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flightgear/src/FDM/JSBSim/models/FGLGear.cpp

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/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
Module: FGLGear.cpp
Author: Jon S. Berndt
Norman H. Princen
Bertrand Coconnier
2006-01-12 15:04:22 +00:00
Date started: 11/18/99
Purpose: Encapsulates the landing gear elements
Called by: FGAircraft
2009-08-30 08:22:03 +00:00
------------- Copyright (C) 1999 Jon S. Berndt (jon@jsbsim.org) -------------
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This program is free software; you can redistribute it and/or modify it under
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the terms of the GNU Lesser General Public License as published by the Free Software
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Foundation; either version 2 of the License, or (at your option) any later
version.
This program is distributed in the hope that it will be useful, but WITHOUT
ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or FITNESS
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FOR A PARTICULAR PURPOSE. See the GNU Lesser General Public License for more
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details.
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You should have received a copy of the GNU Lesser General Public License along with
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this program; if not, write to the Free Software Foundation, Inc., 59 Temple
Place - Suite 330, Boston, MA 02111-1307, USA.
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Further information about the GNU Lesser General Public License can also be found on
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the world wide web at http://www.gnu.org.
FUNCTIONAL DESCRIPTION
--------------------------------------------------------------------------------
HISTORY
--------------------------------------------------------------------------------
11/18/99 JSB Created
01/30/01 NHP Extended gear model to properly simulate steering and braking
07/08/09 BC Modified gear model to support large angles between aircraft and ground
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/%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
INCLUDES
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
#include "FGLGear.h"
namespace JSBSim {
/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
DEFINITIONS
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
GLOBAL DATA
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
static const char *IdSrc = "$Id$";
static const char *IdHdr = ID_LGEAR;
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// Body To Structural (body frame is rotated 180 deg about Y and lengths are given in
// ft instead of inches)
const FGMatrix33 FGLGear::Tb2s(-1./inchtoft, 0., 0., 0., 1./inchtoft, 0., 0., 0., -1./inchtoft);
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/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
CLASS IMPLEMENTATION
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
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FGLGear::FGLGear(Element* el, FGFDMExec* fdmex, int number) :
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FGForce(fdmex),
GearNumber(number)
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{
Element *force_table=0;
Element *dampCoeff=0;
Element *dampCoeffRebound=0;
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string force_type="";
kSpring = bDamp = bDampRebound = dynamicFCoeff = staticFCoeff = rollingFCoeff = maxSteerAngle = 0;
sSteerType = sBrakeGroup = sSteerType = "";
isRetractable = 0;
eDampType = dtLinear;
eDampTypeRebound = dtLinear;
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name = el->GetAttributeValue("name");
sContactType = el->GetAttributeValue("type");
if (sContactType == "BOGEY") {
eContactType = ctBOGEY;
} else if (sContactType == "STRUCTURE") {
eContactType = ctSTRUCTURE;
} else {
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// Unknown contact point types will be treated as STRUCTURE.
eContactType = ctSTRUCTURE;
}
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if (el->FindElement("spring_coeff"))
kSpring = el->FindElementValueAsNumberConvertTo("spring_coeff", "LBS/FT");
if (el->FindElement("damping_coeff")) {
dampCoeff = el->FindElement("damping_coeff");
if (dampCoeff->GetAttributeValue("type") == "SQUARE") {
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eDampType = dtSquare;
bDamp = el->FindElementValueAsNumberConvertTo("damping_coeff", "LBS/FT2/SEC2");
} else {
bDamp = el->FindElementValueAsNumberConvertTo("damping_coeff", "LBS/FT/SEC");
}
}
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if (el->FindElement("damping_coeff_rebound")) {
dampCoeffRebound = el->FindElement("damping_coeff_rebound");
if (dampCoeffRebound->GetAttributeValue("type") == "SQUARE") {
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eDampTypeRebound = dtSquare;
bDampRebound = el->FindElementValueAsNumberConvertTo("damping_coeff_rebound", "LBS/FT2/SEC2");
} else {
bDampRebound = el->FindElementValueAsNumberConvertTo("damping_coeff_rebound", "LBS/FT/SEC");
}
} else {
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bDampRebound = bDamp;
eDampTypeRebound = eDampType;
}
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if (el->FindElement("dynamic_friction"))
dynamicFCoeff = el->FindElementValueAsNumber("dynamic_friction");
if (el->FindElement("static_friction"))
staticFCoeff = el->FindElementValueAsNumber("static_friction");
if (el->FindElement("rolling_friction"))
rollingFCoeff = el->FindElementValueAsNumber("rolling_friction");
if (el->FindElement("max_steer"))
maxSteerAngle = el->FindElementValueAsNumberConvertTo("max_steer", "DEG");
if (el->FindElement("retractable"))
isRetractable = ((unsigned int)el->FindElementValueAsNumber("retractable"))>0.0?true:false;
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ForceY_Table = 0;
force_table = el->FindElement("table");
while (force_table) {
force_type = force_table->GetAttributeValue("type");
if (force_type == "CORNERING_COEFF") {
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ForceY_Table = new FGTable(fdmex->GetPropertyManager(), force_table);
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} else {
cerr << "Undefined force table for " << name << " contact point" << endl;
}
force_table = el->FindNextElement("table");
}
sBrakeGroup = el->FindElementValue("brake_group");
if (maxSteerAngle == 360) sSteerType = "CASTERED";
else if (maxSteerAngle == 0.0) sSteerType = "FIXED";
else sSteerType = "STEERABLE";
Element* element = el->FindElement("location");
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if (element) vXYZn = element->FindElementTripletConvertTo("IN");
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else {cerr << "No location given for contact " << name << endl; exit(-1);}
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SetTransformType(FGForce::tCustom);
element = el->FindElement("orientation");
if (element && (eContactType == ctBOGEY)) {
vGearOrient = element->FindElementTripletConvertTo("RAD");
double cp,sp,cr,sr,cy,sy;
cp=cos(vGearOrient(ePitch)); sp=sin(vGearOrient(ePitch));
cr=cos(vGearOrient(eRoll)); sr=sin(vGearOrient(eRoll));
cy=cos(vGearOrient(eYaw)); sy=sin(vGearOrient(eYaw));
mTGear(1,1) = cp*cy;
mTGear(2,1) = cp*sy;
mTGear(3,1) = -sp;
mTGear(1,2) = sr*sp*cy - cr*sy;
mTGear(2,2) = sr*sp*sy + cr*cy;
mTGear(3,2) = sr*cp;
mTGear(1,3) = cr*sp*cy + sr*sy;
mTGear(2,3) = cr*sp*sy - sr*cy;
mTGear(3,3) = cr*cp;
}
else {
mTGear(1,1) = 1.;
mTGear(2,2) = 1.;
mTGear(3,3) = 1.;
}
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if (sBrakeGroup == "LEFT" ) eBrakeGrp = bgLeft;
else if (sBrakeGroup == "RIGHT" ) eBrakeGrp = bgRight;
else if (sBrakeGroup == "CENTER") eBrakeGrp = bgCenter;
else if (sBrakeGroup == "NOSE" ) eBrakeGrp = bgNose;
else if (sBrakeGroup == "TAIL" ) eBrakeGrp = bgTail;
else if (sBrakeGroup == "NONE" ) eBrakeGrp = bgNone;
else if (sBrakeGroup.empty() ) {eBrakeGrp = bgNone;
sBrakeGroup = "NONE (defaulted)";}
else {
cerr << "Improper braking group specification in config file: "
<< sBrakeGroup << " is undefined." << endl;
}
if (sSteerType == "STEERABLE") eSteerType = stSteer;
else if (sSteerType == "FIXED" ) eSteerType = stFixed;
else if (sSteerType == "CASTERED" ) eSteerType = stCaster;
else if (sSteerType.empty() ) {eSteerType = stFixed;
sSteerType = "FIXED (defaulted)";}
else {
cerr << "Improper steering type specification in config file: "
<< sSteerType << " is undefined." << endl;
}
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RFRV = 0.7; // Rolling force relaxation velocity, default value
SFRV = 0.7; // Side force relaxation velocity, default value
Element* relax_vel = el->FindElement("relaxation_velocity");
if (relax_vel) {
if (relax_vel->FindElement("rolling")) {
RFRV = relax_vel->FindElementValueAsNumberConvertTo("rolling", "FT/SEC");
}
if (relax_vel->FindElement("side")) {
SFRV = relax_vel->FindElementValueAsNumberConvertTo("side", "FT/SEC");
}
}
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State = fdmex->GetState();
Aircraft = fdmex->GetAircraft();
Propagate = fdmex->GetPropagate();
Auxiliary = fdmex->GetAuxiliary();
FCS = fdmex->GetFCS();
MassBalance = fdmex->GetMassBalance();
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LongForceLagFilterCoeff = 1/State->Getdt(); // default longitudinal force filter coefficient
LatForceLagFilterCoeff = 1/State->Getdt(); // default lateral force filter coefficient
Element* force_lag_filter_elem = el->FindElement("force_lag_filter");
if (force_lag_filter_elem) {
if (force_lag_filter_elem->FindElement("rolling")) {
LongForceLagFilterCoeff = force_lag_filter_elem->FindElementValueAsNumber("rolling");
}
if (force_lag_filter_elem->FindElement("side")) {
LatForceLagFilterCoeff = force_lag_filter_elem->FindElementValueAsNumber("side");
}
}
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LongForceFilter = Filter(LongForceLagFilterCoeff, State->Getdt());
LatForceFilter = Filter(LatForceLagFilterCoeff, State->Getdt());
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WheelSlipLagFilterCoeff = 1/State->Getdt();
Element *wheel_slip_angle_lag_elem = el->FindElement("wheel_slip_filter");
if (wheel_slip_angle_lag_elem) {
WheelSlipLagFilterCoeff = wheel_slip_angle_lag_elem->GetDataAsNumber();
}
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WheelSlipFilter = Filter(WheelSlipLagFilterCoeff, State->Getdt());
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GearUp = false;
GearDown = true;
GearPos = 1.0;
useFCSGearPos = false;
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Servicable = true;
// Add some AI here to determine if gear is located properly according to its
// brake group type ??
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WOW = lastWOW = false;
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ReportEnable = true;
FirstContact = false;
StartedGroundRun = false;
TakeoffReported = LandingReported = false;
LandingDistanceTraveled = TakeoffDistanceTraveled = TakeoffDistanceTraveled50ft = 0.0;
MaximumStrutForce = MaximumStrutTravel = 0.0;
SinkRate = GroundSpeed = 0.0;
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vWhlBodyVec = MassBalance->StructuralToBody(vXYZn);
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vLocalGear = Propagate->GetTb2l() * vWhlBodyVec;
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vWhlVelVec.InitMatrix();
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compressLength = 0.0;
compressSpeed = 0.0;
brakePct = 0.0;
maxCompLen = 0.0;
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WheelSlip = 0.0;
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TirePressureNorm = 1.0;
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// Set Pacejka terms
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Stiffness = 0.06;
Shape = 2.8;
Peak = staticFCoeff;
Curvature = 1.03;
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Debug(0);
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}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
FGLGear::~FGLGear()
{
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delete ForceY_Table;
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Debug(1);
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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FGColumnVector3& FGLGear::GetBodyForces(void)
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{
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double t = fdmex->GetState()->Getsim_time();
dT = State->Getdt()*fdmex->GetGroundReactions()->GetRate();
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vFn.InitMatrix();
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if (isRetractable) ComputeRetractionState();
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if (GearDown) {
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double verticalZProj = 0.;
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vWhlBodyVec = MassBalance->StructuralToBody(vXYZn); // Get wheel in body frame
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vLocalGear = Propagate->GetTb2l() * vWhlBodyVec; // Get local frame wheel location
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gearLoc = Propagate->GetLocation().LocalToLocation(vLocalGear);
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// Compute the height of the theoretical location of the wheel (if strut is not compressed) with
// respect to the ground level
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double height = fdmex->GetGroundCallback()->GetAGLevel(t, gearLoc, contact, normal, cvel);
vGroundNormal = -1. * Propagate->GetTec2b() * normal;
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// The height returned above is the AGL and is expressed in the Z direction of the local
// coordinate frame. We now need to transform this height in actual compression of the strut (BOGEY)
// of in the normal direction to the ground (STRUCTURE)
switch (eContactType) {
case ctBOGEY:
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verticalZProj = (Propagate->GetTb2l()*mTGear*FGColumnVector3(0.,0.,1.))(eZ);
compressLength = verticalZProj > 0.0 ? -height / verticalZProj : 0.0;
break;
case ctSTRUCTURE:
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verticalZProj = (Propagate->GetTec2l()*normal)(eZ);
compressLength = fabs(verticalZProj) > 0.0 ? -height / verticalZProj : 0.0;
break;
}
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if (compressLength > 0.00) {
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WOW = true;
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// [The next equation should really use the vector to the contact patch of
// the tire including the strut compression and not the original vWhlBodyVec.]
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FGColumnVector3 vWhlDisplVec = mTGear * FGColumnVector3(0., 0., compressLength);
FGColumnVector3 vWhlContactVec = vWhlBodyVec - vWhlDisplVec;
vActingXYZn = vXYZn - Tb2s * vWhlDisplVec;
FGColumnVector3 vBodyWhlVel = Propagate->GetPQR() * vWhlContactVec;
vBodyWhlVel += Propagate->GetUVW() - Propagate->GetTec2b() * cvel;
vWhlVelVec = mTGear.Transposed() * vBodyWhlVel;
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InitializeReporting();
ComputeSteeringAngle();
ComputeGroundCoordSys();
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vLocalWhlVel = Transform().Transposed() * vBodyWhlVel;
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switch (eContactType) {
case ctBOGEY:
// Compression speed along the strut
compressSpeed = -vWhlVelVec(eZ);
case ctSTRUCTURE:
// Compression speed along the ground normal
compressSpeed = -vLocalWhlVel(eX);
}
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ComputeVerticalStrutForce();
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// Compute the forces in the wheel ground plane.
if (eContactType == ctBOGEY) {
ComputeSlipAngle();
ComputeBrakeForceCoefficient();
ComputeSideForceCoefficient();
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double sign = vLocalWhlVel(eY)>0?1.0:(vLocalWhlVel(eY)<0?-1.0:0.0);
vFn(eY) = - ((1.0 - TirePressureNorm) * 30 + vFn(eX) * BrakeFCoeff) * sign;
vFn(eZ) = vFn(eX) * FCoeff;
}
else if (eContactType == ctSTRUCTURE) {
FGColumnVector3 vSlipVec = vLocalWhlVel;
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vSlipVec(eX) = 0.;
vSlipVec.Normalize();
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vFn -= staticFCoeff * vFn(eX) * vSlipVec;
}
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// Lag and attenuate the XY-plane forces dependent on velocity. This code
// uses a lag filter, C/(s + C) where "C" is the filter coefficient. When
// "C" is chosen at the frame rate (in Hz), the jittering is significantly
// reduced. This is because the jitter is present *at* the execution rate.
// If a coefficient is set to something equal to or less than zero, the
// filter is bypassed.
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if (LongForceLagFilterCoeff > 0) vFn(eY) = LongForceFilter.execute(vFn(eY));
if (LatForceLagFilterCoeff > 0) vFn(eZ) = LatForceFilter.execute(vFn(eZ));
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if ((fabs(vLocalWhlVel(eY)) <= RFRV) && RFRV > 0) vFn(eY) *= fabs(vLocalWhlVel(eY))/RFRV;
if ((fabs(vLocalWhlVel(eZ)) <= SFRV) && SFRV > 0) vFn(eZ) *= fabs(vLocalWhlVel(eZ))/SFRV;
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// End section for attenuating gear jitter
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} else { // Gear is NOT compressed
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WOW = false;
compressLength = 0.0;
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compressSpeed = 0.0;
// Let wheel spin down slowly
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vWhlVelVec(eX) -= 13.0*dT;
if (vWhlVelVec(eX) < 0.0) vWhlVelVec(eX) = 0.0;
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// Return to neutral position between 1.0 and 0.8 gear pos.
SteerAngle *= max(GetGearUnitPos()-0.8, 0.0)/0.2;
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ResetReporting();
}
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}
ReportTakeoffOrLanding();
// Require both WOW and LastWOW to be true before checking crash conditions
// to allow the WOW flag to be used in terminating a scripted run.
if (WOW && lastWOW) CrashDetect();
lastWOW = WOW;
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return FGForce::GetBodyForces();
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}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
// Build a local "ground" coordinate system defined by
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// eX : normal to the ground
// eY : projection of the rolling direction on the ground
// eZ : projection of the sliping direction on the ground
void FGLGear::ComputeGroundCoordSys(void)
{
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// Euler angles are built up to create a local frame to describe the forces
// applied to the gear by the ground. Here pitch, yaw and roll do not have
// any physical meaning. It is just a convenient notation.
// First, "pitch" and "yaw" are determined in order to align eX with the
// ground normal.
if (vGroundNormal(eZ) < -1.0)
vOrient(ePitch) = 0.5*M_PI;
else if (1.0 < vGroundNormal(eZ))
vOrient(ePitch) = -0.5*M_PI;
else
vOrient(ePitch) = asin(-vGroundNormal(eZ));
if (fabs(vOrient(ePitch)) == 0.5*M_PI)
vOrient(eYaw) = 0.;
else
vOrient(eYaw) = atan2(vGroundNormal(eY), vGroundNormal(eX));
vOrient(eRoll) = 0.;
UpdateCustomTransformMatrix();
if (eContactType == ctBOGEY) {
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// In the case of a bogey, the third angle "roll" is used to align the axis eY and eZ
// to the rolling and sliping direction respectively.
FGColumnVector3 updatedRollingAxis = Transform().Transposed() * mTGear
* FGColumnVector3(-sin(SteerAngle), cos(SteerAngle), 0.);
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vOrient(eRoll) = atan2(updatedRollingAxis(eY), -updatedRollingAxis(eZ));
UpdateCustomTransformMatrix();
}
}
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//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
void FGLGear::ComputeRetractionState(void)
{
double gearPos = GetGearUnitPos();
if (gearPos < 0.01) {
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GearUp = true;
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WOW = false;
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GearDown = false;
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vWhlVelVec.InitMatrix();
} else if (gearPos > 0.99) {
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GearDown = true;
GearUp = false;
} else {
GearUp = false;
GearDown = false;
}
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
void FGLGear::ComputeSlipAngle(void)
{
// Calculate tire slip angle.
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WheelSlip = -atan2(vLocalWhlVel(eZ), fabs(vLocalWhlVel(eY)))*radtodeg;
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// Filter the wheel slip angle
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if (WheelSlipLagFilterCoeff > 0) WheelSlip = WheelSlipFilter.execute(WheelSlip);
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}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
// Compute the steering angle in any case.
// This will also make sure that animations will look right.
void FGLGear::ComputeSteeringAngle(void)
{
switch (eSteerType) {
case stSteer:
SteerAngle = degtorad * FCS->GetSteerPosDeg(GearNumber);
break;
case stFixed:
SteerAngle = 0.0;
break;
case stCaster:
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SteerAngle = atan2(vWhlVelVec(eY), fabs(vWhlVelVec(eX)));
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break;
default:
cerr << "Improper steering type membership detected for this gear." << endl;
break;
}
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
// Reset reporting functionality after takeoff
void FGLGear::ResetReporting(void)
{
if (Propagate->GetDistanceAGL() > 200.0) {
FirstContact = false;
StartedGroundRun = false;
LandingReported = false;
TakeoffReported = true;
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LandingDistanceTraveled = 0.0;
MaximumStrutForce = MaximumStrutTravel = 0.0;
}
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
void FGLGear::InitializeReporting(void)
{
// If this is the first time the wheel has made contact, remember some values
// for later printout.
if (!FirstContact) {
FirstContact = true;
SinkRate = compressSpeed;
GroundSpeed = Propagate->GetVel().Magnitude();
TakeoffReported = false;
}
// If the takeoff run is starting, initialize.
if ((Propagate->GetVel().Magnitude() > 0.1) &&
(FCS->GetBrake(bgLeft) == 0) &&
(FCS->GetBrake(bgRight) == 0) &&
(FCS->GetThrottlePos(0) > 0.90) && !StartedGroundRun)
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{
TakeoffDistanceTraveled = 0;
TakeoffDistanceTraveled50ft = 0;
StartedGroundRun = true;
}
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
// Takeoff and landing reporting functionality
void FGLGear::ReportTakeoffOrLanding(void)
{
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double deltaT = State->Getdt()*fdmex->GetGroundReactions()->GetRate();
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if (FirstContact)
LandingDistanceTraveled += Auxiliary->GetVground()*deltaT;
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if (StartedGroundRun) {
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TakeoffDistanceTraveled50ft += Auxiliary->GetVground()*deltaT;
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if (WOW) TakeoffDistanceTraveled += Auxiliary->GetVground()*deltaT;
}
if ( ReportEnable
&& Auxiliary->GetVground() <= 0.05
&& !LandingReported
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&& fdmex->GetGroundReactions()->GetWOW())
{
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if (debug_lvl > 0) Report(erLand);
}
if ( ReportEnable
&& !TakeoffReported
&& (Propagate->GetDistanceAGL() - vLocalGear(eZ)) > 50.0
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&& !fdmex->GetGroundReactions()->GetWOW())
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{
if (debug_lvl > 0) Report(erTakeoff);
}
if (lastWOW != WOW) PutMessage("GEAR_CONTACT: " + name, WOW);
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
// Crash detection logic (really out-of-bounds detection)
void FGLGear::CrashDetect(void)
{
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if ( (compressLength > 500.0 ||
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vFn.Magnitude() > 100000000.0 ||
GetMoments().Magnitude() > 5000000000.0 ||
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SinkRate > 1.4666*30 ) && !State->IntegrationSuspended())
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{
PutMessage("Crash Detected: Simulation FREEZE.");
State->SuspendIntegration();
}
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
// The following needs work regarding friction coefficients and braking and
// steering The BrakeFCoeff formula assumes that an anti-skid system is used.
// It also assumes that we won't be turning and braking at the same time.
// Will fix this later.
// [JSB] The braking force coefficients include normal rolling coefficient +
// a percentage of the static friction coefficient based on braking applied.
void FGLGear::ComputeBrakeForceCoefficient(void)
{
switch (eBrakeGrp) {
case bgLeft:
BrakeFCoeff = ( rollingFCoeff*(1.0 - FCS->GetBrake(bgLeft)) +
staticFCoeff*FCS->GetBrake(bgLeft) );
break;
case bgRight:
BrakeFCoeff = ( rollingFCoeff*(1.0 - FCS->GetBrake(bgRight)) +
staticFCoeff*FCS->GetBrake(bgRight) );
break;
case bgCenter:
BrakeFCoeff = ( rollingFCoeff*(1.0 - FCS->GetBrake(bgCenter)) +
staticFCoeff*FCS->GetBrake(bgCenter) );
break;
case bgNose:
BrakeFCoeff = ( rollingFCoeff*(1.0 - FCS->GetBrake(bgCenter)) +
staticFCoeff*FCS->GetBrake(bgCenter) );
break;
case bgTail:
BrakeFCoeff = ( rollingFCoeff*(1.0 - FCS->GetBrake(bgCenter)) +
staticFCoeff*FCS->GetBrake(bgCenter) );
break;
case bgNone:
BrakeFCoeff = rollingFCoeff;
break;
default:
cerr << "Improper brake group membership detected for this gear." << endl;
break;
}
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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// Compute the sideforce coefficients using Pacejka's Magic Formula.
//
// y(x) = D sin {C arctan [Bx - E(Bx - arctan Bx)]}
//
// Where: B = Stiffness Factor (0.06, here)
// C = Shape Factor (2.8, here)
// D = Peak Factor (0.8, here)
// E = Curvature Factor (1.03, here)
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void FGLGear::ComputeSideForceCoefficient(void)
{
if (ForceY_Table) {
FCoeff = ForceY_Table->GetValue(WheelSlip);
} else {
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double StiffSlip = Stiffness*WheelSlip;
FCoeff = Peak * sin(Shape*atan(StiffSlip - Curvature*(StiffSlip - atan(StiffSlip))));
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}
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
// Compute the vertical force on the wheel using square-law damping (per comment
// in paper AIAA-2000-4303 - see header prologue comments). We might consider
// allowing for both square and linear damping force calculation. Also need to
// possibly give a "rebound damping factor" that differs from the compression
// case.
void FGLGear::ComputeVerticalStrutForce(void)
{
double springForce = 0;
double dampForce = 0;
springForce = -compressLength * kSpring;
if (compressSpeed >= 0.0) {
if (eDampType == dtLinear) dampForce = -compressSpeed * bDamp;
else dampForce = -compressSpeed * compressSpeed * bDamp;
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} else {
if (eDampTypeRebound == dtLinear)
dampForce = -compressSpeed * bDampRebound;
else
dampForce = compressSpeed * compressSpeed * bDampRebound;
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}
StrutForce = min(springForce + dampForce, (double)0.0);
// The reaction force of the wheel is always normal to the ground
switch (eContactType) {
case ctBOGEY:
// Project back the strut force in the local coordinate frame of the ground
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vFn(eX) = StrutForce / (mTGear.Transposed()*vGroundNormal)(eZ);
break;
case ctSTRUCTURE:
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vFn(eX) = -StrutForce;
break;
}
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// Remember these values for reporting
MaximumStrutForce = max(MaximumStrutForce, fabs(StrutForce));
MaximumStrutTravel = max(MaximumStrutTravel, fabs(compressLength));
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}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
double FGLGear::GetGearUnitPos(void)
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{
// hack to provide backward compatibility to gear/gear-pos-norm property
if( useFCSGearPos || FCS->GetGearPos() != 1.0 ) {
useFCSGearPos = true;
return FCS->GetGearPos();
}
return GearPos;
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}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
void FGLGear::bind(void)
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{
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string property_name;
string base_property_name;
base_property_name = CreateIndexedPropertyName("gear/unit", GearNumber);
if (eContactType == ctBOGEY) {
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property_name = base_property_name + "/slip-angle-deg";
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fdmex->GetPropertyManager()->Tie( property_name.c_str(), &WheelSlip );
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property_name = base_property_name + "/WOW";
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fdmex->GetPropertyManager()->Tie( property_name.c_str(), &WOW );
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property_name = base_property_name + "/wheel-speed-fps";
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fdmex->GetPropertyManager()->Tie( property_name.c_str(), (FGLGear*)this,
&FGLGear::GetWheelRollVel);
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property_name = base_property_name + "/z-position";
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fdmex->GetPropertyManager()->Tie( property_name.c_str(), (FGForce*)this,
&FGForce::GetLocationZ, &FGForce::SetLocationZ);
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property_name = base_property_name + "/compression-ft";
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fdmex->GetPropertyManager()->Tie( property_name.c_str(), &compressLength );
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property_name = base_property_name + "/side_friction_coeff";
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fdmex->GetPropertyManager()->Tie( property_name.c_str(), &FCoeff );
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property_name = base_property_name + "/static_friction_coeff";
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fdmex->GetPropertyManager()->Tie( property_name.c_str(), &staticFCoeff );
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if (eSteerType == stCaster) {
property_name = base_property_name + "/steering-angle-rad";
fdmex->GetPropertyManager()->Tie( property_name.c_str(), &SteerAngle );
}
}
if( isRetractable ) {
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property_name = base_property_name + "/pos-norm";
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fdmex->GetPropertyManager()->Tie( property_name.c_str(), &GearPos );
}
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}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
void FGLGear::Report(ReportType repType)
{
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if (fabs(TakeoffDistanceTraveled) < 0.001) return; // Don't print superfluous reports
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switch(repType) {
case erLand:
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cout << endl << "Touchdown report for " << name << " (WOW at time: "
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<< fdmex->GetState()->Getsim_time() << " seconds)" << endl;
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cout << " Sink rate at contact: " << SinkRate << " fps, "
<< SinkRate*0.3048 << " mps" << endl;
cout << " Contact ground speed: " << GroundSpeed*.5925 << " knots, "
<< GroundSpeed*0.3048 << " mps" << endl;
cout << " Maximum contact force: " << MaximumStrutForce << " lbs, "
<< MaximumStrutForce*4.448 << " Newtons" << endl;
cout << " Maximum strut travel: " << MaximumStrutTravel*12.0 << " inches, "
<< MaximumStrutTravel*30.48 << " cm" << endl;
cout << " Distance traveled: " << LandingDistanceTraveled << " ft, "
<< LandingDistanceTraveled*0.3048 << " meters" << endl;
LandingReported = true;
break;
case erTakeoff:
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cout << endl << "Takeoff report for " << name << " (Liftoff at time: "
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<< fdmex->GetState()->Getsim_time() << " seconds)" << endl;
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cout << " Distance traveled: " << TakeoffDistanceTraveled
<< " ft, " << TakeoffDistanceTraveled*0.3048 << " meters" << endl;
cout << " Distance traveled (over 50'): " << TakeoffDistanceTraveled50ft
<< " ft, " << TakeoffDistanceTraveled50ft*0.3048 << " meters" << endl;
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cout << " [Altitude (ASL): " << fdmex->GetPropagate()->GetAltitudeASL() << " ft. / "
<< fdmex->GetPropagate()->GetAltitudeASLmeters() << " m | Temperature: "
<< fdmex->GetAtmosphere()->GetTemperature() - 459.67 << " F / "
<< RankineToCelsius(fdmex->GetAtmosphere()->GetTemperature()) << " C]" << endl;
cout << " [Velocity (KCAS): " << fdmex->GetAuxiliary()->GetVcalibratedKTS() << "]" << endl;
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TakeoffReported = true;
break;
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case erNone:
break;
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}
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
// 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 FGLGear::Debug(int from)
{
if (debug_lvl <= 0) return;
if (debug_lvl & 1) { // Standard console startup message output
if (from == 0) { // Constructor - loading and initialization
cout << " " << sContactType << " " << name << endl;
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cout << " Location: " << vXYZn << endl;
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cout << " Spring Constant: " << kSpring << endl;
if (eDampType == dtLinear)
cout << " Damping Constant: " << bDamp << " (linear)" << endl;
else
cout << " Damping Constant: " << bDamp << " (square law)" << endl;
if (eDampTypeRebound == dtLinear)
cout << " Rebound Damping Constant: " << bDampRebound << " (linear)" << endl;
else
cout << " Rebound Damping Constant: " << bDampRebound << " (square law)" << endl;
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cout << " Dynamic Friction: " << dynamicFCoeff << endl;
cout << " Static Friction: " << staticFCoeff << endl;
if (eContactType == ctBOGEY) {
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cout << " Rolling Friction: " << rollingFCoeff << endl;
cout << " Steering Type: " << sSteerType << endl;
cout << " Grouping: " << sBrakeGroup << endl;
cout << " Max Steer Angle: " << maxSteerAngle << endl;
cout << " Retractable: " << isRetractable << endl;
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cout << " Relaxation Velocities:" << endl;
cout << " Rolling: " << RFRV << endl;
cout << " Side: " << SFRV << endl;
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}
}
}
if (debug_lvl & 2 ) { // Instantiation/Destruction notification
if (from == 0) cout << "Instantiated: FGLGear" << endl;
if (from == 1) cout << "Destroyed: FGLGear" << 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;
}
}
}
} // namespace JSBSim