed * (1 - c));
+}
+
+void FGAIBallistic::setHt(double h, double dt, double coeff) {
+ double c = dt / (coeff + dt);
+ _height = (h * c) + (_height * (1 - c));
+}
+
+int FGAIBallistic::setHdg(double tgt_hdg, double dt, double coeff) {
+ double recip = getRecip(hdg);
+ double c = dt / (coeff + dt);
+ //cout << "set heading " << tgt_hdg << endl;
+ //we need to ensure that we turn the short way to the new hdg
+ if (tgt_hdg < recip && tgt_hdg < hdg && hdg > 180) {
+ hdg = ((tgt_hdg + 360) * c) + (hdg * (1 - c));
+// cout << "case 1: right turn" << endl;
+ } else if (tgt_hdg > recip && tgt_hdg > hdg && hdg <= 180){
+ hdg = ((tgt_hdg - 360) * c) + (hdg * (1 - c));
+// cout << "case 2: left turn" << endl;
+ } else {
+ hdg = (tgt_hdg * c) + (hdg * (1 - c));
+// cout << "case 4: left turn" << endl;
+ }
+ return -1;
+}
+
+double FGAIBallistic::getTgtXOffset() const {
+ return _tgt_x_offset;
+}
+
+double FGAIBallistic::getTgtYOffset() const {
+ return _tgt_y_offset;
+}
+
+double FGAIBallistic::getTgtZOffset() const {
+ return _tgt_z_offset;
+}
+
+void FGAIBallistic::setTgtXOffset(double x) {
+ _tgt_x_offset = x;
+}
+
+void FGAIBallistic::setTgtYOffset(double y) {
+ _tgt_y_offset = y;
+}
+
+void FGAIBallistic::setTgtZOffset(double z) {
+ _tgt_z_offset = z;
+}
+
+void FGAIBallistic::slaveToAC(double dt) {
+ if (invisible)
+ return;
+
+ double hdg, pch, rll;//, agl = 0;
+
+ if (_pnode != 0) {
+ setParentPos();
+ hdg = _p_hdg_node->getDoubleValue();
+ pch = _p_pch_node->getDoubleValue();
+ rll = _p_rll_node->getDoubleValue();
+// agl = _p_agl_node->getDoubleValue();
+ setOffsetPos(_parentpos, hdg, pch, rll);
+ setSpeed(_p_spd_node->getDoubleValue());
+ }
+ else {
+ hdg = manager->get_user_heading();
+ pch = manager->get_user_pitch();
+ rll = manager->get_user_roll();
+// agl = manager->get_user_agl();
+ setOffsetPos(globals->get_aircraft_position(), hdg, pch, rll);
+ setSpeed(manager->get_user_speed());
+ }
+
+ pos.setLatitudeDeg(_offsetpos.getLatitudeDeg());
+ pos.setLongitudeDeg(_offsetpos.getLongitudeDeg());
+ pos.setElevationFt(_offsetpos.getElevationFt());
+ setHeading(hdg);
+ setPitch(pch + _pitch_offset);
+ setBank(rll + _roll_offset);
+ setOffsetVelocity(dt, pos);
+ setTime(0);
+
+ //update the mass (slugs)
+ _mass = (_weight_lb + getContents()) / slugs_to_lbs;
+
+ _impact_reported = false;
+
+ //cout << _name << " _mass "<<_mass <<" " << getContents()
+ //<< " " << getContents() / slugs_to_lbs << " weight " << _weight_lb << endl;
+ // cout << _name << " update hs " << hs << " vs " << vs << endl;
}
void FGAIBallistic::Run(double dt) {
_life_timer += dt;
- // cout << "life timer 1" << _life_timer << dt << endl;
- if (_life_timer > life)
- setDie(true);
+
+ //_pass += 1;
+ //cout<<"AIBallistic run: name " << _name.c_str()
+ // << " dt " << dt << " _life_timer " << _life_timer << " pass " << _pass << endl;
+
+ // if life = -1 the object does not die
+ if (_life_timer > life && life != -1) {
+ if (_report_expiry && !_expiry_reported && !_impact_reported && !_collision_reported) {
+ //cout<<"AIBallistic run: name " << _name.c_str() << " expiry "
+ //<< " _life_timer " << _life_timer<< endl;
+ handle_expiry();
+ }
+ else {
+ //cout<<"AIBallistic run: name " << _name.c_str()
+ // << " die " << " _life_timer " << _life_timer << endl;
+ setDie(true);
+ }
+
+ setTime(0);
+ }
- double speed_north_deg_sec;
- double speed_east_deg_sec;
- double wind_speed_from_north_deg_sec;
- double wind_speed_from_east_deg_sec;
- double Cdm; // Cd adjusted by Mach Number
+ // Set the contents in the appropriate tank or other property in the parent to zero
+ setContents(0);
- //randomise Cd by +- 5%
- if (_random)
- _Cd = _Cd * 0.95 + (0.05 * sg_random());
+ if (_random) {
+ // Keep the new Cd within +- 10% of the current Cd to avoid a fluctuating value
+ double cd_min = _cd * 0.9;
+ double cd_max = _cd * 1.1;
+
+ // Randomize Cd by +- a certain percentage of the initial Cd
+ _cd = _init_cd * (1 - _cd_randomness + 2 * _cd_randomness * sg_random());
+
+ if (_cd < cd_min) _cd = cd_min;
+ if (_cd > cd_max) _cd = cd_max;
+ }
// Adjust Cd by Mach number. The equations are based on curves
// for a conventional shell/bullet (no boat-tail).
- if (Mach >= 1.2)
- Cdm = 0.2965 * pow ( Mach, -1.1506 ) + _Cd;
- else if (Mach >= 0.7)
- Cdm = 0.3742 * pow ( Mach, 2) - 0.252 * Mach + 0.0021 + _Cd;
+ double Cdm;
+
+ if (Mach < 0.7)
+ Cdm = 0.0125 * Mach + _cd;
+ else if (Mach < 1.2)
+ Cdm = 0.3742 * pow(Mach, 2) - 0.252 * Mach + 0.0021 + _cd;
else
- Cdm = 0.0125 * Mach + _Cd;
+ Cdm = 0.2965 * pow(Mach, -1.1506) + _cd;
- //cout << " Mach , " << Mach << " , Cdm , " << Cdm << " ballistic speed kts //"<< speed << endl;
+ //cout <<_name << " Mach " << Mach << " Cdm " << Cdm
+ // << " ballistic speed kts "<< speed << endl;
// drag = Cd * 0.5 * rho * speed * speed * drag_area;
// rho is adjusted for altitude in void FGAIBase::update,
speed -= (Cdm * 0.5 * rho * speed * speed * _drag_area/_mass) * dt;
// don't let speed become negative
- if ( speed < 0.0 )
+ if (speed < 0.0)
speed = 0.0;
- double speed_fps = speed * SG_KT_TO_FPS;
+// double speed_fps = speed * SG_KT_TO_FPS;
// calculate vertical and horizontal speed components
- vs = sin( pitch * SG_DEGREES_TO_RADIANS ) * speed_fps;
- double hs = cos( pitch * SG_DEGREES_TO_RADIANS ) * speed_fps;
+ calcVSHS();
- // convert horizontal speed (fps) to degrees per second
- speed_north_deg_sec = cos(hdg / SG_RADIANS_TO_DEGREES) * hs / ft_per_deg_lat;
- speed_east_deg_sec = sin(hdg / SG_RADIANS_TO_DEGREES) * hs / ft_per_deg_lon;
+ //resolve horizontal speed into north and east components:
+ //and convert horizontal speed (fps) to degrees per second
+ calcNE();
- // if wind not required, set to zero
+ // If wind not required, set to zero
if (!_wind) {
_wind_from_north = 0;
_wind_from_east = 0;
}
+ else {
+ _wind_from_north = manager->get_wind_from_north();
+ _wind_from_east = manager->get_wind_from_east();
+ }
+
+ // Calculate velocity due to external force
+ double force_speed_north_deg_sec = 0;
+ double force_speed_east_deg_sec = 0;
+ double hs_force_fps = 0;
+ double v_force_acc_fpss = 0;
+ double force_speed_north_fps = 0;
+ double force_speed_east_fps = 0;
+ double h_force_lbs = 0;
+ double normal_force_lbs = 0;
+ double normal_force_fpss = 0;
+ double static_friction_force_lbs = 0;
+ double dynamic_friction_force_lbs = 0;
+ double friction_force_speed_north_fps = 0;
+ double friction_force_speed_east_fps = 0;
+ double friction_force_speed_north_deg_sec = 0;
+ double friction_force_speed_east_deg_sec = 0;
+ double force_elevation_deg = 0;
+ double force_azimuth_deg = 0;
+ double force_lbs = 0;
+
+ if (_external_force) {
+ //cout << _name << " external force " << hdg << " az " << _azimuth << endl;
+
+ SGPropertyNode *n = fgGetNode(_force_path.c_str(), true);
+ force_lbs = n->getChild("force-lb", 0, true)->getDoubleValue();
+ force_elevation_deg = n->getChild("force-elevation-deg", 0, true)->getDoubleValue();
+ force_azimuth_deg = n->getChild("force-azimuth-deg", 0, true)->getDoubleValue();
+
+ // Resolve force into vertical and horizontal components:
+ double v_force_lbs = force_lbs * sin( force_elevation_deg * SG_DEGREES_TO_RADIANS );
+ h_force_lbs = force_lbs * cos( force_elevation_deg * SG_DEGREES_TO_RADIANS );
+
+ // Perform ground interaction if impacts are not calculated
+ if (!_report_impact && getHtAGL(10000)) {
+ double deadzone = 0.1;
+
+ if (_ht_agl_ft <= (0 + _ground_offset + deadzone) && _solid) {
+ normal_force_lbs = (_mass * slugs_to_lbs) - v_force_lbs;
+
+ if (normal_force_lbs < 0)
+ normal_force_lbs = 0;
+
+ pos.setElevationFt(0 + _ground_offset);
+ if (vs < 0)
+ vs = -vs * 0.5;
+
+ // Calculate friction. We assume a static coefficient of
+ // friction (mu) of 0.62 (wood on concrete)
+ double mu = 0.62;
+
+ static_friction_force_lbs = mu * normal_force_lbs * _frictionFactor;
+
+ // Adjust horizontal force. We assume that a speed of <= 5 fps is static
+ if (h_force_lbs <= static_friction_force_lbs && hs <= 5) {
+ h_force_lbs = hs = 0;
+ _speed_north_fps = _speed_east_fps = 0;
+ }
+ else
+ dynamic_friction_force_lbs = (static_friction_force_lbs * 0.95);
+
+ // Ignore wind when on the ground for now
+ //TODO fix this
+ _wind_from_north = 0;
+ _wind_from_east = 0;
+ }
+ }
+
+ //acceleration = (force(lbsf)/mass(slugs))
+ v_force_acc_fpss = v_force_lbs / _mass;
+ normal_force_fpss = normal_force_lbs / _mass;
+ double h_force_acc_fpss = h_force_lbs / _mass;
+ double dynamic_friction_acc_fpss = dynamic_friction_force_lbs / _mass;
+
+ // velocity = acceleration * dt
+ hs_force_fps = h_force_acc_fpss * dt;
+ double friction_force_fps = dynamic_friction_acc_fpss * dt;
+
+ //resolve horizontal speeds into north and east components:
+ force_speed_north_fps = cos(force_azimuth_deg * SG_DEGREES_TO_RADIANS) * hs_force_fps;
+ force_speed_east_fps = sin(force_azimuth_deg * SG_DEGREES_TO_RADIANS) * hs_force_fps;
+
+ friction_force_speed_north_fps = cos(getRecip(hdg) * SG_DEGREES_TO_RADIANS) * friction_force_fps;
+ friction_force_speed_east_fps = sin(getRecip(hdg) * SG_DEGREES_TO_RADIANS) * friction_force_fps;
+
+ // convert horizontal speed (fps) to degrees per second
+ force_speed_north_deg_sec = force_speed_north_fps / ft_per_deg_lat;
+ force_speed_east_deg_sec = force_speed_east_fps / ft_per_deg_lon;
+
+ friction_force_speed_north_deg_sec = friction_force_speed_north_fps / ft_per_deg_lat;
+ friction_force_speed_east_deg_sec = friction_force_speed_east_fps / ft_per_deg_lon;
+ }
- // convert wind speed (fps) to degrees per second
- wind_speed_from_north_deg_sec = _wind_from_north / ft_per_deg_lat;
- wind_speed_from_east_deg_sec = _wind_from_east / ft_per_deg_lon;
+ // convert wind speed (fps) to degrees lat/lon per second
+ double wind_speed_from_north_deg_sec = _wind_from_north / ft_per_deg_lat;
+ double wind_speed_from_east_deg_sec = _wind_from_east / ft_per_deg_lon;
- // set new position
- pos.setLatitudeDeg( pos.getLatitudeDeg()
- + (speed_north_deg_sec - wind_speed_from_north_deg_sec) * dt );
- pos.setLongitudeDeg( pos.getLongitudeDeg()
- + (speed_east_deg_sec - wind_speed_from_east_deg_sec) * dt );
+ //recombine the horizontal velocity components
+ hs = sqrt(((_speed_north_fps + force_speed_north_fps + friction_force_speed_north_fps)
+ * (_speed_north_fps + force_speed_north_fps + friction_force_speed_north_fps))
+ + ((_speed_east_fps + force_speed_east_fps + friction_force_speed_east_fps)
+ * (_speed_east_fps + force_speed_east_fps + friction_force_speed_east_fps)));
- // adjust vertical speed for acceleration of gravity and buoyancy
- vs -= (_gravity - _buoyancy) * dt;
+ if (hs <= 0.00001)
+ hs = 0;
- // adjust altitude (feet)
- altitude_ft += vs * dt;
- pos.setElevationFt(altitude_ft);
+ // adjust vertical speed for acceleration of gravity, buoyancy, and vertical force
+ double gravity = SG_METER_TO_FEET * (Environment::Gravity::instance()->getGravity(pos));
+ vs -= (gravity - _buoyancy - v_force_acc_fpss - normal_force_fpss) * dt;
- // recalculate pitch (velocity vector) if aerostabilized
- /*cout << _name << ": " << "aero_stabilised " << _aero_stabilised
- << " pitch " << pitch <<" vs " << vs <<endl ;*/
+ if (vs <= 0.00001 && vs >= -0.00001)
+ vs = 0;
+
+ // set new position
+ if (_slave_load_to_ac) {
+ setOffsetPos(pos,
+ manager->get_user_heading(),
+ manager->get_user_pitch(),
+ manager->get_user_roll()
+ );
+ pos.setLatitudeDeg(_offsetpos.getLatitudeDeg());
+ pos.setLongitudeDeg(_offsetpos.getLongitudeDeg());
+ pos.setElevationFt(_offsetpos.getElevationFt());
+
+ if (getHtAGL(10000)) {
+ double deadzone = 0.1;
+
+ if (_ht_agl_ft <= (0 + _ground_offset + deadzone) && _solid) {
+ pos.setElevationFt(0 + _ground_offset);
+ }
+ else {
+ pos.setElevationFt(_offsetpos.getElevationFt() + _load_offset);
+ }
+ }
+ }
+ else {
+ pos.setLatitudeDeg( pos.getLatitudeDeg()
+ + (speed_north_deg_sec - wind_speed_from_north_deg_sec
+ + force_speed_north_deg_sec + friction_force_speed_north_deg_sec) * dt );
+ pos.setLongitudeDeg( pos.getLongitudeDeg()
+ + (speed_east_deg_sec - wind_speed_from_east_deg_sec
+ + force_speed_east_deg_sec + friction_force_speed_east_deg_sec) * dt );
+ pos.setElevationFt(pos.getElevationFt() + vs * dt);
+ }
- if (_aero_stabilised)
- pitch = atan2( vs, hs ) * SG_RADIANS_TO_DEGREES;
+// cout << _name << " run hs " << hs << " vs " << vs << endl;
// recalculate total speed
- speed = sqrt( vs * vs + hs * hs) / SG_KT_TO_FPS;
+ if ( vs == 0 && hs == 0)
+ speed = 0;
+ else
+ speed = sqrt( vs * vs + hs * hs) / SG_KT_TO_FPS;
+
+ // recalculate elevation and azimuth (velocity vectors)
+ _elevation = atan2( vs, hs ) * SG_RADIANS_TO_DEGREES;
+ _azimuth = atan2((_speed_east_fps + force_speed_east_fps + friction_force_speed_east_fps),
+ (_speed_north_fps + force_speed_north_fps + friction_force_speed_north_fps))
+ * SG_RADIANS_TO_DEGREES;
- if (_impact && !_impact_data && vs < 0)
+ // rationalise azimuth
+ if (_azimuth < 0)
+ _azimuth += 360;
+
+ if (_aero_stabilised) { // we simulate rotational moment of inertia by using a filter
+ //cout<< "_aero_stabilised " << hdg << " az " << _azimuth << endl;
+ const double coeff = 0.9;
+
+ // we assume a symetrical MI about the pitch and yaw axis
+ setPch(_elevation, dt, coeff);
+ setHdg(_azimuth, dt, coeff);
+ }
+ else if (_force_stabilised) { // we simulate rotational moment of inertia by using a filter
+ //cout<< "_force_stabilised "<< endl;
+
+ const double coeff = 0.9;
+ double ratio = h_force_lbs/(_mass * slugs_to_lbs);
+
+ if (ratio > 1) ratio = 1;
+ if (ratio < -1) ratio = -1;
+
+ double force_pitch = acos(ratio) * SG_RADIANS_TO_DEGREES;
+
+ if (force_pitch <= force_elevation_deg)
+ force_pitch = force_elevation_deg;
+
+ // we assume a symetrical MI about the pitch and yaw axis
+ setPch(force_pitch,dt, coeff);
+ setHdg(_azimuth, dt, coeff);
+ }
+
+ // Do impacts and collisions
+ if (_report_impact && !_impact_reported)
handle_impact();
- // set destruction flag if altitude less than sea level -1000
- if (altitude_ft < -1000.0)
- setDie(true);
+ if (_report_collision && !_collision_reported)
+ handle_collision();
-} // end Run
+ // Set destruction flag if altitude less than sea level -1000
+ if (altitude_ft < -1000.0 && life != -1)
+ setDie(true);
+}
double FGAIBallistic::_getTime() const {
- // cout << "life timer 2" << _life_timer << endl;
return _life_timer;
}
+void FGAIBallistic::setTime(double s) {
+ _life_timer = s;
+}
+
+void FGAIBallistic::handleEndOfLife(double elevation) {
+ report_impact(elevation);
+
+ // Make the submodel invisible if the submodel is immortal, otherwise kill it if it has no subsubmodels
+ if (life == -1) {
+ invisible = true;
+ }
+ else if (_subID == 0) {
+ // Kill the AIObject if there is no subsubmodel
+ setDie(true);
+ }
+}
+
void FGAIBallistic::handle_impact() {
- double elevation_m;
- const SGMaterial* material;
+ // Try terrain intersection
+ double start = pos.getElevationM() + 100;
- // try terrain intersection
- if (!globals->get_scenery()->get_elevation_m(pos.getLatitudeDeg(), pos.getLongitudeDeg(),
- 10000.0, elevation_m, &material))
+ if (!getHtAGL(start))
return;
- if (material) {
- const vector<string> names = material->get_names();
+ if (_ht_agl_ft <= 0) {
+ SG_LOG(SG_AI, SG_DEBUG, "AIBallistic: terrain impact material" << _mat_name);
+ _impact_reported = true;
+ handleEndOfLife(_elevation_m);
+ }
+}
- if (!names.empty())
- _mat_name = names[0].c_str();
+void FGAIBallistic::handle_expiry() {
+ _expiry_reported = true;
+ handleEndOfLife(pos.getElevationM());
+}
- _solid = material->get_solid();
- _load_resistance = material->get_load_resistance();
- props->setStringValue("material/name", _mat_name.c_str());
- //cout << "material " << _mat_name << " solid " << _solid << " load " << _load_resistance << endl;
+void FGAIBallistic::handle_collision()
+{
+ const FGAIBase *object = manager->calcCollision(pos.getElevationFt(),
+ pos.getLatitudeDeg(),pos.getLongitudeDeg(), _fuse_range);
+
+ if (object) {
+ report_impact(pos.getElevationM(), object);
+ _collision_reported = true;
}
+}
+
+void FGAIBallistic::report_impact(double elevation, const FGAIBase *object)
+{
+ _impact_lat = pos.getLatitudeDeg();
+ _impact_lon = pos.getLongitudeDeg();
+ _impact_elev = elevation;
+ _impact_speed = speed * SG_KT_TO_MPS;
+ _impact_hdg = hdg;
+ _impact_pitch = pitch;
+ _impact_roll = roll;
+
+ SGPropertyNode *n = props->getNode("impact", true);
+
+ if (object)
+ n->setStringValue("type", object->getTypeString());
+ else
+ n->setStringValue("type", "terrain");
- _ht_agl_ft = pos.getElevationFt() - elevation_m * SG_METER_TO_FEET;
+ SG_LOG(SG_AI, SG_DEBUG, "AIBallistic: object impact " << _name
+ << " lon " <<_impact_lon << " lat " <<_impact_lat << " sec " << _life_timer);
- // report impact by setting tied variables
- if (_ht_agl_ft <= 0) {
- _impact_data = true;
+ n->setDoubleValue("longitude-deg", _impact_lon);
+ n->setDoubleValue("latitude-deg", _impact_lat);
+ n->setDoubleValue("elevation-m", _impact_elev);
+ n->setDoubleValue("heading-deg", _impact_hdg);
+ n->setDoubleValue("pitch-deg", _impact_pitch);
+ n->setDoubleValue("roll-deg", _impact_roll);
+ n->setDoubleValue("speed-mps", _impact_speed);
+
+ _impact_report_node->setStringValue(props->getPath());
+}
+
+SGVec3d FGAIBallistic::getCartHitchPos() const {
+ // convert geodetic positions to geocentered
+ SGVec3d cartuserPos = globals->get_aircraft_position_cart();
+
+ //SGVec3d cartPos = getCartPos();
+
+ // Transform to the right coordinate frame, configuration is done in
+ // the x-forward, y-right, z-up coordinates (feet), computation
+ // in the simulation usual body x-forward, y-right, z-down coordinates
+ // (meters) )
+ SGVec3d _off(_x_offset * SG_FEET_TO_METER,
+ _y_offset * SG_FEET_TO_METER,
+ -_z_offset * SG_FEET_TO_METER);
+
+ // Transform the user position to the horizontal local coordinate system.
+ SGQuatd hlTrans = SGQuatd::fromLonLat(globals->get_aircraft_position());
+
+ // and postrotate the orientation of the user model wrt the horizontal
+ // local frame
+ hlTrans *= SGQuatd::fromYawPitchRollDeg(
+ manager->get_user_heading(),
+ manager->get_user_pitch(),
+ manager->get_user_roll());
+
+ // The offset converted to the usual body fixed coordinate system
+ // rotated to the earth-fixed coordinates axis
+ SGVec3d off = hlTrans.backTransform(_off);
+
+ // Add the position offset of the user model to get the geocentered position
+ SGVec3d offsetPos = cartuserPos + off;
+ return offsetPos;
+}
+
+void FGAIBallistic::setOffsetPos(SGGeod inpos, double heading, double pitch, double roll) {
+ // Convert the hitch geocentered position to geodetic
+ SGVec3d cartoffsetPos = getCartOffsetPos(inpos, heading, pitch, roll);
+ SGGeodesy::SGCartToGeod(cartoffsetPos, _offsetpos);
+}
+
+double FGAIBallistic::getDistanceToHitch() const {
+ //calculate the distance load to hitch
+ SGVec3d carthitchPos = getCartHitchPos();
+ SGVec3d cartPos = getCartPos();
- _impact_lat = pos.getLatitudeDeg();
- _impact_lon = pos.getLongitudeDeg();
- _impact_elev = elevation_m;
- _impact_speed = speed * SG_KT_TO_MPS;
- _impact_energy = (_mass * slugs_to_kgs) * _impact_speed
- * _impact_speed / (2 * 1000);
+ SGVec3d diff = carthitchPos - cartPos;
+ double distance = norm(diff);
+ return distance * SG_METER_TO_FEET;
+}
- if (_impact_report_node)
- _impact_report_node->setStringValue(props->getPath());
+double FGAIBallistic::getElevToHitch() const {
+ // now the angle, positive angles are upwards
+ double distance = getDistanceToHitch() * SG_FEET_TO_METER;
+ double angle = 0;
+ double daltM = _offsetpos.getElevationM() - pos.getElevationM();
+
+ if (fabs(distance) < SGLimits<float>::min()) {
+ angle = 0;
+ } else {
+ double sAngle = daltM/distance;
+ sAngle = SGMiscd::min(1, SGMiscd::max(-1, sAngle));
+ angle = SGMiscd::rad2deg(asin(sAngle));
}
+
+ return angle;
}
-// end AIBallistic
+double FGAIBallistic::getBearingToHitch() const {
+ //calculate the bearing and range of the second pos from the first
+ double distance = getDistanceToHitch() * SG_FEET_TO_METER;
+ double az1, az2;
+ geo_inverse_wgs_84(pos, _offsetpos, &az1, &az2, &distance);
+
+ return az1;
+}
+
+double FGAIBallistic::getRelBrgHitchToUser() const {
+ //calculate the relative bearing
+ double az1, az2, distance;
+
+ geo_inverse_wgs_84(_offsetpos, globals->get_aircraft_position(), &az1, &az2, &distance);
+
+ double rel_brg = az1 - hdg;
+
+ SG_NORMALIZE_RANGE(rel_brg, -180.0, 180.0);
+
+ return rel_brg;
+}
+
+double FGAIBallistic::getElevHitchToUser() const {
+ // Calculate the distance from the user position
+ SGVec3d carthitchPos = getCartHitchPos();
+ SGVec3d cartuserPos = globals->get_aircraft_position_cart();
+
+ SGVec3d diff = cartuserPos - carthitchPos;
+
+ double distance = norm(diff);
+ double angle = 0;
+
+ double daltM = globals->get_aircraft_position().getElevationM() - _offsetpos.getElevationM();
+
+ // Now the angle, positive angles are upwards
+ if (fabs(distance) < SGLimits<float>::min()) {
+ angle = 0;
+ }
+ else {
+ double sAngle = daltM/distance;
+ sAngle = SGMiscd::min(1, SGMiscd::max(-1, sAngle));
+ angle = SGMiscd::rad2deg(asin(sAngle));
+ }
+
+ return angle;
+}
+
+void FGAIBallistic::setTgtOffsets(double dt, double coeff) {
+ double c = dt / (coeff + dt);
+
+ _x_offset = (_tgt_x_offset * c) + (_x_offset * (1 - c));
+ _y_offset = (_tgt_y_offset * c) + (_y_offset * (1 - c));
+ _z_offset = (_tgt_z_offset * c) + (_z_offset * (1 - c));
+}
+
+void FGAIBallistic::calcVSHS() {
+ // Calculate vertical and horizontal speed components
+ double speed_fps = speed * SG_KT_TO_FPS;
+
+ if (speed == 0.0) {
+ hs = vs = 0.0;
+ }
+ else {
+ vs = sin( _elevation * SG_DEGREES_TO_RADIANS ) * speed_fps;
+ hs = cos( _elevation * SG_DEGREES_TO_RADIANS ) * speed_fps;
+ }
+}
+
+void FGAIBallistic::calcNE() {
+ // Resolve horizontal speed into north and east components:
+ _speed_north_fps = cos(_azimuth / SG_RADIANS_TO_DEGREES) * hs;
+ _speed_east_fps = sin(_azimuth / SG_RADIANS_TO_DEGREES) * hs;
+
+ // Convert horizontal speed (fps) to degrees per second
+ speed_north_deg_sec = _speed_north_fps / ft_per_deg_lat;
+ speed_east_deg_sec = _speed_east_fps / ft_per_deg_lon;
+}
+
+SGVec3d FGAIBallistic::getCartOffsetPos(SGGeod inpos, double user_heading,
+ double user_pitch, double user_roll
+ ) const {
+ // Convert geodetic positions to geocentered
+ SGVec3d cartuserPos = SGVec3d::fromGeod(inpos);
+
+ // Transform to the right coordinate frame, configuration is done in
+ // the x-forward, y-right, z-up coordinates (feet), computation
+ // in the simulation usual body x-forward, y-right, z-down coordinates
+ // (meters) )
+ SGVec3d _off(_x_offset * SG_FEET_TO_METER,
+ _y_offset * SG_FEET_TO_METER,
+ -_z_offset * SG_FEET_TO_METER);
+
+ // Transform the user position to the horizontal local coordinate system.
+ SGQuatd hlTrans = SGQuatd::fromLonLat(inpos);
+
+ // And postrotate the orientation of the user model wrt the horizontal
+ // local frame
+ hlTrans *= SGQuatd::fromYawPitchRollDeg(
+ user_heading,
+ user_pitch,
+ user_roll);
+
+ // The offset converted to the usual body fixed coordinate system
+ // rotated to the earth-fixed coordinates axis
+ SGVec3d off = hlTrans.backTransform(_off);
+
+ // Add the position offset of the user model to get the geocentered position
+ SGVec3d offsetPos = cartuserPos + off;
+
+ return offsetPos;
+}
+
+void FGAIBallistic::setOffsetVelocity(double dt, SGGeod offsetpos) {
+ // Calculate the distance from the previous offset position
+ SGVec3d cartoffsetPos = SGVec3d::fromGeod(offsetpos);
+ SGVec3d diff = cartoffsetPos - _oldcartoffsetPos;
+
+ double distance = norm(diff);
+ // Calculate speed knots
+ speed = (distance / dt) * SG_MPS_TO_KT;
+
+ // Now calulate the angle between the old and current postion positions (degrees)
+ double angle = 0;
+ double daltM = offsetpos.getElevationM() - _oldoffsetpos.getElevationM();
+
+ if (fabs(distance) < SGLimits<float>::min()) {
+ angle = 0;
+ }
+ else {
+ double sAngle = daltM / distance;
+ sAngle = SGMiscd::min(1, SGMiscd::max(-1, sAngle));
+ angle = SGMiscd::rad2deg(asin(sAngle));
+ }
+
+ _elevation = angle;
+
+ // Calculate vertical and horizontal speed components
+ calcVSHS();
+
+ // Calculate the bearing of the new offset position from the old
+ // Don't do this if speed is low
+ //cout << "speed " << speed << endl;
+ if (speed > 0.1) {
+ double az1, az2, dist;
+ geo_inverse_wgs_84(_oldoffsetpos, offsetpos, &az1, &az2, &dist);
+ _azimuth = az1;
+ //cout << "offset az " << _azimuth << endl;
+ }
+ else {
+ _azimuth = hdg;
+ //cout << " slow offset az " << _azimuth << endl;
+ }
+
+ // Resolve horizontal speed into north and east components
+ calcNE();
+
+ // And finally store the new values
+ _oldcartoffsetPos = cartoffsetPos;
+ _oldoffsetpos = offsetpos;
+}
projects / flightgear.git / blobdiff