/******************************************************************************* Module: FGLGear.cpp Author: Jon S. Berndt Date started: 11/18/99 Purpose: Encapsulates the landing gear elements Called by: FGAircraft ------------- Copyright (C) 1999 Jon S. Berndt (jsb@hal-pc.org) ------------- This program is free software; you can redistribute it and/or modify it under the terms of the GNU General Public License as published by the Free Software 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 FOR A PARTICULAR PURPOSE. See the GNU General Public License for more details. You should have received a copy of the GNU General Public License along with this program; if not, write to the Free Software Foundation, Inc., 59 Temple Place - Suite 330, Boston, MA 02111-1307, USA. Further information about the GNU General Public License can also be found on the world wide web at http://www.gnu.org. FUNCTIONAL DESCRIPTION -------------------------------------------------------------------------------- HISTORY -------------------------------------------------------------------------------- 11/18/99 JSB Created ******************************************************************************** INCLUDES *******************************************************************************/ #include "FGLGear.h" #include /******************************************************************************* ************************************ CODE ************************************** *******************************************************************************/ FGLGear::FGLGear(FGConfigFile* AC_cfg, FGFDMExec* fdmex) : vXYZ(3), vMoment(3), Exec(fdmex) { string tmp; *AC_cfg >> tmp >> name >> vXYZ(1) >> vXYZ(2) >> vXYZ(3) >> kSpring >> bDamp >> statFCoeff >> brakeCoeff; State = Exec->GetState(); Aircraft = Exec->GetAircraft(); Position = Exec->GetPosition(); Rotation = Exec->GetRotation(); WOW = false; } /******************************************************************************/ FGLGear::~FGLGear(void) { } /******************************************************************************/ FGColumnVector FGLGear::Force(void) { static FGColumnVector vForce(3); static FGColumnVector vLocalForce(3); static FGColumnVector vLocalGear(3); static FGColumnVector vWhlBodyVec(3); static FGColumnVector vWhlVelVec(3); vWhlBodyVec = vXYZ - Aircraft->GetXYZcg(); vWhlBodyVec(eX) = -vWhlBodyVec(eX); vWhlBodyVec(eZ) = -vWhlBodyVec(eZ); vWhlBodyVec = vWhlBodyVec/12.0; vLocalGear = State->GetTb2l() * vWhlBodyVec; compressLength = vLocalGear(eZ) - Position->GetDistanceAGL(); if (compressLength > 0.00) { WOW = true; vWhlVelVec = State->GetTb2l() * (Rotation->GetPQR() * vWhlBodyVec); compressSpeed = vWhlVelVec(eZ) + Position->GetVd(); vLocalForce(eZ) = min(-compressLength * kSpring - compressSpeed * bDamp, (float)0.0); vForce = State->GetTl2b() * vLocalForce ; // currently only aircraft body axis Z-force modeled vMoment(eX) = vForce(eZ) * vWhlBodyVec(eY); vMoment(eY) = -vForce(eZ) * vWhlBodyVec(eX); vMoment(eZ) = 0.0; } else { WOW = false; vForce.InitMatrix(); vMoment.InitMatrix(); } return vForce; } /******************************************************************************/