]> git.mxchange.org Git - flightgear.git/blobdiff - src/Instrumentation/mrg.cxx
Merge branch 'maint2' into next
[flightgear.git] / src / Instrumentation / mrg.cxx
index 918160ae54eaf8053c4a4e293cb8afe4a61a0a24..69b220d7f9204554d58ba6f529d9481be5cc59a4 100644 (file)
@@ -1,5 +1,5 @@
-// MRG.cxx - an electrcally powered master reference gyro.
-// Written by Vivian Meazza based on wrok by David Megginson, started 2006.
+// MRG.cxx - an electrically powered master reference gyro.
+// Written by Vivian Meazza based on work by David Megginson, started 2006.
 //
 // This file is in the Public Domain and comes with no warranty.
 
@@ -7,9 +7,11 @@
 // - better spin-up
 
 #include <simgear/compiler.h>
+#include <simgear/sg_inlines.h>
 
-#include STL_IOSTREAM
-#include STL_STRING
+
+#include <iostream>
+#include <string>
 #include <sstream>
 #include <math.h>      // fabs()
 
 
 
 MasterReferenceGyro::MasterReferenceGyro ( SGPropertyNode *node ) :
-       name("master-reference-gyro"),
-       num(0)
-{
-       int i;
-       for ( i = 0; i < node->nChildren(); ++i ) {
-               SGPropertyNode *child = node->getChild(i);
-               string cname = child->getName();
-               string cval = child->getStringValue();
-               if ( cname == "name" ) {
-                       name = cval;
-               } else if ( cname == "number" ) {
-                       num = (int) child->getDoubleValue();
-               } else {
-                       SG_LOG( SG_INSTR, SG_WARN, "Error in mrg config logic" );
-                       if ( name.length() ) {
-                               SG_LOG( SG_INSTR, SG_WARN, "Section = " << name );
-                       }
-               }
-       }
-}
-
-MasterReferenceGyro::MasterReferenceGyro ()
+       _name(node->getStringValue("name", "master-reference-gyro")),
+       _num(node->getIntValue("number", 0))
 {
 }
 
@@ -63,31 +45,36 @@ MasterReferenceGyro::init ()
        _indicated_pitch_rate = 0;
        
        string branch;
-       branch = "/instrumentation/" + name;
+       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-damped", 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 );
+       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-error-deg", 0, true);
+       _error_out_node = node->getChild("heading-bug-error-deg", 0, true);
+       _hdg_input_source_node = node->getChild("heading-source", 0, true);
 
        _electrical_node->setDoubleValue(0);
        _responsiveness_node->setDoubleValue(0.75);
        _off_node->setBoolValue(false);
+       _hdg_input_source_node->setBoolValue(false);
 }
 
 void
@@ -95,8 +82,8 @@ MasterReferenceGyro::bind ()
 {
        std::ostringstream temp;
        string branch;
-       temp << num;
-       branch = "/instrumentation/" + name + "[" + temp.str() + "]";
+       temp << _num;
+       branch = "/instrumentation/" + _name + "[" + temp.str() + "]";
 
        fgTie((branch + "/serviceable").c_str(),
                &_gyro, &Gyro::is_serviceable, &Gyro::set_serviceable);
@@ -109,8 +96,8 @@ MasterReferenceGyro::unbind ()
 {
        std::ostringstream temp;
        string branch;
-       temp << num;
-       branch = "/instrumentation/" + name + "[" + temp.str() + "]";
+       temp << _num;
+       branch = "/instrumentation/" + _name + "[" + temp.str() + "]";
 
        fgUntie((branch + "/serviceable").c_str());
        fgUntie((branch + "/spin").c_str());
@@ -141,22 +128,35 @@ MasterReferenceGyro::update (double dt)
        }
 
        // 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 hdg = _hdg_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 , yaw_rate, 0.15 );
 
        // store the new values
        _last_roll = roll;
@@ -165,9 +165,10 @@ MasterReferenceGyro::update (double dt)
        _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 ( abs ( yaw_rate ) <= 5
+       if ( fabs ( yaw_rate ) <= 5
                        && (_g_in_node->getDoubleValue() <= 1.5
                        || _g_in_node->getDoubleValue() >= -0.5) ) {
                indicated_roll = _last_roll;
@@ -185,21 +186,24 @@ MasterReferenceGyro::update (double dt)
        // calculate the difference between the indicated heading
        // and the selected heading for use with an autopilot
        static SGPropertyNode *bnode
-               = fgGetNode( "autopilot/settings/target-heading-deg", false );
+               = 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()<<);
        }
-       //cout << "autopilot input " << bnode->getDoubleValue() << "output " << _error_out_node->getDoubleValue()<<endl ;
+       
        //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_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 );