Moved random ground cover object management code (userdata.[ch]xx) over

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

diff --git a/src/Network/net_fdm.hxx b/src/Network/net_fdm.hxx
index bb9728a3dab94b99fdd384ce9ccc576f8c6737c1..6cd71760099ada302df35bc82ec76a83a128fd84 100644 (file)
--- a/src/Network/net_fdm.hxx
+++ b/src/Network/net_fdm.hxx
@@ -32,7 +32,7 @@
 
 #include <time.h> // time_t
 
-const int FG_NET_FDM_VERSION = 8;
+const int FG_NET_FDM_VERSION = 11;
 
 
 // Define a structure containing the top level flight dynamics model
@@ -69,12 +69,26 @@ public:
     double psidot;             // yaw rate (radians/sec)
     double vcas;               // calibrated airspeed
     double climb_rate;         // feet per second
+    double v_north;             // north velocity in local/body frame, fps
+    double v_east;              // east velocity in local/body frame, fps
+    double v_down;              // down/vertical velocity in local/body frame, fps
+    double v_wind_body_north;   // north velocity in local/body frame
+                                // relative to local airmass, fps
+    double v_wind_body_east;    // east velocity in local/body frame
+                                // relative to local airmass, fps
+    double v_wind_body_down;    // down/vertical velocity in local/body
+                                // frame relative to local airmass, fps
+
+    // Stall
+    double stall_warning;        // 0.0 - 1.0 indicating the amount of stall
 
     // Accelerations
     double A_X_pilot;          // X accel in body frame ft/sec^2
     double A_Y_pilot;          // Y accel in body frame ft/sec^2
     double A_Z_pilot;          // Z accel in body frame ft/sec^2
 
+    // Pressure
+    
     // Engine status
     int num_engines;           // Number of valid engines
     int eng_state[FG_MAX_ENGINES]; // Engine state (off, cranking, running)