X-Git-Url: https://git.mxchange.org/?a=blobdiff_plain;f=src%2FFDM%2FExternalPipe%2FExternalPipe.cxx;h=abe6569601a4a98b81d943647a23eeff558c398d;hb=2ea50c63bbb95e143662de2f136c79898236e38d;hp=8f33df584c36c0b719a94b7b8bd333aa9c519a00;hpb=8be4e97f54121260feb292e1fcbe3d072d28c941;p=flightgear.git

diff --git a/src/FDM/ExternalPipe/ExternalPipe.cxx b/src/FDM/ExternalPipe/ExternalPipe.cxx
index 8f33df584..abe656960 100644
--- a/src/FDM/ExternalPipe/ExternalPipe.cxx
+++ b/src/FDM/ExternalPipe/ExternalPipe.cxx
@@ -31,6 +31,7 @@
 #  include <unistd.h>           // unlink()
 #endif
 
+#include <cstring>
 #include <stdio.h>              // FILE*, fopen(), fread(), fwrite(), et. al.
 #include <iostream>             // for cout, endl
 
@@ -428,42 +429,48 @@ void FGExternalPipe::update_binary( double dt ) {
 
 
 // Process remote FDM "set" commands
-static void process_set_command( const string_list &tokens ) {
+
+void FGExternalPipe::process_set_command( const string_list &tokens ) {
     if ( tokens[1] == "geodetic_position" ) {
         double lat_rad = atof( tokens[2].c_str() );
         double lon_rad = atof( tokens[3].c_str() );
         double alt_m   = atof( tokens[4].c_str() );
-        cur_fdm_state->_updateGeodeticPosition( lat_rad, lon_rad,
+        _updateGeodeticPosition( lat_rad, lon_rad,
                                                 alt_m * SG_METER_TO_FEET );
 
-        double agl_m = alt_m - cur_fdm_state->get_Runway_altitude_m();
-        cur_fdm_state->_set_Altitude_AGL( agl_m * SG_METER_TO_FEET );
+        double agl_m = alt_m - get_Runway_altitude_m();
+        _set_Altitude_AGL( agl_m * SG_METER_TO_FEET );
     } else if ( tokens[1] == "euler_angles" ) {
         double phi_rad   = atof( tokens[2].c_str() );
         double theta_rad = atof( tokens[3].c_str() );
         double psi_rad   = atof( tokens[4].c_str() );
-        cur_fdm_state->_set_Euler_Angles( phi_rad, theta_rad, psi_rad );
+        _set_Euler_Angles( phi_rad, theta_rad, psi_rad );
     } else if ( tokens[1] == "euler_rates" ) {
         double phidot   = atof( tokens[2].c_str() );
         double thetadot = atof( tokens[3].c_str() );
         double psidot   = atof( tokens[4].c_str() );
-        cur_fdm_state->_set_Euler_Rates( phidot, thetadot, psidot );
+        _set_Euler_Rates( phidot, thetadot, psidot );
+    } else if ( tokens[1] == "ned" ) {
+	double north_fps = atof( tokens[2].c_str() );
+	double east_fps = atof( tokens[3].c_str() );
+	double down_fps = atof( tokens[4].c_str() );
+	_set_Velocities_Local( north_fps, east_fps, down_fps );
     } else if ( tokens[1] == "alpha" ) {
-        cur_fdm_state->_set_Alpha( atof(tokens[2].c_str()) );
+        _set_Alpha( atof(tokens[2].c_str()) );
     } else if ( tokens[1] == "beta" ) {
-        cur_fdm_state->_set_Beta( atof(tokens[2].c_str()) );
+        _set_Beta( atof(tokens[2].c_str()) );
 
 #if 0
-    cur_fdm_state->_set_V_calibrated_kts( net->vcas );
-    cur_fdm_state->_set_Climb_Rate( net->climb_rate );
-    cur_fdm_state->_set_Velocities_Local( net->v_north,
+    _set_V_calibrated_kts( net->vcas );
+    _set_Climb_Rate( net->climb_rate );
+    _set_Velocities_Local( net->v_north,
                                           net->v_east,
                                           net->v_down );
-    cur_fdm_state->_set_Velocities_Wind_Body( net->v_wind_body_north,
+    _set_Velocities_Wind_Body( net->v_wind_body_north,
                                               net->v_wind_body_east,
                                               net->v_wind_body_down );
 
-    cur_fdm_state->_set_Accels_Pilot_Body( net->A_X_pilot,
+    _set_Accels_Pilot_Body( net->A_X_pilot,
                                            net->A_Y_pilot,
                                            net->A_Z_pilot );
 #endif