Fix for bug 1304 - crash loading XML route

[flightgear.git] / src / Network / net_fdm.hxx

diff --git a/src/Network/net_fdm.hxx b/src/Network/net_fdm.hxx
index 3ede199606110b3b56f761fa21c149caf5c13eb6..353a1812b1a883a9df41ca60e55b975b63440f80 100644 (file)
--- a/src/Network/net_fdm.hxx
+++ b/src/Network/net_fdm.hxx
@@ -22,7 +22,7 @@
 // I am not aware of any platforms that don't use 4 bytes for float
 // and 8 bytes for double.
 
-const uint32_t FG_NET_FDM_VERSION = 23;
+const uint32_t FG_NET_FDM_VERSION = 24;
 
 
 // Define a structure containing the top level flight dynamics model
@@ -61,13 +61,10 @@ public:
     float v_north;              // north velocity in local/body frame, fps
     float v_east;               // east velocity in local/body frame, fps
     float v_down;               // down/vertical velocity in local/body frame, fps
-    float v_wind_body_north;    // north velocity in local/body frame
-                                // relative to local airmass, fps
-    float v_wind_body_east;     // east velocity in local/body frame
-                                // relative to local airmass, fps
-    float v_wind_body_down;     // down/vertical velocity in local/body
-                                // frame relative to local airmass, fps
-
+    float v_body_u;    // ECEF velocity in body frame
+    float v_body_v;    // ECEF velocity in body frame 
+    float v_body_w;    // ECEF velocity in body frame
+    
     // Accelerations
     float A_X_pilot;           // X accel in body frame ft/sec^2
     float A_Y_pilot;           // Y accel in body frame ft/sec^2
@@ -84,6 +81,7 @@ public:
     uint32_t eng_state[FG_MAX_ENGINES];// Engine state (off, cranking, running)
     float rpm[FG_MAX_ENGINES];      // Engine RPM rev/min
     float fuel_flow[FG_MAX_ENGINES]; // Fuel flow gallons/hr
+    float fuel_px[FG_MAX_ENGINES];   // Fuel pressure psi
     float egt[FG_MAX_ENGINES];      // Exhuast gas temp deg F
     float cht[FG_MAX_ENGINES];      // Cylinder head temp deg F
     float mp_osi[FG_MAX_ENGINES];    // Manifold pressure