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flightgear/src/Instrumentation/attitude_indicator.cxx

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// attitude_indicator.cxx - a vacuum-powered attitude indicator.
// Written by David Megginson, started 2002.
//
// This file is in the Public Domain and comes with no warranty.
#include "attitude_indicator.hxx"
#include <Main/fg_props.hxx>
AttitudeIndicator::AttitudeIndicator ()
{
}
AttitudeIndicator::~AttitudeIndicator ()
{
}
void
AttitudeIndicator::init ()
{
// TODO: allow index of pump and AI
// to be configured.
_serviceable_node =
fgGetNode("/instrumentation/attitude-indicator/serviceable", true);
_pitch_in_node = fgGetNode("/orientation/pitch-deg", true);
_roll_in_node = fgGetNode("/orientation/roll-deg", true);
_suction_node = fgGetNode("/systems/vacuum[0]/suction-inhg", true);
_pitch_out_node =
fgGetNode("/instrumentation/attitude-indicator/indicated-pitch-deg",
true);
_roll_out_node =
fgGetNode("/instrumentation/attitude-indicator/indicated-roll-deg",
true);
}
void
AttitudeIndicator::bind ()
{
}
void
AttitudeIndicator::unbind ()
{
}
void
AttitudeIndicator::update (double dt)
{
// First, calculate the bogo-spin from 0 to 1.
// All numbers are made up.
_spin -= 0.01 * dt; // spin decays every 1% every second.
// spin increases up to 10% every second
// if suction is available and the gauge
// is serviceable.
if (_serviceable_node->getBoolValue()) {
double suction = _suction_node->getDoubleValue();
double step = 0.10 * (suction / 5.0) * dt;
if ((_spin + step) <= (suction / 5.0))
_spin += step;
}
// Next, calculate the indicated roll
// and pitch, introducing errors if
// the spin is less than 0.8 (80%).
double roll = _roll_in_node->getDoubleValue();
double pitch = _pitch_in_node->getDoubleValue();
if (_spin < 0.8) {
// TODO
}
_roll_out_node->setDoubleValue(roll);
_pitch_out_node->setDoubleValue(pitch);
}
// end of attitude_indicator.cxx