]> git.mxchange.org Git - flightgear.git/blobdiff - src/Instrumentation/airspeed_indicator.cxx
James Turner:
[flightgear.git] / src / Instrumentation / airspeed_indicator.cxx
index 5ae7543324d253e23a919e979154a7106ed845eb..0196ddbaef9bd20b3d420f1c0f78ae0f868b9af0 100644 (file)
 // A higher number means more responsive.
 #define RESPONSIVENESS 50.0
 
-
-AirspeedIndicator::AirspeedIndicator ()
+AirspeedIndicator::AirspeedIndicator ( SGPropertyNode *node )
+    :
+    _name(node->getStringValue("name", "airspeed-indicator")),
+    _num(node->getIntValue("number", 0)),
+    _total_pressure(node->getStringValue("total-pressure", "/systems/pitot/total-pressure-inhg")),
+    _static_pressure(node->getStringValue("static-pressure", "/systems/static/pressure-inhg"))
 {
 }
 
@@ -27,22 +31,17 @@ AirspeedIndicator::~AirspeedIndicator ()
 void
 AirspeedIndicator::init ()
 {
-    _serviceable_node =
-        fgGetNode("/instrumentation/airspeed-indicator/serviceable",
-                  true);
-    _total_pressure_node =
-        fgGetNode("/systems/pitot/total-pressure-inhg", true);
-    _static_pressure_node =
-        fgGetNode("/systems/static/pressure-inhg", true);
-    _speed_node =
-        fgGetNode("/instrumentation/airspeed-indicator/indicated-speed-kt",
-                  true);
+    string branch;
+    branch = "/instrumentation/" + _name;
+
+    SGPropertyNode *node = fgGetNode(branch.c_str(), _num, true );
+    _serviceable_node = node->getChild("serviceable", 0, true);
+    _total_pressure_node = fgGetNode(_total_pressure.c_str(), true);
+    _static_pressure_node = fgGetNode(_static_pressure.c_str(), true);
+    _density_node = fgGetNode("/environment/density-slugft3", true);
+    _speed_node = node->getChild("indicated-speed-kt", 0, true);
 }
 
-#ifndef SEA_LEVEL_DENSITY_SLUGFG3
-# define SEA_LEVEL_DENSITY_SLUGFT3 0.002378
-#endif
-
 #ifndef FPSTOKTS
 # define FPSTOKTS 0.592484
 #endif
@@ -55,14 +54,15 @@ void
 AirspeedIndicator::update (double dt)
 {
     if (_serviceable_node->getBoolValue()) {
-        double pt = _total_pressure_node->getDoubleValue();
-        double p = _static_pressure_node->getDoubleValue();
-        double q = ( pt - p ) * INHGTOPSF;      // dynamic pressure
+        double pt = _total_pressure_node->getDoubleValue() * INHGTOPSF;
+        double p = _static_pressure_node->getDoubleValue() * INHGTOPSF;
+        double r = _density_node->getDoubleValue();
+        double q = ( pt - p );  // dynamic pressure
 
         // Now, reverse the equation (normalize dynamic pressure to
         // avoid "nan" results from sqrt)
         if ( q < 0 ) { q = 0.0; }
-        double v_fps = sqrt((2 * q) / SEA_LEVEL_DENSITY_SLUGFT3);
+        double v_fps = sqrt((2 * q) / r);
 
                                 // Publish the indicated airspeed
         double last_speed_kt = _speed_node->getDoubleValue();