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flightgear/src/Instrumentation/altimeter.cxx
Tim Moore 738e06e845 _kollsman member not initialized
From Csaba Helasz
2009-01-26 09:37:46 +01:00

83 lines
2.8 KiB
C++

// altimeter.cxx - an altimeter tied to the static port.
// Written by David Megginson, started 2002.
// Modified by John Denker in 2007 to use a two layer atmosphere
// model in src/Environment/atmosphere.?xx
//
// This file is in the Public Domain and comes with no warranty.
// Example invocation, in the instrumentation.xml file:
// <altimeter>
// <name>encoder</name>
// <number>0</number>
// <static-pressure>/systems/static/pressure-inhg</static-pressure>
// <quantum>10</quantum>
// <tau>0</tau>
// </altimeter>
// Note non-default name, quantum, and tau values.
#ifdef HAVE_CONFIG_H
# include <config.h>
#endif
#include <simgear/math/interpolater.hxx>
#include <simgear/math/SGMath.hxx>
#include <Main/fg_props.hxx>
#include <Main/util.hxx>
#include <Environment/atmosphere.hxx>
#include "altimeter.hxx"
Altimeter::Altimeter ( SGPropertyNode *node, double quantum )
: _name(node->getStringValue("name", "altimeter")),
_num(node->getIntValue("number", 0)),
_static_pressure(node->getStringValue("static-pressure", "/systems/static/pressure-inhg")),
_tau(node->getDoubleValue("tau", 0.1)),
_quantum(node->getDoubleValue("quantum", quantum))
{}
Altimeter::~Altimeter ()
{}
void
Altimeter::init ()
{
string branch;
branch = "/instrumentation/" + _name;
SGPropertyNode *node = fgGetNode(branch.c_str(), _num, true );
raw_PA = 0.0;
_kollsman = 0.0;
_pressure_node = fgGetNode(_static_pressure.c_str(), true);
_serviceable_node = node->getChild("serviceable", 0, true);
_setting_node = node->getChild("setting-inhg", 0, true);
_press_alt_node = node->getChild("pressure-alt-ft", 0, true);
_mode_c_node = node->getChild("mode-c-alt-ft", 0, true);
_altitude_node = node->getChild("indicated-altitude-ft", 0, true);
if (_setting_node->getDoubleValue() == 0)
_setting_node->setDoubleValue(29.921260);
}
void
Altimeter::update (double dt)
{
if (_serviceable_node->getBoolValue()) {
double trat = _tau > 0 ? dt/_tau : 100;
double pressure = _pressure_node->getDoubleValue();
double setting = _setting_node->getDoubleValue();
double press_alt = _press_alt_node->getDoubleValue();
// The mechanism settles slowly toward new pressure altitude:
raw_PA = fgGetLowPass(raw_PA, _altimeter.press_alt_ft(pressure), trat);
_mode_c_node->setDoubleValue(100 * SGMiscd::round(raw_PA/100));
_kollsman = fgGetLowPass(_kollsman, _altimeter.kollsman_ft(setting), trat);
if (_quantum)
press_alt = _quantum * SGMiscd::round(raw_PA/_quantum);
else
press_alt = raw_PA;
_press_alt_node->setDoubleValue(press_alt);
_altitude_node->setDoubleValue(press_alt - _kollsman);
}
}
// end of altimeter.cxx