1
0
Fork 0
flightgear/src/Instrumentation/attitude_indicator.cxx

162 lines
5 KiB
C++
Raw Normal View History

// 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 <simgear/compiler.h>
#include <iostream>
#include <string>
#include <sstream>
2003-04-05 13:05:24 +00:00
#include <math.h> // fabs()
#include "attitude_indicator.hxx"
#include <Main/fg_props.hxx>
#include <Main/util.hxx>
AttitudeIndicator::AttitudeIndicator ( SGPropertyNode *node )
:
_name(node->getStringValue("name", "attitude-indicator")),
_num(node->getIntValue("number", 0)),
_suction(node->getStringValue("suction", "/systems/vacuum/suction-inhg"))
{
}
AttitudeIndicator::~AttitudeIndicator ()
{
}
void
AttitudeIndicator::init ()
{
string branch;
branch = "/instrumentation/" + _name;
SGPropertyNode *node = fgGetNode(branch.c_str(), _num, true );
_pitch_in_node = fgGetNode("/orientation/pitch-deg", true);
_roll_in_node = fgGetNode("/orientation/roll-deg", true);
_suction_node = fgGetNode(_suction.c_str(), true);
SGPropertyNode *cnode = node->getChild("config", 0, true);
_tumble_flag_node = cnode->getChild("tumble-flag", 0, true);
_caged_node = node->getChild("caged-flag", 0, true);
_tumble_node = node->getChild("tumble-norm", 0, true);
_pitch_int_node = node->getChild("internal-pitch-deg", 0, true);
_roll_int_node = node->getChild("internal-roll-deg", 0, true);
_pitch_out_node = node->getChild("indicated-pitch-deg", 0, true);
_roll_out_node = node->getChild("indicated-roll-deg", 0, true);
}
void
AttitudeIndicator::bind ()
{
std::ostringstream temp;
string branch;
temp << _num;
branch = "/instrumentation/" + _name + "[" + temp.str() + "]";
fgTie((branch + "/serviceable").c_str(),
2003-01-26 20:20:15 +00:00
&_gyro, &Gyro::is_serviceable, &Gyro::set_serviceable);
fgTie((branch + "/spin").c_str(),
&_gyro, &Gyro::get_spin_norm, &Gyro::set_spin_norm);
}
void
AttitudeIndicator::unbind ()
{
std::ostringstream temp;
string branch;
temp << _num;
branch = "/instrumentation/" + _name + "[" + temp.str() + "]";
fgUntie((branch + "/serviceable").c_str());
fgUntie((branch + "/spin").c_str());
}
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;
2003-04-25 03:36:51 +00:00
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