X-Git-Url: https://git.mxchange.org/?a=blobdiff_plain;f=src%2FFDM%2FJSBSim%2FFGOutput.cpp;h=b3b3858088f2c6d0986a541acef77d82397ac8e3;hb=b5d116dad7816125dbaf94989aba774349f01017;hp=e7efe9cfbe95c0b36327459b92d67bb235d5a203;hpb=d2156b5649fdad7f825f9cbb8a789215d5c11c72;p=flightgear.git

diff --git a/src/FDM/JSBSim/FGOutput.cpp b/src/FDM/JSBSim/FGOutput.cpp
index e7efe9cfb..b3b385808 100644
--- a/src/FDM/JSBSim/FGOutput.cpp
+++ b/src/FDM/JSBSim/FGOutput.cpp
@@ -98,8 +98,9 @@ bool FGOutput::Run(void)
       } else {
         // Not a valid type of output
       }
-
+	  return false;
     } else {
+	  return true;
     }
   }
   return false;
@@ -117,7 +118,7 @@ void FGOutput::SetType(string type)
     Type = otSocket;
   } else if (type == "TERMINAL") {
     Type = otTerminal;
-  } else if (type != string("NONE")){
+  } else if (type != string("NONE")) {
     Type = otUnknown;
     cerr << "Unknown type of output specified in config file" << endl;
   }
@@ -172,7 +173,10 @@ void FGOutput::DelimitedOutput(string fname)
       outstream << ", ";
       outstream << "Drag, Side, Lift, ";
       outstream << "L/D, ";
-      outstream << "Xforce, Yforce, Zforce";
+      outstream << "Xforce, Yforce, Zforce, ";
+      outstream << "xGravity, yGravity, zGravity, ";
+      outstream << "xCoriolis, yCoriolis, zCoriolis, ";
+      outstream << "xCentrifugal, yCentrifugal, zCentrifugal";
     }
     if (SubSystems & ssMoments) {
       outstream << ", ";
@@ -207,6 +211,10 @@ void FGOutput::DelimitedOutput(string fname)
       outstream << ", ";
       outstream << Aerodynamics->GetCoefficientStrings();
     }
+    if (SubSystems & ssFCS) {
+      outstream << ", ";
+      outstream << FCS->GetComponentStrings();
+    }
     if (SubSystems & ssGroundReactions) {
       outstream << ", ";
       outstream << GroundReactions->GetGroundReactionStrings();
@@ -252,7 +260,10 @@ void FGOutput::DelimitedOutput(string fname)
     outstream << ", ";
     outstream << Aerodynamics->GetvFs() << ", ";
     outstream << Aerodynamics->GetLoD() << ", ";
-    outstream << Aircraft->GetForces();
+    outstream << Aircraft->GetForces() << ", ";
+    outstream << Inertial->GetGravity() << ", ";
+    outstream << Inertial->GetCoriolis() << ", ";
+    outstream << Inertial->GetCentrifugal();
   }
   if (SubSystems & ssMoments) {
     outstream << ", ";
@@ -287,6 +298,10 @@ void FGOutput::DelimitedOutput(string fname)
     outstream << ", ";
     outstream << Aerodynamics->GetCoefficientValues();
   }
+  if (SubSystems & ssFCS) {
+    outstream << ", ";
+    outstream << FCS->GetComponentValues();
+  }
   if (SubSystems & ssGroundReactions) {
     outstream << ", ";
     outstream << GroundReactions->GetGroundReactionValues();