📄 fin.cpp
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/* -*- indent-tabs-mode:T; c-basic-offset:8; tab-width:8; -*- vi: set ts=8: * $Id: Fin.cpp,v 2.0 2002/09/22 02:07:31 tramm Exp $ * * (c) Aaron Kahn * (c) Trammell Hudson * * Aerodynamic fin simulation * ************* * * This file is part of the autopilot simulation package. * * For more details: * * http://autopilot.sourceforge.net/ * * Autopilot 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. * * Autopilot 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 Autopilot; if not, write to the Free Software * Foundation, Inc., 59 Temple Place, Suite 330, Boston, MA 02111-1307 USA * */#include "Fin.h"#include <mat/Frames.h>#include <cmath>namespace sim {using namespace libmat;/* * Computes the rotor downwash and other forces on the aerodynamic * bodies related to the aircraft. */voidFin::step( Forces * cg, double downwash){ double rho2 = cg->rho() / 2.0; const Force<Frame::Body> F( rho2 * this->xuu * cg->uvw[0] * fabs(cg->uvw[0]), rho2 * this->yvv * cg->uvw[1] * fabs(cg->uvw[1]), rho2 * this->zww * cg->uvw[2] * fabs(cg->uvw[2]) - rho2 * this->zww * downwash ); const Moment<Frame::Body> M( F[1]*this->h, F[2]*this->d - F[0]*this->h, -F[1]*this->d ); // Sum Up Total Forces and Moments At CG cg->F += F; cg->M += M;}}
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