#include "mrg.hxx"
+const double MasterReferenceGyro::gravity = -32.1740485564;
MasterReferenceGyro::MasterReferenceGyro ( SGPropertyNode *node ) :
- _name(node->getStringValue("name", "master-reference-gyro")),
- _num(node->getIntValue("number", 0))
+_name(node->getStringValue("name", "master-reference-gyro")),
+_num(node->getIntValue("number", 0))
{
}
void
MasterReferenceGyro::init ()
{
- _last_hdg = 0;
- _last_roll = 0;
- _last_pitch = 0;
- _indicated_hdg = 0;
- _indicated_roll = 0;
- _indicated_pitch = 0;
- _indicated_hdg_rate = 0;
- _indicated_roll_rate = 0;
- _indicated_pitch_rate = 0;
- _erect_time = 0;
-
- string branch;
- branch = "/instrumentation/" + _name;
-
- _pitch_in_node = fgGetNode("/orientation/pitch-deg", true);
- _roll_in_node = fgGetNode("/orientation/roll-deg", true);
- _hdg_in_node = fgGetNode("/orientation/heading-deg", true);
- _hdg_mag_in_node = fgGetNode("/orientation/heading-magnetic-deg", true);
- _pitch_rate_node = fgGetNode("/orientation/pitch-rate-degps", true);
- _roll_rate_node = fgGetNode("/orientation/roll-rate-degps", true);
- _yaw_rate_node = fgGetNode("/orientation/yaw-rate-degps", true);
- _g_in_node = fgGetNode("/accelerations/pilot-g", true);
- _electrical_node = fgGetNode("/systems/electrical/outputs/MRG", true);
- _hdg_mag_in_node = fgGetNode("/orientation/heading-magnetic-deg", true);
-
- SGPropertyNode *node = fgGetNode(branch.c_str(), _num, true );
- _off_node = node->getChild("off-flag", 0, true);
- _pitch_out_node = node->getChild("indicated-pitch-deg", 0, true);
- _roll_out_node = node->getChild("indicated-roll-deg", 0, true);
- _hdg_out_node = node->getChild("indicated-hdg-deg", 0, true);
- _hdg_mag_out_node = node->getChild("indicated-mag-hdg-deg", 0, true);
- _pitch_rate_out_node = node->getChild("indicated-pitch-rate-degps", 0, true);
- _roll_rate_out_node = node->getChild("indicated-roll-rate-degps", 0, true);
- _hdg_rate_out_node = node->getChild("indicated-hdg-rate-degps", 0, true);
- _responsiveness_node = node->getChild("responsiveness", 0, true);
- _error_out_node = node->getChild("heading-bug-error-deg", 0, true);
- _hdg_input_source_node = node->getChild("heading-source", 0, true);
- _fast_erect_node = node->getChild("fast-erect", 0, true);
-
- _electrical_node->setDoubleValue(0);
- _responsiveness_node->setDoubleValue(0.75);
- _off_node->setBoolValue(false);
- _hdg_input_source_node->setBoolValue(false);
- _fast_erect_node->setBoolValue(false);
+ _last_hdg = 0;
+ _last_roll = 0;
+ _last_pitch = 0;
+ _indicated_hdg = 0;
+ _indicated_roll = 0;
+ _indicated_pitch = 0;
+ _indicated_hdg_rate = 0;
+ _indicated_roll_rate = 0;
+ _indicated_pitch_rate = 0;
+ _erect_time = 180;
+ _last_g = 1;
+ _g_error = 10;
+
+ string branch;
+ branch = "/instrumentation/" + _name;
+
+ _pitch_in_node = fgGetNode("/orientation/pitch-deg", true);
+ _roll_in_node = fgGetNode("/orientation/roll-deg", true);
+ _hdg_in_node = fgGetNode("/orientation/heading-deg", true);
+ _hdg_mag_in_node = fgGetNode("/orientation/heading-magnetic-deg", true);
+ _pitch_rate_node = fgGetNode("/orientation/pitch-rate-degps", true);
+ _roll_rate_node = fgGetNode("/orientation/roll-rate-degps", true);
+ _yaw_rate_node = fgGetNode("/orientation/yaw-rate-degps", true);
+ //_g_in_node = fgGetNode("/accelerations/pilot/z-accel-fps_sec", true);
+ _g_in_node = fgGetNode("/accelerations/pilot-g", true);
+ _electrical_node = fgGetNode("/systems/electrical/outputs/MRG", true);
+ _hdg_mag_in_node = fgGetNode("/orientation/heading-magnetic-deg", true);
+
+ SGPropertyNode *node = fgGetNode(branch.c_str(), _num, true );
+ _off_node = node->getChild("off-flag", 0, true);
+ _pitch_out_node = node->getChild("indicated-pitch-deg", 0, true);
+ _roll_out_node = node->getChild("indicated-roll-deg", 0, true);
+ _hdg_out_node = node->getChild("indicated-hdg-deg", 0, true);
+ _hdg_mag_out_node = node->getChild("indicated-mag-hdg-deg", 0, true);
+ _pitch_rate_out_node = node->getChild("indicated-pitch-rate-degps", 0, true);
+ _roll_rate_out_node = node->getChild("indicated-roll-rate-degps", 0, true);
+ _hdg_rate_out_node = node->getChild("indicated-hdg-rate-degps", 0, true);
+ _responsiveness_node = node->getChild("responsiveness", 0, true);
+ _error_out_node = node->getChild("heading-bug-error-deg", 0, true);
+ _hdg_input_source_node = node->getChild("heading-source", 0, true);
+ _fast_erect_node = node->getChild("fast-erect", 0, true);
+
+ _electrical_node->setDoubleValue(0);
+ _responsiveness_node->setDoubleValue(0.75);
+ _off_node->setBoolValue(false);
+ _hdg_input_source_node->setBoolValue(false);
+ _fast_erect_node->setBoolValue(false);
+ _g_in_node->setDoubleValue(1);
}
void
MasterReferenceGyro::bind ()
{
- std::ostringstream temp;
- string branch;
- temp << _num;
- branch = "/instrumentation/" + _name + "[" + temp.str() + "]";
-
- fgTie((branch + "/serviceable").c_str(),
- &_gyro, &Gyro::is_serviceable, &Gyro::set_serviceable);
- fgTie((branch + "/spin").c_str(),
- &_gyro, &Gyro::get_spin_norm, &Gyro::set_spin_norm);
+ std::ostringstream temp;
+ string branch;
+ temp << _num;
+ branch = "/instrumentation/" + _name + "[" + temp.str() + "]";
+
+ fgTie((branch + "/serviceable").c_str(),
+ &_gyro, &Gyro::is_serviceable, &Gyro::set_serviceable);
+ fgTie((branch + "/spin").c_str(),
+ &_gyro, &Gyro::get_spin_norm, &Gyro::set_spin_norm);
}
void
MasterReferenceGyro::unbind ()
{
- std::ostringstream temp;
- string branch;
- temp << _num;
- branch = "/instrumentation/" + _name + "[" + temp.str() + "]";
+ std::ostringstream temp;
+ string branch;
+ temp << _num;
+ branch = "/instrumentation/" + _name + "[" + temp.str() + "]";
- fgUntie((branch + "/serviceable").c_str());
- fgUntie((branch + "/spin").c_str());
+ fgUntie((branch + "/serviceable").c_str());
+ fgUntie((branch + "/spin").c_str());
}
void
MasterReferenceGyro::update (double dt)
{
- double indicated_roll = 0;
- double indicated_pitch = 0;
- double indicated_hdg = 0;
- double indicated_roll_rate = 0;
- double indicated_pitch_rate = 0;
- double indicated_hdg_rate = 0;
-
- // Get the spin from the gyro
- _gyro.set_power_norm( _electrical_node->getDoubleValue()/24 );
- _gyro.update(dt);
- double spin = _gyro.get_spin_norm();
-
- // set the "off-flag"
- if ( _electrical_node->getDoubleValue() > 0 && spin >= 0.25) {
- _off_node->setBoolValue(false);
- } else {
- _off_node->setBoolValue(true);
+ //sanity check
+ if (!fgGetBool("/sim/fdm-initialized", false)) {
return;
- }
-
- // Get the input values
- double hdg = _hdg_mag_in_node->getDoubleValue();
-
- if(_hdg_input_source_node->getBoolValue())
- hdg = _hdg_in_node->getDoubleValue();
-
- double roll = _roll_in_node->getDoubleValue();
- double pitch = _pitch_in_node->getDoubleValue();
-
- double roll_rate = _yaw_rate_node->getDoubleValue();
- double pitch_rate = _yaw_rate_node->getDoubleValue();
- double yaw_rate = _yaw_rate_node->getDoubleValue();
- double g = _g_in_node->getDoubleValue();
-
- //modulate the input by the spin rate
- double responsiveness = spin * spin * spin * spin * spin * spin;
- roll = fgGetLowPass( _last_roll, roll, responsiveness );
- pitch = fgGetLowPass( _last_pitch , pitch, responsiveness );
-
- if ((hdg - _last_hdg) > 180)
- _last_hdg += 360;
- if ((hdg - _last_hdg) < -180)
- _last_hdg -= 360;
-
- hdg = fgGetLowPass( _last_hdg , hdg, responsiveness );
+ }
- //but we need to filter the hdg and yaw_rate as well - yuk!
- responsiveness = 0.1 / (spin * spin * spin * spin * spin * spin);
- yaw_rate = fgGetLowPass( _last_yaw_rate , yaw_rate, responsiveness );
- g = fgGetLowPass( _last_g , g, 0.015 );
+ double indicated_roll = 0;
+ double indicated_pitch = 0;
+ double indicated_hdg = 0;
+ double indicated_roll_rate = 0;
+ double indicated_pitch_rate = 0;
+ double indicated_hdg_rate = 0;
+ double hdg = 0;
+ double erect_time_factor = 1;
+
+ const double erect_time = 180;
+ const double max_g_error = 10.0;
+
+ //Get the spin from the gyro
+ _gyro.set_power_norm( _electrical_node->getDoubleValue()/24 );
+ _gyro.update(dt);
+ double spin = _gyro.get_spin_norm();
+
+ // set the "off-flag"
+ if ( _electrical_node->getDoubleValue() > 0 && spin >= 0.25) {
+ _off_node->setBoolValue(false);
+ } else {
+ _off_node->setBoolValue(true);
+ return;
+ }
+ // Get the input values
+ if(_hdg_input_source_node->getBoolValue()){
+ hdg = _hdg_in_node->getDoubleValue();
+ } else {
+ hdg = _hdg_mag_in_node->getDoubleValue();
+ }
- // store the new values
- _last_roll = roll;
- _last_pitch = pitch;
- _last_hdg = hdg;
- _last_roll_rate = roll_rate;
- _last_pitch_rate = pitch_rate;
- _last_yaw_rate = yaw_rate;
- _last_g = g;
+ double roll = _roll_in_node->getDoubleValue();
+ double pitch = _pitch_in_node->getDoubleValue();
+ double g = _g_in_node->getDoubleValue()/* / gravity*/;
+
+ double roll_rate = _yaw_rate_node->getDoubleValue();
+ double pitch_rate = _pitch_rate_node->getDoubleValue();
+ double yaw_rate = _yaw_rate_node->getDoubleValue();
+
+ //modulate the input by the spin rate
+ double responsiveness = spin * spin * spin * spin * spin * spin;
+ roll = fgGetLowPass( _last_roll, roll, responsiveness );
+ pitch = fgGetLowPass( _last_pitch , pitch, responsiveness );
+
+ if ((hdg - _last_hdg) > 180)
+ _last_hdg += 360;
+ if ((hdg - _last_hdg) < -180)
+ _last_hdg -= 360;
+
+ hdg = fgGetLowPass( _last_hdg , hdg, responsiveness );
+
+ //but we need to filter the hdg and yaw_rate as well - yuk!
+ responsiveness = 0.1 / (spin * spin * spin * spin * spin * spin);
+ yaw_rate = fgGetLowPass( _last_yaw_rate , yaw_rate, responsiveness );
+ g = fgGetLowPass( _last_g , g, 1.5);
+
+
+ // store the new values
+ _last_roll = roll;
+ _last_pitch = pitch;
+ _last_hdg = hdg;
+ _last_roll_rate = roll_rate;
+ _last_pitch_rate = pitch_rate;
+ _last_yaw_rate = yaw_rate;
+ _last_g = g;
+
+ //the gyro only erects inside limits
+ if ( fabs ( yaw_rate ) <= 5
+ && g <= 1.5 && g >= -0.5){
+
+ if ( !_fast_erect_node->getBoolValue() ){
+ erect_time_factor = 1;
+ } else {
+ erect_time_factor = 2;
+ }
+
+ _g_error -= (max_g_error/(erect_time * 0.33)) * dt * erect_time_factor;
+ } else {
+ _g_error += (max_g_error /(erect_time * 0.33)) * dt * 2;
+
+ //SG_LOG(SG_GENERAL, SG_ALERT,_num <<
+ // " g input " << _g_in_node->getDoubleValue() * gravity
+ // <<" _erect_time " << _erect_time
+ // << " yaw " << yaw_rate
+ // << " pitch " << _pitch_rate_node->getDoubleValue()
+ // << " roll " << _roll_rate_node->getDoubleValue());
- if (_erect_time > 0){
+ }
- if ( !_fast_erect_node->getBoolValue() )
- _erect_time -= dt;
- else
- _erect_time -= 2 * dt;
+ //cout << "_g_error "<< _g_error << endl;
+ _g_error = SGMiscd::clip(_g_error, 0, 10);
+// cout << "_g_error clip "<< _g_error << endl;
+ indicated_roll = _last_roll + _g_error;
+ indicated_pitch = _last_pitch + _g_error;
+ indicated_hdg = _last_hdg + _g_error;
+ indicated_roll_rate = _last_roll_rate;
+ indicated_pitch_rate = _last_pitch_rate;
+ indicated_hdg_rate = _last_yaw_rate;
+ // calculate the difference between the indicated heading
+ // and the selected heading for use with an autopilot
+ static SGPropertyNode *bnode
+ = fgGetNode( "/autopilot/settings/heading-bug-deg", false );
+
+ if ( bnode ) {
+ double diff = bnode->getDoubleValue() - indicated_hdg;
+ if ( diff < -180.0 ) { diff += 360.0; }
+ if ( diff > 180.0 ) { diff -= 360.0; }
+ _error_out_node->setDoubleValue( diff );
+ //SG_LOG(SG_GENERAL, SG_ALERT,
+ //"autopilot input " << bnode->getDoubleValue()
+ //<< " output " << _error_out_node->getDoubleValue()<<);
+ }
+ //smooth the output
+ double factor = _responsiveness_node->getDoubleValue() * dt;
+
+ indicated_roll = fgGetLowPass( _indicated_roll, indicated_roll, factor );
+ indicated_pitch = fgGetLowPass( _indicated_pitch , indicated_pitch, factor );
+ //indicated_hdg = fgGetLowPass( _indicated_hdg , indicated_hdg, factor );
+
+ indicated_roll_rate = fgGetLowPass( _indicated_roll_rate, indicated_roll_rate, factor );
+ indicated_pitch_rate = fgGetLowPass( _indicated_pitch_rate , indicated_pitch_rate, factor );
+ indicated_hdg_rate = fgGetLowPass( _indicated_hdg_rate , indicated_hdg_rate, factor );
+
+ // store the new values
+ _indicated_roll = indicated_roll;
+ _indicated_pitch = indicated_pitch;
+ _indicated_hdg = indicated_hdg;
+
+ _indicated_roll_rate = indicated_roll_rate;
+ _indicated_pitch_rate = indicated_pitch_rate;
+ _indicated_hdg_rate = indicated_hdg_rate;
+
+ // add in a gyro underspin "error" if gyro is spinning too slowly
+ const double spin_thresh = 0.8;
+ const double max_roll_error = 40.0;
+ const double max_pitch_error = 12.0;
+ const double max_hdg_error = 140.0;
+ double roll_error;
+ double pitch_error;
+ double hdg_error;
+
+ if ( spin <= spin_thresh ) {
+ double roll_error_factor = ( spin_thresh - spin ) / spin_thresh;
+ double pitch_error_factor = ( spin_thresh - spin ) / spin_thresh;
+ double hdg_error_factor = ( spin_thresh - spin ) / spin_thresh;
+ roll_error = roll_error_factor * roll_error_factor * max_roll_error;
+ pitch_error = pitch_error_factor * pitch_error_factor * max_pitch_error;
+ hdg_error = hdg_error_factor * hdg_error_factor * max_hdg_error;
+ } else {
+ roll_error = 0.0;
+ pitch_error = 0.0;
+ hdg_error = 0.0;
}
- //SG_LOG(SG_GENERAL, SG_ALERT,
- // "g input " << g <<" _erect_time " << _erect_time << " spin " << spin);
-
- //the gyro only erects inside limits
- if ( fabs ( yaw_rate ) <= 5
- && ( g <= 1.5 || g >= -0.5)
- && _erect_time <=0 ) {
- indicated_roll = _last_roll;
- indicated_pitch = _last_pitch;
- indicated_hdg = _last_hdg;
- indicated_roll_rate = _last_roll_rate;
- indicated_pitch_rate = _last_pitch_rate;
- indicated_hdg_rate = _last_yaw_rate;
- } else {
- indicated_roll_rate = 0;
- indicated_pitch_rate = 0;
- indicated_hdg_rate = 0;
-
- if (_erect_time <= 0 )
- _erect_time = 34;
-
- }
-
- // calculate the difference between the indicated heading
- // and the selected heading for use with an autopilot
- static SGPropertyNode *bnode
- = fgGetNode( "/autopilot/settings/heading-bug-deg", false );
-
- if ( bnode ) {
- double diff = bnode->getDoubleValue() - indicated_hdg;
- if ( diff < -180.0 ) { diff += 360.0; }
- if ( diff > 180.0 ) { diff -= 360.0; }
- _error_out_node->setDoubleValue( diff );
- //SG_LOG(SG_GENERAL, SG_ALERT,
- //"autopilot input " << bnode->getDoubleValue()
- //<< " output " << _error_out_node->getDoubleValue()<<);
- }
-
- //smooth the output
- double factor = _responsiveness_node->getDoubleValue() * dt;
-
- indicated_roll = fgGetLowPass( _indicated_roll, indicated_roll, factor );
- indicated_pitch = fgGetLowPass( _indicated_pitch , indicated_pitch, factor );
- //indicated_hdg = fgGetLowPass( _indicated_hdg , indicated_hdg, factor );
-
- indicated_roll_rate = fgGetLowPass( _indicated_roll_rate, indicated_roll_rate, factor );
- indicated_pitch_rate = fgGetLowPass( _indicated_pitch_rate , indicated_pitch_rate, factor );
- indicated_hdg_rate = fgGetLowPass( _indicated_hdg_rate , indicated_hdg_rate, factor );
-
- // store the new values
- _indicated_roll = indicated_roll;
- _indicated_pitch = indicated_pitch;
- _indicated_hdg = indicated_hdg;
-
- _indicated_roll_rate = indicated_roll_rate;
- _indicated_pitch_rate = indicated_pitch_rate;
- _indicated_hdg_rate = indicated_hdg_rate;
-
- // add in a gyro underspin "error" if gyro is spinning too slowly
- const double spin_thresh = 0.8;
- const double max_roll_error = 40.0;
- const double max_pitch_error = 12.0;
- const double max_hdg_error = 140.0;
- double roll_error;
- double pitch_error;
- double hdg_error;
-
- if ( spin <= spin_thresh ) {
- double roll_error_factor = ( spin_thresh - spin ) / spin_thresh;
- double pitch_error_factor = ( spin_thresh - spin ) / spin_thresh;
- double hdg_error_factor = ( spin_thresh - spin ) / spin_thresh;
- roll_error = roll_error_factor * roll_error_factor * max_roll_error;
- pitch_error = pitch_error_factor * pitch_error_factor * max_pitch_error;
- hdg_error = hdg_error_factor * hdg_error_factor * max_hdg_error;
- } else {
- roll_error = 0.0;
- pitch_error = 0.0;
- hdg_error = 0.0;
- }
-
- _roll_out_node->setDoubleValue( _indicated_roll + roll_error );
- _pitch_out_node->setDoubleValue( _indicated_pitch + pitch_error );
- _hdg_out_node->setDoubleValue( _indicated_hdg + hdg_error );
- _pitch_rate_out_node ->setDoubleValue( _indicated_pitch_rate );
- _roll_rate_out_node ->setDoubleValue( _indicated_roll_rate );
- _hdg_rate_out_node ->setDoubleValue( _indicated_hdg_rate );
+ _roll_out_node->setDoubleValue( _indicated_roll + roll_error );
+ _pitch_out_node->setDoubleValue( _indicated_pitch + pitch_error );
+ _hdg_out_node->setDoubleValue( _indicated_hdg + hdg_error );
+ _pitch_rate_out_node ->setDoubleValue( _indicated_pitch_rate );
+ _roll_rate_out_node ->setDoubleValue( _indicated_roll_rate );
+ _hdg_rate_out_node ->setDoubleValue( _indicated_hdg_rate );
}
// end of mrg.cxx
projects / flightgear.git / commitdiff