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path: root/src/modules/uavcan/gnss_receiver.cpp
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/****************************************************************************
 *
 *   Copyright (C) 2014 PX4 Development Team. 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 PX4 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 gnss_receiver.cpp
 *
 * @author Pavel Kirienko <pavel.kirienko@gmail.com>
 * @author Andrew Chambers <achamber@gmail.com>
 *
 */

#include "gnss_receiver.hpp"
#include <systemlib/err.h>

#define MM_PER_CM 10	// Millimeters per centimeter

UavcanGnssReceiver::UavcanGnssReceiver(uavcan::INode &node) :
	_node(node),
	_uavcan_sub_status(node),
	_report_pub(-1)
{
}

int UavcanGnssReceiver::init()
{
	int res = -1;

	// GNSS fix subscription
	res = _uavcan_sub_status.start(FixCbBinder(this, &UavcanGnssReceiver::gnss_fix_sub_cb));
	if (res < 0)
	{
		warnx("GNSS fix sub failed %i", res);
		return res;
	}

	// Clear the uORB GPS report
	memset(&_report, 0, sizeof(_report));

	return res;
}

void UavcanGnssReceiver::gnss_fix_sub_cb(const uavcan::ReceivedDataStructure<uavcan::equipment::gnss::Fix> &msg)
{
	_report.timestamp_position = hrt_absolute_time();
	_report.lat = msg.lat_1e7;
	_report.lon = msg.lon_1e7;
	_report.alt = msg.alt_1e2 * MM_PER_CM;					// Convert from centimeter (1e2) to millimeters (1e3)

	_report.timestamp_variance = _report.timestamp_position;
	_report.s_variance_m_s = msg.velocity_covariance[0] + msg.velocity_covariance[4] + msg.velocity_covariance[8];
	_report.p_variance_m = msg.position_covariance[0] + msg.position_covariance[4];

	/* Use Jacobian to transform velocity covariance to heading covariance
	 * heading = atan2(vel_e_m_s, vel_n_m_s)
	 * For math, see http://en.wikipedia.org/wiki/Atan2#Derivative
	 *
	 * To calculate the variance of heading from the variance of velocity,
	 * var(heading) = J(velocity)*var(velocity)*J(velocity)^T
	 */
	_report.c_variance_rad =
			msg.ned_velocity[1] * msg.ned_velocity[1] * msg.velocity_covariance[0] +
			-2*msg.ned_velocity[1] * msg.ned_velocity[0] * msg.velocity_covariance[1] +
			msg.ned_velocity[0] * msg.ned_velocity[0] * msg.velocity_covariance[4];

	_report.fix_type = msg.status;

	_report.eph_m = sqrtf(_report.p_variance_m);
	_report.epv_m = sqrtf(msg.position_covariance[8]);

	_report.timestamp_velocity = _report.timestamp_position;
	_report.vel_n_m_s = msg.ned_velocity[0];
	_report.vel_e_m_s = msg.ned_velocity[1];
	_report.vel_d_m_s = msg.ned_velocity[2];
	_report.vel_m_s = sqrtf(_report.vel_n_m_s * _report.vel_n_m_s + _report.vel_e_m_s * _report.vel_e_m_s + _report.vel_d_m_s * _report.vel_d_m_s);
	_report.cog_rad = atan2f(_report.vel_e_m_s, _report.vel_n_m_s);
	_report.vel_ned_valid = true;

	_report.timestamp_time = _report.timestamp_position;
	_report.time_gps_usec = msg.timestamp.husec * msg.timestamp.USEC_PER_LSB;	// Convert to microseconds

	_report.timestamp_satellites = _report.timestamp_position;
	_report.satellites_visible = msg.sats_used;
	_report.satellite_info_available = 0;					// Set to 0 for no info available

	if (_report_pub > 0) {
		orb_publish(ORB_ID(vehicle_gps_position), _report_pub, &_report);

	} else {
		_report_pub = orb_advertise(ORB_ID(vehicle_gps_position), &_report);
	}

}