/**************************************************************************** * * Copyright (c) 2013 Estimation and Control Library (ECL). All rights reserved. * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions * are met: * * 1. Redistributions of source code must retain the above copyright * notice, this list of conditions and the following disclaimer. * 2. Redistributions in binary form must reproduce the above copyright * notice, this list of conditions and the following disclaimer in * the documentation and/or other materials provided with the * distribution. * 3. Neither the name ECL nor the names of its contributors may be * used to endorse or promote products derived from this software * without specific prior written permission. * * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE * POSSIBILITY OF SUCH DAMAGE. * ****************************************************************************/ /** * @file estimator_base.cpp * Definition of base class for attitude estimators * * @author Roman Bast * */ #include #include "estimator_base.h" #include EstimatorBase::EstimatorBase() { } EstimatorBase::~EstimatorBase() { } // Accumulate imu data and store to buffer at desired rate void EstimatorBase::setIMUData(uint64_t time_usec, uint64_t delta_ang_dt, uint64_t delta_vel_dt, float *delta_ang, float *delta_vel) { if (!_initialised) { initialiseVariables(time_usec); _initialised = true; _start_predict_enabled = true; } float dt = (float)(time_usec - _time_last_imu) / 1000 / 1000; dt = math::max(dt, 1.0e-4f); dt = math::min(dt, 0.02f); _time_last_imu = time_usec; if (_imu_time_last > 0) { _dt_imu_avg = 0.8f * _dt_imu_avg + 0.2f * dt; } // copy data imuSample imu_sample_new = {}; memcpy(&imu_sample_new.delta_ang._data[0], delta_ang, sizeof(imu_sample_new.delta_ang._data)); memcpy(&imu_sample_new.delta_vel._data[0], delta_vel, sizeof(imu_sample_new.delta_vel._data)); imu_sample_new.delta_ang_dt = delta_ang_dt / 1e6f; imu_sample_new.delta_vel_dt = delta_vel_dt / 1e6f; imu_sample_new.time_us = time_usec; imu_sample_new.delta_ang(0) = imu_sample_new.delta_ang(0) * _state.gyro_scale(0); imu_sample_new.delta_ang(1) = imu_sample_new.delta_ang(1) * _state.gyro_scale(1); imu_sample_new.delta_ang(2) = imu_sample_new.delta_ang(2) * _state.gyro_scale(2); imu_sample_new.delta_ang -= _state.gyro_bias; imu_sample_new.delta_vel(2) -= _state.accel_z_bias; _imu_down_sampled.delta_ang_dt += imu_sample_new.delta_ang_dt; _imu_down_sampled.delta_vel_dt += imu_sample_new.delta_vel_dt; Quaternion delta_q; delta_q.rotate(imu_sample_new.delta_ang); _q_down_sampled = _q_down_sampled * delta_q; _q_down_sampled.normalize(); matrix::Dcm delta_R(delta_q.inversed()); _imu_down_sampled.delta_vel = delta_R * _imu_down_sampled.delta_vel; _imu_down_sampled.delta_vel += imu_sample_new.delta_vel; _imu_ticks++; if ((_dt_imu_avg * _imu_ticks >= (float)(FILTER_UPDATE_PERRIOD_MS) / 1000 && _start_predict_enabled) || (_dt_imu_avg * _imu_ticks >= 0.02f)) { _imu_down_sampled.delta_ang = _q_down_sampled.to_axis_angle(); _imu_down_sampled.time_us = time_usec; _imu_buffer.push(_imu_down_sampled); _imu_down_sampled.delta_ang.setZero(); _imu_down_sampled.delta_vel.setZero(); _imu_down_sampled.delta_ang_dt = 0.0f; _imu_down_sampled.delta_vel_dt = 0.0f; _q_down_sampled(0) = 1.0f; _q_down_sampled(1) = _q_down_sampled(2) = _q_down_sampled(3) = 0.0f; _imu_ticks = 0; _imu_updated = true; } else { _imu_updated = false; } _imu_sample_delayed = _imu_buffer.get_oldest(); } void EstimatorBase::setMagData(uint64_t time_usec, float *data) { if (time_usec - _time_last_mag > 70000) { magSample mag_sample_new = {}; mag_sample_new.time_us = time_usec - _params.mag_delay_ms * 1000; mag_sample_new.time_us -= FILTER_UPDATE_PERRIOD_MS * 1000 / 2; _time_last_mag = mag_sample_new.time_us; memcpy(&mag_sample_new.mag._data[0], data, sizeof(mag_sample_new.mag._data)); _mag_buffer.push(mag_sample_new); } } void EstimatorBase::setGpsData(uint64_t time_usec, struct gps_message *gps) { if (!_gps_initialised) { initialiseGPS(gps); return; } if (time_usec - _time_last_gps > 70000 && gps_is_good(gps)) { gpsSample gps_sample_new = {}; gps_sample_new.time_us = gps->time_usec - _params.gps_delay_ms * 1000; gps_sample_new.time_us -= FILTER_UPDATE_PERRIOD_MS * 1000 / 2; _time_last_gps = gps_sample_new.time_us; gps_sample_new.time_us = math::max(gps_sample_new.time_us, _imu_sample_delayed.time_us); memcpy(gps_sample_new.vel._data[0], gps->vel_ned, sizeof(gps_sample_new.vel._data)); _gps_speed_valid = gps->vel_ned_valid; float lpos_x = 0.0f; float lpos_y = 0.0f; map_projection_project(&_posRef, (gps->lat / 1.0e7), (gps->lon / 1.0e7), &lpos_x, &lpos_y); gps_sample_new.pos(0) = lpos_x; gps_sample_new.pos(1) = lpos_y; gps_sample_new.hgt = gps->alt / 1e3f; _gps_buffer.push(gps_sample_new); } } void EstimatorBase::setBaroData(uint64_t time_usec, float *data) { if (time_usec - _time_last_baro > 70000) { baroSample baro_sample_new; baro_sample_new.hgt = *data; baro_sample_new.time_us = time_usec - _params.baro_delay_ms * 1000; baro_sample_new.time_us -= FILTER_UPDATE_PERRIOD_MS * 1000 / 2; _time_last_baro = baro_sample_new.time_us; baro_sample_new.time_us = math::max(baro_sample_new.time_us, _imu_sample_delayed.time_us); _baro_buffer.push(baro_sample_new); } } void EstimatorBase::setAirspeedData(uint64_t time_usec, float *data) { if (time_usec > _time_last_airspeed) { airspeedSample airspeed_sample_new; airspeed_sample_new.airspeed = *data; airspeed_sample_new.time_us -= _params.airspeed_delay_ms * 1000; airspeed_sample_new.time_us = time_usec -= FILTER_UPDATE_PERRIOD_MS * 1000 / 2; _time_last_airspeed = airspeed_sample_new.time_us; _airspeed_buffer.push(airspeed_sample_new); } } // set range data void EstimatorBase::setRangeData(uint64_t time_usec, float *data) { } // set optical flow data void EstimatorBase::setOpticalFlowData(uint64_t time_usec, float *data) { } void EstimatorBase::initialiseVariables(uint64_t time_usec) { _imu_buffer.allocate(IMU_BUFFER_LENGTH); _gps_buffer.allocate(OBS_BUFFER_LENGTH); _mag_buffer.allocate(OBS_BUFFER_LENGTH); _baro_buffer.allocate(OBS_BUFFER_LENGTH); _range_buffer.allocate(OBS_BUFFER_LENGTH); _airspeed_buffer.allocate(OBS_BUFFER_LENGTH); _flow_buffer.allocate(OBS_BUFFER_LENGTH); _output_buffer.allocate(IMU_BUFFER_LENGTH); _state.ang_error.setZero(); _state.vel.setZero(); _state.pos.setZero(); _state.gyro_bias.setZero(); _state.gyro_scale(0) = 1.0f; _state.gyro_scale(1) = 1.0f; _state.gyro_scale(2) = 1.0f; _state.accel_z_bias = 0.0f; _state.mag_I.setZero(); _state.mag_B.setZero(); _state.wind_vel.setZero(); _state.quat_nominal.setZero(); _state.quat_nominal(0) = 1.0f; _params.mag_delay_ms = 0; _params.baro_delay_ms = 0; _params.gps_delay_ms = 200; _params.airspeed_delay_ms = 0; _params.requiredEph = 200; _params.requiredEpv = 200; _params.gyro_noise = 1e-3f; _params.accel_noise = 1e-1f; _params.gyro_bias_p_noise = 1e-5f; _params.accel_bias_p_noise = 1e-3f; _params.gyro_scale_p_noise = 1e-4f; _params.mag_p_noise = 1e-2f; _params.wind_vel_p_noise = 0.05f; _params.gps_vel_noise = 0.05f; _params.gps_pos_noise = 1.0f; _params.baro_noise = 0.1f; _params.mag_heading_noise = 3e-2f; _params.mag_declination_deg = 10.0f; _params.heading_innov_gate = 0.5f; _dt_imu_avg = 0.0f; _imu_time_last = time_usec; _imu_sample_delayed.delta_ang.setZero(); _imu_sample_delayed.delta_vel.setZero(); _imu_sample_delayed.delta_ang_dt = 0.0f; _imu_sample_delayed.delta_vel_dt = 0.0f; _imu_sample_delayed.time_us = time_usec; _imu_down_sampled.delta_ang.setZero(); _imu_down_sampled.delta_vel.setZero(); _imu_down_sampled.delta_ang_dt = 0.0f; _imu_down_sampled.delta_vel_dt = 0.0f; _imu_down_sampled.time_us = time_usec; _q_down_sampled(0) = 1.0f; _q_down_sampled(1) = 0.0f; _q_down_sampled(2) = 0.0f; _q_down_sampled(3) = 0.0f; _imu_ticks = 0; _imu_updated = false; _start_predict_enabled = false; _initialised = false; _gps_initialised = false; _gps_speed_valid = false; _mag_healthy = false; _in_air = true; // XXX get this flag from the application _time_last_imu = 0; _time_last_gps = 0; _time_last_mag = 0; _time_last_baro = 0; _time_last_range = 0; _time_last_airspeed = 0; memset(&_fault_status, 0, sizeof(_fault_status)); } void EstimatorBase::initialiseGPS(struct gps_message *gps) { //Check if the GPS fix is good enough for us to use if (gps_is_good(gps)) { printf("gps is good\n"); // Initialise projection double lat = gps->lat / 1.0e7; double lon = gps->lon / 1.0e7; map_projection_init(&_posRef, lat, lon); _gps_alt_ref = gps->alt / 1e3f; _gps_initialised = true; } } bool EstimatorBase::gps_is_good(struct gps_message *gps) { // go through apm implementation of calcGpsGoodToAlign for fancier checks if ((gps->fix_type >= 3) && (gps->eph < _params.requiredEph) && (gps->epv < _params.requiredEpv)) { return true; } else { return false; } } void EstimatorBase::printStoredIMU() { printf("---------Printing IMU data buffer------------\n"); for (int i = 0; i < IMU_BUFFER_LENGTH; i++) { printIMU(&_imu_buffer[i]); } } void EstimatorBase::printIMU(struct imuSample *data) { printf("time %i\n", data->time_us); printf("delta_ang_dt %.5f\n", (double)data->delta_ang_dt); printf("delta_vel_dt %.5f\n", (double)data->delta_vel_dt); printf("dA: %.5f %.5f %.5f \n", (double)data->delta_ang(0), (double)data->delta_ang(1), (double)data->delta_ang(2)); printf("dV: %.5f %.5f %.5f \n\n", (double)data->delta_vel(0), (double)data->delta_vel(1), (double)data->delta_vel(2)); } void EstimatorBase::printQuaternion(Quaternion &q) { printf("q1 %.5f q2 %.5f q3 %.5f q4 %.5f\n", (double)q(0), (double)q(1), (double)q(2), (double)q(3)); } void EstimatorBase::print_imu_avg_time() { printf("dt_avg: %.5f\n", (double)_dt_imu_avg); } void EstimatorBase::printStoredMag() { printf("---------Printing mag data buffer------------\n"); for (int i = 0; i < OBS_BUFFER_LENGTH; i++) { printMag(&_mag_buffer[i]); } } void EstimatorBase::printMag(struct magSample *data) { printf("time %i\n", data->time_us); printf("mag: %.5f %.5f %.5f \n\n", (double)data->mag(0), (double)data->mag(1), (double)data->mag(2)); } void EstimatorBase::printBaro(struct baroSample *data) { printf("time %i\n", data->time_us); printf("baro: %.5f\n\n", (double)data->hgt); } void EstimatorBase::printStoredBaro() { printf("---------Printing baro data buffer------------\n"); for (int i = 0; i < OBS_BUFFER_LENGTH; i++) { printBaro(&_baro_buffer[i]); } } void EstimatorBase::printGps(struct gpsSample *data) { printf("time %i\n", data->time_us); printf("gps pos: %.5f %.5f %.5f\n", (double)data->pos(0), (double)data->pos(1), (double)data->hgt); printf("gps vel %.5f %.5f %.5f\n\n", (double)data->vel(0), (double)data->vel(1), (double)data->vel(2)); } void EstimatorBase::printStoredGps() { printf("---------Printing GPS data buffer------------\n"); for (int i = 0; i < OBS_BUFFER_LENGTH; i++) { printGps(&_gps_buffer[i]); } }