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flightgear/src/FDM/JSBSim/models/flight_control/FGAccelerometer.cpp
2010-07-16 11:05:59 +02:00

152 lines
5.1 KiB
C++
Executable file

/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
Module: FGAccelerometer.cpp
Author: Jon Berndt
Date started: 9 July 2005
------------- Copyright (C) 2005 -------------
This program is free software; you can redistribute it and/or modify it under
the terms of the GNU Lesser 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 Lesser General Public License for more
details.
You should have received a copy of the GNU Lesser 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 Lesser General Public License can also be found on
the world wide web at http://www.gnu.org.
FUNCTIONAL DESCRIPTION
--------------------------------------------------------------------------------
HISTORY
--------------------------------------------------------------------------------
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
COMMENTS, REFERENCES, and NOTES
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
INCLUDES
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
#include "FGAccelerometer.h"
#include <iostream>
#include <cstdlib>
using namespace std;
namespace JSBSim {
static const char *IdSrc = "$Id: FGAccelerometer.cpp,v 1.8 2009/10/24 22:59:30 jberndt Exp $";
static const char *IdHdr = ID_ACCELEROMETER;
/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
CLASS IMPLEMENTATION
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
FGAccelerometer::FGAccelerometer(FGFCS* fcs, Element* element)
: FGSensor(fcs, element),
FGSensorOrientation(element)
{
Propagate = fcs->GetExec()->GetPropagate();
MassBalance = fcs->GetExec()->GetMassBalance();
Inertial = fcs->GetExec()->GetInertial();
Element* location_element = element->FindElement("location");
if (location_element) vLocation = location_element->FindElementTripletConvertTo("IN");
else {cerr << "No location given for accelerometer. " << endl; exit(-1);}
vRadius = MassBalance->StructuralToBody(vLocation);
Debug(0);
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
FGAccelerometer::~FGAccelerometer()
{
Debug(1);
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
bool FGAccelerometer::Run(void )
{
// There is no input assumed. This is a dedicated acceleration sensor.
vRadius = MassBalance->StructuralToBody(vLocation);
//gravitational forces
vAccel = Propagate->GetTl2b() * FGColumnVector3(0, 0, Inertial->gravity());
//aircraft forces
vAccel += (Propagate->GetUVWdot()
+ Propagate->GetPQRdot() * vRadius
+ Propagate->GetPQR() * (Propagate->GetPQR() * vRadius));
// transform to the specified orientation
vAccel = mT * vAccel;
Input = vAccel(axis);
ProcessSensorSignal();
return true;
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
// 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 FGAccelerometer::Debug(int from)
{
string ax[4] = {"none", "X", "Y", "Z"};
if (debug_lvl <= 0) return;
if (debug_lvl & 1) { // Standard console startup message output
if (from == 0) { // Constructor
cout << " Axis: " << ax[axis] << endl;
}
}
if (debug_lvl & 2 ) { // Instantiation/Destruction notification
if (from == 0) cout << "Instantiated: FGAccelerometer" << endl;
if (from == 1) cout << "Destroyed: FGAccelerometer" << 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;
}
}
}
}