#include "FGPosition.h"
#include "FGAuxiliary.h"
#include "FGOutput.h"
+#include "FGPropertyManager.h"
/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
DEFINITIONS
FGAircraft::FGAircraft(FGFDMExec* fdmex) : FGModel(fdmex)
{
Name = "FGAircraft";
- alphaclmin = alphaclmax = 0;
- HTailArea = VTailArea = HTailArm = VTailArm = 0.0;
- lbarh = lbarv = vbarh = vbarv = 0.0;
- WingIncidence=0;
- impending_stall = 0;
+ HTailArea = VTailArea = 0.0;
+ HTailArm = VTailArm = 0.0;
+ lbarh = lbarv = 0.0;
+ vbarh = vbarv = 0.0;
+
+ bind();
Debug(0);
}
FGAircraft::~FGAircraft()
{
+ unbind();
Debug(1);
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-bool FGAircraft::Load(FGConfigFile* AC_cfg)
-{
- string token;
-
- if (!ReadPrologue(AC_cfg)) return false;
-
- while ((AC_cfg->GetNextConfigLine() != string("EOF")) &&
- (token = AC_cfg->GetValue()) != string("/FDM_CONFIG")) {
- if (token == "METRICS") {
- if (debug_lvl > 0) cout << fgcyan << "\n Reading Metrics" << fgdef << endl;
- if (!ReadMetrics(AC_cfg)) return false;
- } else if (token == "AERODYNAMICS") {
- if (debug_lvl > 0) cout << fgcyan << "\n Reading Aerodynamics" << fgdef << endl;
- if (!ReadAerodynamics(AC_cfg)) return false;
- } else if (token == "UNDERCARRIAGE") {
- if (debug_lvl > 0) cout << fgcyan << "\n Reading Landing Gear" << fgdef << endl;
- if (!ReadUndercarriage(AC_cfg)) return false;
- } else if (token == "PROPULSION") {
- if (debug_lvl > 0) cout << fgcyan << "\n Reading Propulsion" << fgdef << endl;
- if (!ReadPropulsion(AC_cfg)) return false;
- } else if (token == "FLIGHT_CONTROL") {
- if (debug_lvl > 0) cout << fgcyan << "\n Reading Flight Control" << fgdef << endl;
- if (!ReadFlightControls(AC_cfg)) return false;
- } else if (token == "OUTPUT") {
- if (debug_lvl > 0) cout << fgcyan << "\n Reading Output directives" << fgdef << endl;
- if (!ReadOutput(AC_cfg)) return false;
- }
- }
-
- return true;
-}
-
-//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-
bool FGAircraft::Run(void)
{
if (!FGModel::Run()) { // if false then execute this Run()
vNwcg = State->GetTb2s() * vNcg;
vNwcg(3) = -1*vNwcg(3) + 1;
- if (alphaclmax != 0) {
- if (Translation->Getalpha() > 0.85*alphaclmax) {
- impending_stall = 10*(Translation->Getalpha()/alphaclmax - 0.85);
- } else {
- impending_stall = 0;
- }
- }
-
return false;
} else { // skip Run() execution this time
return true;
float FGAircraft::GetNlf(void)
{
- return vNwcg(3);
+ return -1*Aerodynamics->GetvFs(3)/MassBalance->GetWeight();
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-bool FGAircraft::ReadPrologue(FGConfigFile* AC_cfg)
-{
- string token = AC_cfg->GetValue();
- string scratch;
- AircraftName = AC_cfg->GetValue("NAME");
- if (debug_lvl > 0) cout << underon << "Reading Aircraft Configuration File"
- << underoff << ": " << highint << AircraftName << normint << endl;
- scratch = AC_cfg->GetValue("VERSION").c_str();
-
- CFGVersion = AC_cfg->GetValue("VERSION");
-
- if (debug_lvl > 0)
- cout << " Version: " << highint << CFGVersion
- << normint << endl;
- if (CFGVersion != needed_cfg_version) {
- cerr << endl << fgred << "YOU HAVE AN INCOMPATIBLE CFG FILE FOR THIS AIRCRAFT."
- " RESULTS WILL BE UNPREDICTABLE !!" << endl;
- cerr << "Current version needed is: " << needed_cfg_version << endl;
- cerr << " You have version: " << CFGVersion << endl << fgdef << endl;
- return false;
- }
- return true;
-}
-
-//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-
-bool FGAircraft::ReadMetrics(FGConfigFile* AC_cfg)
+bool FGAircraft::Load(FGConfigFile* AC_cfg)
{
string token = "";
string parameter;
} else if (parameter == "AC_AERORP") {
*AC_cfg >> vXYZrp(eX) >> vXYZrp(eY) >> vXYZrp(eZ);
if (debug_lvl > 0) cout << " Ref Pt (x, y, z): " << vXYZrp << endl;
- } else if (parameter == "AC_ALPHALIMITS") {
- *AC_cfg >> alphaclmin >> alphaclmax;
- if (debug_lvl > 0) cout << " Maximum Alpha: " << alphaclmax
- << " Minimum Alpha: " << alphaclmin
- << endl;
} else if (parameter == "AC_POINTMASS") {
*AC_cfg >> pmWt >> pmX >> pmY >> pmZ;
+ MassBalance->AddPointMass(pmWt, pmX, pmY, pmZ);
if (debug_lvl > 0) cout << " Point Mass Object: " << pmWt << " lbs. at "
<< "X, Y, Z (in.): " << pmX << " " << pmY << " " << pmZ
<< endl;
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-bool FGAircraft::ReadPropulsion(FGConfigFile* AC_cfg)
+void FGAircraft::bind(void)
{
- if (!Propulsion->Load(AC_cfg)) {
- cerr << " Propulsion not successfully loaded" << endl;
- return false;
- }
- return true;
+ typedef double (FGAircraft::*PMF)(int) const;
+ PropertyManager->Tie("metrics/Sw-sqft", this,
+ &FGAircraft::GetWingArea);
+ PropertyManager->Tie("metrics/bw-ft", this,
+ &FGAircraft::GetWingSpan);
+ PropertyManager->Tie("metrics/cbarw-ft", this,
+ &FGAircraft::Getcbar);
+ PropertyManager->Tie("metrics/iw-deg", this,
+ &FGAircraft::GetWingIncidence);
+ PropertyManager->Tie("metrics/Sh-sqft", this,
+ &FGAircraft::GetHTailArea);
+ PropertyManager->Tie("metrics/lh-ft", this,
+ &FGAircraft::GetHTailArm);
+ PropertyManager->Tie("metrics/Sv-sqft", this,
+ &FGAircraft::GetVTailArea);
+ PropertyManager->Tie("metrics/lv-ft", this,
+ &FGAircraft::GetVTailArm);
+ PropertyManager->Tie("metrics/lh-norm", this,
+ &FGAircraft::Getlbarh);
+ PropertyManager->Tie("metrics/lv-norm", this,
+ &FGAircraft::Getlbarv);
+ PropertyManager->Tie("metrics/vbarh-norm", this,
+ &FGAircraft::Getvbarh);
+ PropertyManager->Tie("metrics/vbarv-norm", this,
+ &FGAircraft::Getvbarv);
+ PropertyManager->Tie("moments/l-total-lbsft", this,1,
+ (PMF)&FGAircraft::GetMoments);
+ PropertyManager->Tie("moments/m-total-lbsft", this,2,
+ (PMF)&FGAircraft::GetMoments);
+ PropertyManager->Tie("moments/n-total-lbsft", this,3,
+ (PMF)&FGAircraft::GetMoments);
+ PropertyManager->Tie("forces/fbx-total-lbs", this,1,
+ (PMF)&FGAircraft::GetForces);
+ PropertyManager->Tie("forces/fby-total-lbs", this,2,
+ (PMF)&FGAircraft::GetForces);
+ PropertyManager->Tie("forces/fbz-total-lbs", this,3,
+ (PMF)&FGAircraft::GetForces);
+ PropertyManager->Tie("metrics/aero-rp-x-ft", this,1,
+ (PMF)&FGAircraft::GetXYZrp);
+ PropertyManager->Tie("metrics/aero-rp-y-ft", this,2,
+ (PMF)&FGAircraft::GetXYZrp);
+ PropertyManager->Tie("metrics/aero-rp-z-ft", this,3,
+ (PMF)&FGAircraft::GetXYZrp);
+ PropertyManager->Tie("metrics/eyepoint-x-ft", this,1,
+ (PMF)&FGAircraft::GetXYZep);
+ PropertyManager->Tie("metrics/eyepoint-y-ft", this,2,
+ (PMF)&FGAircraft::GetXYZep);
+ PropertyManager->Tie("metrics/eyepoint-z-ft", this,3,
+ (PMF)&FGAircraft::GetXYZep);
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-bool FGAircraft::ReadFlightControls(FGConfigFile* AC_cfg)
+void FGAircraft::unbind(void)
{
- if (!FCS->Load(AC_cfg)) {
- cerr << " Flight Controls not successfully loaded" << endl;
- return false;
- }
- return true;
-}
-
-//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-
-bool FGAircraft::ReadAerodynamics(FGConfigFile* AC_cfg)
-{
- if (!Aerodynamics->Load(AC_cfg)) {
- cerr << " Aerodynamics not successfully loaded" << endl;
- return false;
- }
- return true;
-}
-
-//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-
-bool FGAircraft::ReadUndercarriage(FGConfigFile* AC_cfg)
-{
- if (!GroundReactions->Load(AC_cfg)) {
- cerr << " Ground Reactions not successfully loaded" << endl;
- return false;
- }
- return true;
-}
-
-//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-
-bool FGAircraft::ReadOutput(FGConfigFile* AC_cfg)
-{
- if (!Output->Load(AC_cfg)) {
- cerr << " Output not successfully loaded" << endl;
- return false;
- }
- return true;
+ PropertyManager->Untie("metrics/Sw-sqft");
+ PropertyManager->Untie("metrics/bw-ft");
+ PropertyManager->Untie("metrics/cbarw-ft");
+ PropertyManager->Untie("metrics/iw-deg");
+ PropertyManager->Untie("metrics/Sh-sqft");
+ PropertyManager->Untie("metrics/lh-ft");
+ PropertyManager->Untie("metrics/Sv-sqft");
+ PropertyManager->Untie("metrics/lv-ft");
+ PropertyManager->Untie("metrics/lh-norm");
+ PropertyManager->Untie("metrics/lv-norm");
+ PropertyManager->Untie("metrics/vbarh-norm");
+ PropertyManager->Untie("metrics/vbarv-norm");
+ PropertyManager->Untie("moments/l-total-lbsft");
+ PropertyManager->Untie("moments/m-total-lbsft");
+ PropertyManager->Untie("moments/n-total-lbsft");
+ PropertyManager->Untie("forces/fbx-total-lbs");
+ PropertyManager->Untie("forces/fby-total-lbs");
+ PropertyManager->Untie("forces/fbz-total-lbs");
+ PropertyManager->Untie("metrics/aero-rp-x-ft");
+ PropertyManager->Untie("metrics/aero-rp-y-ft");
+ PropertyManager->Untie("metrics/aero-rp-z-ft");
+ PropertyManager->Untie("metrics/eyepoint-x-ft");
+ PropertyManager->Untie("metrics/eyepoint-y-ft");
+ PropertyManager->Untie("metrics/eyepoint-z-ft");
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
}
if (debug_lvl & 16) { // Sanity checking
}
- if (debug_lvl & 32) { // Turbulence
+ if (debug_lvl & 64) {
+ if (from == 0) { // Constructor
+ cout << IdSrc << endl;
+ cout << IdHdr << endl;
+ }
}
}
projects / flightgear.git / blobdiff