X-Git-Url: https://git.mxchange.org/?a=blobdiff_plain;f=src%2FInstrumentation%2Fattitude_indicator.cxx;h=a6cdfba2628a0e66192f4c1e90c9afefcc12455c;hb=863b0c943251fae620406ec8983e5f69e1424731;hp=02a249e4c3a6991fa8a3b4e06d032a6489653c6e;hpb=677c3e3e9ab9598c40a23cc89f99235d618b3a6f;p=flightgear.git diff --git a/src/Instrumentation/attitude_indicator.cxx b/src/Instrumentation/attitude_indicator.cxx index 02a249e4c..a6cdfba26 100644 --- a/src/Instrumentation/attitude_indicator.cxx +++ b/src/Instrumentation/attitude_indicator.cxx @@ -4,11 +4,13 @@ // This file is in the Public Domain and comes with no warranty. // TODO: -// - tumble // - better spin-up +#include // fabs() + #include "attitude_indicator.hxx" #include
+#include
AttitudeIndicator::AttitudeIndicator () @@ -27,6 +29,19 @@ AttitudeIndicator::init () _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); @@ -39,7 +54,7 @@ void AttitudeIndicator::bind () { fgTie("/instrumentation/attitude-indicator/serviceable", - &_gyro, &Gyro::is_serviceable); + &_gyro, &Gyro::is_serviceable, &Gyro::set_serviceable); fgTie("/instrumentation/attitude-indicator/spin", &_gyro, &Gyro::get_spin_norm, &Gyro::set_spin_norm); } @@ -54,21 +69,81 @@ AttitudeIndicator::unbind () 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(); - // Next, calculate the indicated roll - // and pitch, introducing errors. - double factor = 1.0 - ((1.0 - spin) * (1.0 - spin) * (1.0 - spin)); + // 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(); - roll = 35 + (factor * (roll - 35)); - pitch = 15 + (factor * (pitch - 15)); - _roll_out_node->setDoubleValue(roll); - _pitch_out_node->setDoubleValue(pitch); + // 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