]> git.mxchange.org Git - flightgear.git/blobdiff - src/FDM/JSBSim/FGPosition.cpp
Latest JSBSim changes, including some gear tweaking from Jon and some
[flightgear.git] / src / FDM / JSBSim / FGPosition.cpp
index bc73e33f55d27230f09d285ed6cbb4f421872f5c..a5a278af0e6059e16f7b6c8fe62094ff185ebd71 100644 (file)
@@ -1,4 +1,4 @@
-/*******************************************************************************
+/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
  
  Module:       FGPosition.cpp
  Author:       Jon S. Berndt
@@ -29,14 +29,14 @@ FUNCTIONAL DESCRIPTION
 --------------------------------------------------------------------------------
 This class encapsulates the integration of rates and accelerations to get the
 current position of the aircraft.
+
 HISTORY
 --------------------------------------------------------------------------------
 01/05/99   JSB   Created
-********************************************************************************
+
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 COMMENTS, REFERENCES,  and NOTES
-********************************************************************************
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 [1] Cooke, Zyda, Pratt, and McGhee, "NPSNET: Flight Simulation Dynamic Modeling
     Using Quaternions", Presence, Vol. 1, No. 4, pp. 404-420  Naval Postgraduate
     School, January 1994
@@ -48,14 +48,14 @@ COMMENTS, REFERENCES,  and NOTES
     Wiley & Sons, 1979 ISBN 0-471-03032-5
 [5] Bernard Etkin, "Dynamics of Flight, Stability and Control", Wiley & Sons,
     1982 ISBN 0-471-08936-2
-********************************************************************************
+
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 INCLUDES
-*******************************************************************************/
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
 
 #ifdef FGFS
 #  include <simgear/compiler.h>
-#  ifdef FG_HAVE_STD_INCLUDES
+#  ifdef SG_HAVE_STD_INCLUDES
 #    include <cmath>
 #    include <iomanip>
 #  else
@@ -63,8 +63,13 @@ INCLUDES
 #    include <iomanip.h>
 #  endif
 #else
-#  include <cmath>
-#  include <iomanip>
+#  if defined(sgi) && !defined(__GNUC__)
+#    include <math.h>
+#    include <iomanip.h>
+#  else
+#    include <cmath>
+#    include <iomanip>
+#  endif
 #endif
 
 #include "FGPosition.h"
@@ -73,65 +78,87 @@ INCLUDES
 #include "FGFDMExec.h"
 #include "FGFCS.h"
 #include "FGAircraft.h"
+#include "FGMassBalance.h"
 #include "FGTranslation.h"
 #include "FGRotation.h"
 #include "FGAuxiliary.h"
 #include "FGOutput.h"
 
-/*******************************************************************************
-************************************ CODE **************************************
-*******************************************************************************/
+static const char *IdSrc = "$Id$";
+static const char *IdHdr = ID_POSITION;
+
+/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+CLASS IMPLEMENTATION
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
 
-extern float globalTriNormal[3];
+extern double globalTriNormal[3];
 extern double globalSceneryAltitude;
 extern double globalSeaLevelRadius;
 
-FGPosition::FGPosition(FGFDMExec* fdmex) : FGModel(fdmex),
-    vUVW(3),
-    vVel(3),
-    vVelDot(3)
+FGPosition::FGPosition(FGFDMExec* fdmex) : FGModel(fdmex)
 {
   Name = "FGPosition";
   LongitudeDot = LatitudeDot = RadiusDot = 0.0;
   lastLongitudeDot = lastLatitudeDot = lastRadiusDot = 0.0;
   Longitude = Latitude = 0.0;
   gamma = Vt = Vground = 0.0;
+  hoverbmac = hoverbcg = 0.0;
+  psigt = 0.0;
+
+  Debug(0);
+}
+
+//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+
+FGPosition::~FGPosition(void)
+{
+  Debug(1);
+}
+
+//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+
+bool FGPosition::InitModel(void)
+{
+  FGModel::InitModel();
+
   h = 3.0;                                 // Est. height of aircraft cg off runway
-  SeaLevelRadius = EARTHRAD;               // For initialization ONLY
+  SeaLevelRadius = Inertial->RefRadius();  // For initialization ONLY
   Radius         = SeaLevelRadius + h;
   RunwayRadius   = SeaLevelRadius;
   DistanceAGL    = Radius - RunwayRadius;  // Geocentric
+  vRunwayNormal(3) = -1.0;                 // Initialized for standalone mode
+  b = 1;
+  return true;
 }
 
-/******************************************************************************/
-
-FGPosition::~FGPosition(void) {}
-
-/*************************************************************************** Run
+//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+/*
 Purpose: Called on a schedule to perform Positioning algorithms
 Notes:   [TP] Make sure that -Vt <= hdot <= Vt, which, of course, should always
          be the case
-         [JB] Run in standalone mode, SeaLevelRadius will be EARTHRAD. In FGFS,
-         SeaLevelRadius is stuffed from FGJSBSim in JSBSim.cxx each pass.
+         [JB] Run in standalone mode, SeaLevelRadius will be reference radius.
+              In FGFS, SeaLevelRadius is stuffed from FGJSBSim in JSBSim.cxx each pass.
 */
 
-bool FGPosition:: Run(void) {
+bool FGPosition::Run(void) {
   double cosLat;
   double hdot_Vt;
+  FGColumnVector3 vMac;
 
   if (!FGModel::Run()) {
     GetState();
 
     Vground = sqrt( vVel(eNorth)*vVel(eNorth) + vVel(eEast)*vVel(eEast) );
-    
-    invMass   = 1.0 / Aircraft->GetMass();
+    psigt =  atan2(vVel(eEast), vVel(eNorth));
+    if (psigt < 0.0)
+      psigt += 2*M_PI;
+
     Radius    = h + SeaLevelRadius;
-    invRadius = 1.0 / Radius;
 
     cosLat = cos(Latitude);
     if (cosLat != 0) LongitudeDot = vVel(eEast) / (Radius * cosLat);
 
-    LatitudeDot = vVel(eNorth) * invRadius;
+    LatitudeDot = vVel(eNorth) Radius;
     RadiusDot   = -vVel(eDown);
 
     Longitude += 0.5*dt*rate*(LongitudeDot + lastLongitudeDot);
@@ -141,8 +168,14 @@ bool FGPosition:: Run(void) {
     h = Radius - SeaLevelRadius;           // Geocentric
 
     DistanceAGL = Radius - RunwayRadius;   // Geocentric
-
-    hoverb = DistanceAGL/b;
+    
+    
+    hoverbcg = DistanceAGL/b;
+    
+    vMac=State->GetTb2l()*Aircraft->GetXYZrp();
+    
+    vMac *= inchtoft;
+    hoverbmac = (DistanceAGL + vMac(3))/b;
 
     if (Vt > 0) {
       hdot_Vt = RadiusDot/Vt;
@@ -162,28 +195,79 @@ bool FGPosition:: Run(void) {
   }
 }
 
-/******************************************************************************/
+//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 void FGPosition::GetState(void) {
   dt = State->Getdt();
 
-  vUVW      = Translation->GetUVW();
   Vt        = Translation->GetVt();
-  vVel      = State->GetTb2l()*vUVW;
+  vVel      = State->GetTb2l() * Translation->GetUVW();
   vVelDot   = State->GetTb2l() * Translation->GetUVWdot();
-
-  b = Aircraft->GetWingSpan();
   
+  b = Aircraft->GetWingSpan();
 }
 
-void FGPosition::Seth(double tt) { 
- h=tt;
+//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+
+void FGPosition::Seth(double tt) {
+ h = tt;
  Radius    = h + SeaLevelRadius;
- DistanceAGL = Radius - RunwayRadius;   // Geocentric 
-}  
+ DistanceAGL = Radius - RunwayRadius;   // Geocentric
+ hoverbcg = DistanceAGL/b;
+}
+
+//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 void FGPosition::SetDistanceAGL(double tt) {
   DistanceAGL=tt;
   Radius = RunwayRadius + DistanceAGL;
   h = Radius - SeaLevelRadius;
-}  
+  hoverbcg = DistanceAGL/b;
+}
+
+//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+//    The bitmasked value choices are as follows:
+//    unset: In this case (the default) JSBSim would only print
+//       out the normally expected messages, essentially echoing
+//       the config files as they are read. If the environment
+//       variable is not set, debug_lvl is set to 1 internally
+//    0: This requests JSBSim not to output any messages
+//       whatsoever.
+//    1: This value explicity requests the normal JSBSim
+//       startup messages
+//    2: This value asks for a message to be printed out when
+//       a class is instantiated
+//    4: When this value is set, a message is displayed when a
+//       FGModel object executes its Run() method
+//    8: When this value is set, various runtime state variables
+//       are printed out periodically
+//    16: When set various parameters are sanity checked and
+//       a message is printed out when they go out of bounds
+
+void FGPosition::Debug(int from)
+{
+  if (debug_lvl <= 0) return;
+
+  if (debug_lvl & 1) { // Standard console startup message output
+    if (from == 0) { // Constructor
+
+    }
+  }
+  if (debug_lvl & 2 ) { // Instantiation/Destruction notification
+    if (from == 0) cout << "Instantiated: FGPosition" << endl;
+    if (from == 1) cout << "Destroyed:    FGPosition" << endl;
+  }
+  if (debug_lvl & 4 ) { // Run() method entry print for FGModel-derived objects
+  }
+  if (debug_lvl & 8 ) { // Runtime state variables
+  }
+  if (debug_lvl & 16) { // Sanity checking
+  }
+  if (debug_lvl & 64) {
+    if (from == 0) { // Constructor
+      cout << IdSrc << endl;
+      cout << IdHdr << endl;
+    }
+  }
+}
+