2002-09-24 14:51:37 +00:00
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// attitude_indicator.cxx - a vacuum-powered attitude indicator.
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// Written by David Megginson, started 2002.
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//
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// This file is in the Public Domain and comes with no warranty.
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2002-09-27 18:27:58 +00:00
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// TODO:
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// - better spin-up
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2004-11-19 23:01:34 +00:00
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#include <simgear/compiler.h>
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2008-07-25 18:38:29 +00:00
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#include <iostream>
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#include <string>
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2004-11-19 23:01:34 +00:00
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#include <sstream>
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2003-04-05 13:05:24 +00:00
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#include <math.h> // fabs()
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2002-09-24 14:51:37 +00:00
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#include "attitude_indicator.hxx"
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#include <Main/fg_props.hxx>
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2003-04-04 03:25:02 +00:00
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#include <Main/util.hxx>
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2002-09-24 14:51:37 +00:00
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2004-10-16 12:37:39 +00:00
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AttitudeIndicator::AttitudeIndicator ( SGPropertyNode *node )
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:
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2006-12-06 22:11:43 +00:00
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_name(node->getStringValue("name", "attitude-indicator")),
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_num(node->getIntValue("number", 0)),
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_suction(node->getStringValue("suction", "/systems/vacuum/suction-inhg"))
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2002-09-24 14:51:37 +00:00
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{
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}
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AttitudeIndicator::~AttitudeIndicator ()
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{
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}
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void
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AttitudeIndicator::init ()
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{
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2004-10-16 12:37:39 +00:00
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string branch;
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2006-12-06 22:11:43 +00:00
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branch = "/instrumentation/" + _name;
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2004-10-16 12:37:39 +00:00
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2006-12-06 22:11:43 +00:00
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SGPropertyNode *node = fgGetNode(branch.c_str(), _num, true );
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2004-10-16 12:37:39 +00:00
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2002-09-24 14:51:37 +00:00
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_pitch_in_node = fgGetNode("/orientation/pitch-deg", true);
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_roll_in_node = fgGetNode("/orientation/roll-deg", true);
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2006-12-06 22:11:43 +00:00
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_suction_node = fgGetNode(_suction.c_str(), true);
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2004-10-16 12:37:39 +00:00
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SGPropertyNode *cnode = node->getChild("config", 0, true);
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_tumble_flag_node = cnode->getChild("tumble-flag", 0, true);
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_caged_node = node->getChild("caged-flag", 0, true);
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_tumble_node = node->getChild("tumble-norm", 0, true);
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_pitch_int_node = node->getChild("internal-pitch-deg", 0, true);
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_roll_int_node = node->getChild("internal-roll-deg", 0, true);
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_pitch_out_node = node->getChild("indicated-pitch-deg", 0, true);
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_roll_out_node = node->getChild("indicated-roll-deg", 0, true);
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2002-09-24 14:51:37 +00:00
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}
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void
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AttitudeIndicator::bind ()
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{
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2004-11-19 23:01:34 +00:00
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std::ostringstream temp;
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2004-10-16 12:37:39 +00:00
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string branch;
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2006-12-06 22:11:43 +00:00
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temp << _num;
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branch = "/instrumentation/" + _name + "[" + temp.str() + "]";
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2004-10-16 12:37:39 +00:00
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2004-11-19 23:01:34 +00:00
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fgTie((branch + "/serviceable").c_str(),
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2003-01-26 20:20:15 +00:00
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&_gyro, &Gyro::is_serviceable, &Gyro::set_serviceable);
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2004-11-19 23:01:34 +00:00
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fgTie((branch + "/spin").c_str(),
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2003-01-25 19:49:27 +00:00
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&_gyro, &Gyro::get_spin_norm, &Gyro::set_spin_norm);
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2002-09-24 14:51:37 +00:00
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}
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void
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AttitudeIndicator::unbind ()
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{
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2004-11-19 23:01:34 +00:00
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std::ostringstream temp;
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2004-10-16 12:37:39 +00:00
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string branch;
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2006-12-06 22:11:43 +00:00
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temp << _num;
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branch = "/instrumentation/" + _name + "[" + temp.str() + "]";
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2004-10-16 12:37:39 +00:00
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2004-11-19 23:01:34 +00:00
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fgUntie((branch + "/serviceable").c_str());
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fgUntie((branch + "/spin").c_str());
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2002-09-24 14:51:37 +00:00
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}
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void
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AttitudeIndicator::update (double dt)
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{
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2003-04-05 14:37:12 +00:00
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// If it's caged, it doesn't indicate
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if (_caged_node->getBoolValue()) {
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2003-04-25 02:22:06 +00:00
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_roll_int_node->setDoubleValue(0.0);
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_pitch_int_node->setDoubleValue(0.0);
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2003-04-05 14:37:12 +00:00
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return;
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}
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2003-01-25 19:49:27 +00:00
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// Get the spin from the gyro
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_gyro.set_power_norm(_suction_node->getDoubleValue()/5.0);
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_gyro.update(dt);
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double spin = _gyro.get_spin_norm();
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2002-09-24 14:51:37 +00:00
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2003-04-04 03:25:02 +00:00
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// Calculate the responsiveness
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double responsiveness = spin * spin * spin * spin * spin * spin;
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// Get the indicated roll and pitch
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2002-09-24 14:51:37 +00:00
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double roll = _roll_in_node->getDoubleValue();
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double pitch = _pitch_in_node->getDoubleValue();
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2002-09-24 16:37:28 +00:00
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2003-04-04 03:25:02 +00:00
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// Calculate the tumble for the
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// next pass.
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if (_tumble_flag_node->getBoolValue()) {
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2003-04-05 14:37:12 +00:00
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double tumble = _tumble_node->getDoubleValue();
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if (fabs(roll) > 45.0) {
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double target = (fabs(roll) - 45.0) / 45.0;
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target *= target; // exponential past +-45 degrees
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if (roll < 0)
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target = -target;
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if (fabs(target) > fabs(tumble))
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tumble = target;
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if (tumble > 1.0)
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tumble = 1.0;
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else if (tumble < -1.0)
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tumble = -1.0;
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2003-04-04 03:25:02 +00:00
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}
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2003-04-05 14:37:12 +00:00
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// Reerect in 5 minutes
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double step = dt/300.0;
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if (tumble < -step)
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tumble += step;
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else if (tumble > step)
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tumble -= step;
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roll += tumble * 45;
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_tumble_node->setDoubleValue(tumble);
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2003-04-04 03:25:02 +00:00
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}
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2003-04-25 02:22:06 +00:00
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roll = fgGetLowPass(_roll_int_node->getDoubleValue(), roll,
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2003-04-04 03:25:02 +00:00
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responsiveness);
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2003-04-25 02:22:06 +00:00
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pitch = fgGetLowPass(_pitch_int_node->getDoubleValue(), pitch,
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2003-04-04 03:25:02 +00:00
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responsiveness);
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// Assign the new values
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2003-04-25 02:22:06 +00:00
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_roll_int_node->setDoubleValue(roll);
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_pitch_int_node->setDoubleValue(pitch);
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// add in a gyro underspin "error" if gyro is spinning too slowly
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2003-05-27 19:13:51 +00:00
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const double spin_thresh = 0.8;
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2003-04-25 02:22:06 +00:00
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const double max_roll_error = 40.0;
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2003-04-25 03:36:51 +00:00
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const double max_pitch_error = 12.0;
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2003-04-25 02:22:06 +00:00
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double roll_error;
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double pitch_error;
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if ( spin <= spin_thresh ) {
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double roll_error_factor = (spin_thresh - spin) / spin_thresh;
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double pitch_error_factor = (spin_thresh - spin) / spin_thresh;
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roll_error = roll_error_factor * roll_error_factor * max_roll_error;
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pitch_error = pitch_error_factor * pitch_error_factor * max_pitch_error;
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} else {
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roll_error = 0.0;
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pitch_error = 0.0;
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}
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_roll_out_node->setDoubleValue(roll + roll_error);
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_pitch_out_node->setDoubleValue(pitch + pitch_error);
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2002-09-24 14:51:37 +00:00
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}
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// end of attitude_indicator.cxx
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