]> git.mxchange.org Git - flightgear.git/commitdiff
Updates to the OpenGC interface from John Wojnaroski.
authorcurt <curt>
Thu, 27 Jun 2002 22:26:47 +0000 (22:26 +0000)
committercurt <curt>
Thu, 27 Jun 2002 22:26:47 +0000 (22:26 +0000)
src/Network/opengc.cxx
src/Network/opengc.hxx
src/Network/opengc_data.hxx

index 00a62c2452d36d7a1e543ca75fd4d618be781aeb..ec5cf49d17fa8672d9dc8cceb53f8ca75c5eec12 100644 (file)
 
 SG_USING_STD(vector);
 
-FGOpenGC::FGOpenGC() {
+FGOpenGC::FGOpenGC() : 
+       press_node(fgGetNode("/environment/pressure-inhg", true)),
+       temp_node(fgGetNode("/environment/temperature-degc", true)),
+       wind_dir_node(fgGetNode("/environment/wind-from-heading-deg", true)),
+       wind_speed_node(fgGetNode("/environment/wind-speed-kt", true)),
+       p_left_aileron(fgGetNode("surface-positions/left-aileron-pos-norm", true)),
+       p_right_aileron(fgGetNode("surface-positions/right-aileron-pos-norm", true)),
+       p_elevator(fgGetNode("surface-positions/elevator-pos-norm", true)),
+       p_elevator_trim(fgGetNode("surface-positions/elevator_trim-pos-norm", true)),
+       p_rudder(fgGetNode("surface-positions/rudder-pos-norm", true)),
+       p_flaps(fgGetNode("surface-positions/flap-pos-norm", true)),
+       p_flaps_cmd(fgGetNode("/controls/flaps", true)),
+       p_alphadot(fgGetNode("/fdm/jsbsim/aero/alphadot-radsec", true)),
+       p_betadot(fgGetNode("/fdm/jsbsim/aero/betadot-radsec", true))
+{
 }
 
 FGOpenGC::~FGOpenGC() {
@@ -66,10 +80,10 @@ bool FGOpenGC::open() {
     return true;
 }
 
-
-static void collect_data( const FGInterface *fdm, ogcFGData *data ) {
-                                                                                               
-    data->version_id = 0x0012;
+//static void collect_data( const FGInterface *fdm, ogcFGData *data ) {
+void FGOpenGC::collect_data( const FGInterface *fdm, ogcFGData *data ) {       
+                                                                                       
+    data->version_id = OGC_VERSION;
 
     data->longitude = cur_fdm_state->get_Longitude_deg();   
     data->latitude = cur_fdm_state->get_Latitude_deg();
@@ -84,7 +98,7 @@ static void collect_data( const FGInterface *fdm, ogcFGData *data ) {
     data->vvi = cur_fdm_state->get_Climb_Rate();
     data->mach = cur_fdm_state->get_Mach_number();
     data->groundspeed = cur_fdm_state->get_V_ground_speed();
-    data->v_tas = cur_fdm_state->get_V_equiv_kts();
+    data->v_keas = cur_fdm_state->get_V_equiv_kts();
 
     data->phi_dot = cur_fdm_state->get_Phi_dot();
     data->theta_dot = cur_fdm_state->get_Theta_dot();
@@ -92,23 +106,25 @@ static void collect_data( const FGInterface *fdm, ogcFGData *data ) {
 
     data->alpha = cur_fdm_state->get_Alpha();
     data->beta = cur_fdm_state->get_Beta();
-    data->alpha_dot = cur_fdm_state->get_Alpha_dot();
-    data->beta_dot = cur_fdm_state->get_Beta_dot();
-
-    data->aileron = globals->get_controls()->get_aileron();
-    //data->aileron_trim = p_Controls->get_aileron_trim();
-    data->elevator = globals->get_controls()->get_elevator();
-    data->elevator_trim = globals->get_controls()->get_elevator_trim();
-    data->rudder = globals->get_controls()->get_rudder();
+    data->alpha_dot = p_alphadot->getDoubleValue();
+    data->beta_dot = p_betadot->getDoubleValue();
+    
     //data->rudder_trim = p_Controls->get_rudder_trim();
-    //data->flaps = fgGetDouble("/controls/flaps");
-    data->flaps = globals->get_controls()->get_flaps();
-
-    //data->gear_nose = p_gear[0]->GetPosition();
-    //data->gear_left = p_gear[1]->GetPosition();
-    //data->gear_right = p_gear[2]->GetPosition();
-
+    
+    data->left_aileron = p_left_aileron->getDoubleValue();
+    data->right_aileron = p_right_aileron->getDoubleValue();
+    data->elevator = p_elevator->getDoubleValue();
+    data->elevator_trim = p_elevator_trim->getDoubleValue();
+    data->rudder = p_rudder->getDoubleValue();
+    data->flaps = p_flaps->getDoubleValue();
+    data->flaps_cmd = p_flaps_cmd->getDoubleValue();
+
+    data->gear_nose = fgGetDouble("gear/gear[0]/position-norm");
+    data->gear_nose = fgGetDouble("gear/gear[1]/position-norm");
+    data->gear_nose = fgGetDouble("gear/gear[2]/position-norm");
+         data->gear_nose = fgGetDouble("gear/gear[3]/position-norm");
+         data->gear_nose = fgGetDouble("gear/gear[4]/position-norm");
+         
     data->rpm[0] = fgGetDouble("/engines/engine[0]/rpm");
     data->rpm[1] = fgGetDouble("/engines/engine[1]/rpm");   
 
@@ -116,11 +132,11 @@ static void collect_data( const FGInterface *fdm, ogcFGData *data ) {
     data->epr[1] = fgGetDouble("/engines/engine[1]/epr");
     data->epr[2] = fgGetDouble("/engines/engine[2]/epr");
     data->epr[3] = fgGetDouble("/engines/engine[3]/epr");
-
-    data->egt[0] = fgGetDouble("/engines/engine[0]/egt-degf");
-    data->egt[1] = fgGetDouble("/engines/engine[1]/egt-degf");
-    data->egt[2] = fgGetDouble("/engines/engine[2]/egt-degf");
-    data->egt[3] = fgGetDouble("/engines/engine[3]/egt-degf");
+    
+    data->egt[0] = (fgGetDouble("/engines/engine[0]/egt-degf") - 32.0) * 0.555;
+    data->egt[1] = (fgGetDouble("/engines/engine[1]/egt-degf") - 32.0) * 0.555;
+    data->egt[2] = (fgGetDouble("/engines/engine[2]/egt-degf") - 32.0) * 0.555;
+    data->egt[3] = (fgGetDouble("/engines/engine[3]/egt-degf") - 32.0) * 0.555;
 
     data->n2_turbine[0] = fgGetDouble("/engines/engine[0]/n2");
     data->n2_turbine[1] = fgGetDouble("/engines/engine[1]/n2");
@@ -131,25 +147,30 @@ static void collect_data( const FGInterface *fdm, ogcFGData *data ) {
     data->n1_turbine[1] = fgGetDouble("/engines/engine[1]/n1");
     data->n1_turbine[2] = fgGetDouble("/engines/engine[2]/n1");
     data->n1_turbine[3] = fgGetDouble("/engines/engine[3]/n1");
-
-    data->fuel_flow[0] = fgGetDouble("/engines/engine[0]/fuel-flow-gph");
-    data->fuel_flow[1] = fgGetDouble("/engines/engine[1]/fuel-flow-gph");
-    data->fuel_flow[1] = fgGetDouble("/engines/engine[1]/fuel-flow-gph");
-    data->fuel_flow[2] = fgGetDouble("/engines/engine[2]/fuel-flow-gph");
+// Convert gph to pph for turbine engines
+    data->fuel_flow[0] = fgGetDouble("/engines/engine[0]/fuel-flow-gph") * 6.5;
+    data->fuel_flow[1] = fgGetDouble("/engines/engine[1]/fuel-flow-gph") * 6.5;
+    data->fuel_flow[2] = fgGetDouble("/engines/engine[2]/fuel-flow-gph") * 6.5;
+    data->fuel_flow[3] = fgGetDouble("/engines/engine[3]/fuel-flow-gph") * 6.5;
 
     data->oil_pressure[0] = fgGetDouble("/engines/engine[0]/oil-pressure-psi");
     data->oil_pressure[1] = fgGetDouble("/engines/engine[1]/oil-pressure-psi");
     data->oil_pressure[2] = fgGetDouble("/engines/engine[2]/oil-pressure-psi");
     data->oil_pressure[3] = fgGetDouble("/engines/engine[3]/oil-pressure-psi");
+// Just a few test numbers to test interface and drive EICAS displayss    
+    for (int j=0; j<4; j++) data->oil_pressure[j] = 100.4 + 2.3*j;
 
     data->man_pressure[0] = fgGetDouble("/engines/engine[0]/mp-osi");
     data->man_pressure[1] = fgGetDouble("/engines/engine[1]/mp-osi");    
 
-    data->static_temperature = cur_fdm_state->get_Static_temperature();
     data->total_temperature = cur_fdm_state->get_Total_temperature();
-    data->static_pressure = cur_fdm_state->get_Static_pressure();
     data->total_pressure = cur_fdm_state->get_Total_pressure();
     data->dynamic_pressure = cur_fdm_state->get_Dynamic_pressure();
+    
+    data->static_pressure = press_node->getDoubleValue();
+    data->static_temperature = temp_node->getDoubleValue();
+    data->wind = wind_speed_node->getDoubleValue();
+    data->wind_dir =  wind_dir_node->getDoubleValue();
 }
 
 static void distribute_data( const ogcFGData *data, FGInterface *chunk ) {
index ec4d393c2fabe9b229b1c7787d537eb77cacc4ea..e22871d06b926da071c9741f742d0455f61d4e19 100644 (file)
@@ -31,6 +31,7 @@
 #include STL_STRING
 
 #include <FDM/flight.hxx>
+#include <Main/fg_props.hxx>
 
 #include "protocol.hxx"
 #include "opengc_data.hxx"
@@ -39,6 +40,25 @@ class FGOpenGC : public FGProtocol, public FGInterface {
 
     ogcFGData buf;
     int length;
+    
+    SGPropertyNode *press_node;
+    SGPropertyNode *temp_node;
+    SGPropertyNode *wind_dir_node;
+    SGPropertyNode *wind_speed_node;
+    SGPropertyNode *epr0_node;
+    
+    // Control surfaces
+    SGPropertyNode *p_left_aileron;
+    SGPropertyNode *p_right_aileron;
+    SGPropertyNode *p_elevator;
+    SGPropertyNode *p_elevator_trim;
+    SGPropertyNode *p_rudder;
+    SGPropertyNode *p_flaps;
+    SGPropertyNode *p_flaps_cmd;
+    
+    // Aero numbers
+    SGPropertyNode *p_alphadot;
+    SGPropertyNode *p_betadot;
 
 public:
 
@@ -54,7 +74,7 @@ public:
     // close the channel
     bool close();
 
-   
+    void collect_data( const FGInterface *fdm, ogcFGData *data );
 };
 
 #endif // _FG_OPENGC_HXX
index c0d39a1e08bffb33b3c01eb6330ca9b5bc6aecf3..c0c23427e035f56cfe0c37b99fb157c8e111fa25 100644 (file)
@@ -34,7 +34,7 @@
 # error This library requires C++
 #endif
 
-#include <string>
+const int OGC_VERSION = 4;
 
 class ogcFGData {
 
@@ -43,9 +43,9 @@ public:
     // defines msg types and contents. The msg_content is used as a 'pointer' to
     // a predefined set of msg strings
  
-    unsigned int       version_id;
-    unsigned int       msg_type;
-    unsigned int       msg_content;
+    int        version_id;
+    int        msg_type;
+    int        msg_content;
 
     // position
 
@@ -60,11 +60,11 @@ public:
     double     heading;
     double     altitude;
     double     altitude_agl;  // this can also be the radar altimeter
-    double     v_kcas;
+    double  v_kcas;
     double     groundspeed;
     double     vvi;
     double  mach;
-    double     v_tas;  // true airspeed in knots
+    double     v_keas;  // equivalent airspeed in knots
 
   // Data used by the FMC and autopilots
 
@@ -79,19 +79,23 @@ public:
 
   // Control surface positions
 
-    double     aileron;
+    double     left_aileron;
+    double  right_aileron;
     double     aileron_trim;
     double     elevator;
     double     elevator_trim;
     double     rudder;
     double     rudder_trim;
     double     flaps;
+    double  flaps_cmd;
 
-  // Gear positions 0 = UP and 1 = DOWN
+  // gear positions 0 = up and 1 = down  The 747 has 5 wheel bogey assemblies
 
     double     gear_nose;
     double     gear_left;
     double     gear_right;
+    double  gear_left_rear;
+    double  gear_right_rear;  
 
     // engine data
 
@@ -114,7 +118,10 @@ public:
     double     static_pressure;
     double     total_pressure;
     double     dynamic_pressure;
-       
+    
+    // more environmental data
+               double wind;
+               double wind_dir;
 };
 
 #endif // _OPENGC_HXX