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flightgear/src/Instrumentation/attitude_indicator.cxx
curt d5d38ebe8c Make the attitude indicator gyro error kick in earlier in the gyro spin down
process.
Add the annunciator model to the list of managed instrumentation modules.
2003-05-27 19:13:51 +00:00

149 lines
4.8 KiB
C++

// 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.
// TODO:
// - better spin-up
#include <math.h> // fabs()
#include "attitude_indicator.hxx"
#include <Main/fg_props.hxx>
#include <Main/util.hxx>
AttitudeIndicator::AttitudeIndicator ()
{
}
AttitudeIndicator::~AttitudeIndicator ()
{
}
void
AttitudeIndicator::init ()
{
// TODO: allow index of pump and AI
// to be configured.
_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);
_tumble_flag_node =
fgGetNode("/instrumentation/attitude-indicator/config/tumble-flag",
true);
_caged_node =
fgGetNode("/instrumentation/attitude-indicator/caged-flag", true);
_tumble_node =
fgGetNode("/instrumentation/attitude-indicator/tumble-norm", true);
_pitch_int_node =
fgGetNode("/instrumentation/attitude-indicator/internal-pitch-deg",
true);
_roll_int_node =
fgGetNode("/instrumentation/attitude-indicator/internal-roll-deg",
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 ()
{
fgTie("/instrumentation/attitude-indicator/serviceable",
&_gyro, &Gyro::is_serviceable, &Gyro::set_serviceable);
fgTie("/instrumentation/attitude-indicator/spin",
&_gyro, &Gyro::get_spin_norm, &Gyro::set_spin_norm);
}
void
AttitudeIndicator::unbind ()
{
fgUntie("/instrumentation/attitude-indicator/serviceable");
fgUntie("/instrumentation/attitude-indicator/spin");
}
void
AttitudeIndicator::update (double dt)
{
// If it's caged, it doesn't indicate
if (_caged_node->getBoolValue()) {
_roll_int_node->setDoubleValue(0.0);
_pitch_int_node->setDoubleValue(0.0);
return;
}
// Get the spin from the gyro
_gyro.set_power_norm(_suction_node->getDoubleValue()/5.0);
_gyro.update(dt);
double spin = _gyro.get_spin_norm();
// Calculate the responsiveness
double responsiveness = spin * spin * spin * spin * spin * spin;
// Get the indicated roll and pitch
double roll = _roll_in_node->getDoubleValue();
double pitch = _pitch_in_node->getDoubleValue();
// Calculate the tumble for the
// next pass.
if (_tumble_flag_node->getBoolValue()) {
double tumble = _tumble_node->getDoubleValue();
if (fabs(roll) > 45.0) {
double target = (fabs(roll) - 45.0) / 45.0;
target *= target; // exponential past +-45 degrees
if (roll < 0)
target = -target;
if (fabs(target) > fabs(tumble))
tumble = target;
if (tumble > 1.0)
tumble = 1.0;
else if (tumble < -1.0)
tumble = -1.0;
}
// Reerect in 5 minutes
double step = dt/300.0;
if (tumble < -step)
tumble += step;
else if (tumble > step)
tumble -= step;
roll += tumble * 45;
_tumble_node->setDoubleValue(tumble);
}
roll = fgGetLowPass(_roll_int_node->getDoubleValue(), roll,
responsiveness);
pitch = fgGetLowPass(_pitch_int_node->getDoubleValue(), pitch,
responsiveness);
// Assign the new values
_roll_int_node->setDoubleValue(roll);
_pitch_int_node->setDoubleValue(pitch);
// add in a gyro underspin "error" if gyro is spinning too slowly
const double spin_thresh = 0.8;
const double max_roll_error = 40.0;
const double max_pitch_error = 12.0;
double roll_error;
double pitch_error;
if ( spin <= spin_thresh ) {
double roll_error_factor = (spin_thresh - spin) / spin_thresh;
double pitch_error_factor = (spin_thresh - spin) / spin_thresh;
roll_error = roll_error_factor * roll_error_factor * max_roll_error;
pitch_error = pitch_error_factor * pitch_error_factor * max_pitch_error;
} else {
roll_error = 0.0;
pitch_error = 0.0;
}
_roll_out_node->setDoubleValue(roll + roll_error);
_pitch_out_node->setDoubleValue(pitch + pitch_error);
}
// end of attitude_indicator.cxx