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Set uavcan publisher priorities Switch to ardupilot rtcm message and add heading accuracy
513 lines
14 KiB
C++
513 lines
14 KiB
C++
/****************************************************************************
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*
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* Copyright (c) 2014, 2015 PX4 Development Team. All rights reserved.
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*
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* Redistribution and use in source and binary forms, with or without
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* modification, are permitted provided that the following conditions
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* are met:
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*
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* 1. Redistributions of source code must retain the above copyright
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* notice, this list of conditions and the following disclaimer.
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* 2. Redistributions in binary form must reproduce the above copyright
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* notice, this list of conditions and the following disclaimer in
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* the documentation and/or other materials provided with the
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* distribution.
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* 3. Neither the name PX4 nor the names of its contributors may be
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* used to endorse or promote products derived from this software
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* without specific prior written permission.
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*
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* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
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* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
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* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
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* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
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* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
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* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
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* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
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* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
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* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
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* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
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* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
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* POSSIBILITY OF SUCH DAMAGE.
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*
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****************************************************************************/
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/**
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* @file gnss.cpp
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*
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* @author Pavel Kirienko <pavel.kirienko@gmail.com>
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* @author Andrew Chambers <achamber@gmail.com>
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*
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*/
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#include "gnss.hpp"
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#include <cstdint>
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#include <drivers/drv_hrt.h>
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#include <systemlib/err.h>
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#include <mathlib/mathlib.h>
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using namespace time_literals;
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const char *const UavcanGnssBridge::NAME = "gnss";
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UavcanGnssBridge::UavcanGnssBridge(uavcan::INode &node) :
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UavcanSensorBridgeBase("uavcan_gnss", ORB_ID(sensor_gps)),
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_node(node),
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_sub_auxiliary(node),
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_sub_fix(node),
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_sub_fix2(node),
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_pub_rtcm(node),
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_channel_using_fix2(new bool[_max_channels]),
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_rtcm_perf(perf_alloc(PC_INTERVAL, "uavcan: gnss: rtcm pub"))
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{
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for (uint8_t i = 0; i < _max_channels; i++) {
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_channel_using_fix2[i] = false;
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}
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set_device_type(DRV_GPS_DEVTYPE_UAVCAN);
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}
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UavcanGnssBridge::~UavcanGnssBridge()
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{
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delete [] _channel_using_fix2;
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perf_free(_rtcm_perf);
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}
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int
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UavcanGnssBridge::init()
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{
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int res = _sub_auxiliary.start(AuxiliaryCbBinder(this, &UavcanGnssBridge::gnss_auxiliary_sub_cb));
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if (res < 0) {
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PX4_WARN("GNSS auxiliary sub failed %i", res);
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return res;
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}
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res = _sub_fix.start(FixCbBinder(this, &UavcanGnssBridge::gnss_fix_sub_cb));
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if (res < 0) {
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PX4_WARN("GNSS fix sub failed %i", res);
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return res;
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}
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res = _sub_fix2.start(Fix2CbBinder(this, &UavcanGnssBridge::gnss_fix2_sub_cb));
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if (res < 0) {
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PX4_WARN("GNSS fix2 sub failed %i", res);
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return res;
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}
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_pub_rtcm.setPriority(uavcan::TransferPriority::NumericallyMax);
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return res;
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}
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void
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UavcanGnssBridge::gnss_auxiliary_sub_cb(const uavcan::ReceivedDataStructure<uavcan::equipment::gnss::Auxiliary> &msg)
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{
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// store latest hdop and vdop for use in process_fixx();
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_last_gnss_auxiliary_timestamp = hrt_absolute_time();
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_last_gnss_auxiliary_hdop = msg.hdop;
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_last_gnss_auxiliary_vdop = msg.vdop;
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}
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void
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UavcanGnssBridge::gnss_fix_sub_cb(const uavcan::ReceivedDataStructure<uavcan::equipment::gnss::Fix> &msg)
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{
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// Check to see if this node is also publishing a Fix2 message.
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// If so, ignore the old "Fix" message for this node.
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const int8_t ch = get_channel_index_for_node(msg.getSrcNodeID().get());
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if (ch > -1 && _channel_using_fix2[ch]) {
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return;
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}
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uint8_t fix_type = msg.status;
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const bool valid_pos_cov = !msg.position_covariance.empty();
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const bool valid_vel_cov = !msg.velocity_covariance.empty();
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float pos_cov[9];
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msg.position_covariance.unpackSquareMatrix(pos_cov);
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float vel_cov[9];
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msg.velocity_covariance.unpackSquareMatrix(vel_cov);
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process_fixx(msg, fix_type, pos_cov, vel_cov, valid_pos_cov, valid_vel_cov, NAN, NAN, NAN);
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}
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void
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UavcanGnssBridge::gnss_fix2_sub_cb(const uavcan::ReceivedDataStructure<uavcan::equipment::gnss::Fix2> &msg)
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{
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using uavcan::equipment::gnss::Fix2;
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const int8_t ch = get_channel_index_for_node(msg.getSrcNodeID().get());
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if (ch > -1 && !_channel_using_fix2[ch]) {
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PX4_WARN("GNSS Fix2 msg detected for ch %d; disabling Fix msg for this node", ch);
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_channel_using_fix2[ch] = true;
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}
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uint8_t fix_type = msg.status;
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switch (msg.mode) {
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case Fix2::MODE_DGPS:
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fix_type = 4; // RTCM code differential
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break;
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case Fix2::MODE_RTK:
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switch (msg.sub_mode) {
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case Fix2::SUB_MODE_RTK_FLOAT:
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fix_type = 5; // RTK float
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break;
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case Fix2::SUB_MODE_RTK_FIXED:
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fix_type = 6; // RTK fixed
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break;
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}
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break;
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}
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float pos_cov[9] {};
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float vel_cov[9] {};
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bool valid_covariances = true;
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switch (msg.covariance.size()) {
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case 1: {
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// Scalar matrix
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const auto x = msg.covariance[0];
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pos_cov[0] = x;
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pos_cov[4] = x;
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pos_cov[8] = x;
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vel_cov[0] = x;
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vel_cov[4] = x;
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vel_cov[8] = x;
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}
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break;
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case 6: {
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// Diagonal matrix (the most common case)
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pos_cov[0] = msg.covariance[0];
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pos_cov[4] = msg.covariance[1];
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pos_cov[8] = msg.covariance[2];
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vel_cov[0] = msg.covariance[3];
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vel_cov[4] = msg.covariance[4];
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vel_cov[8] = msg.covariance[5];
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}
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break;
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case 21: {
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// Upper triangular matrix.
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// This code has been carefully optimized by hand. We could use unpackSquareMatrix(), but it's slow.
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// Sub-matrix indexes (empty squares contain velocity-position covariance data):
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// 0 1 2
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// 1 6 7
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// 2 7 11
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// 15 16 17
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// 16 18 19
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// 17 19 20
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pos_cov[0] = msg.covariance[0];
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pos_cov[1] = msg.covariance[1];
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pos_cov[2] = msg.covariance[2];
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pos_cov[3] = msg.covariance[1];
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pos_cov[4] = msg.covariance[6];
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pos_cov[5] = msg.covariance[7];
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pos_cov[6] = msg.covariance[2];
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pos_cov[7] = msg.covariance[7];
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pos_cov[8] = msg.covariance[11];
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vel_cov[0] = msg.covariance[15];
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vel_cov[1] = msg.covariance[16];
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vel_cov[2] = msg.covariance[17];
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vel_cov[3] = msg.covariance[16];
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vel_cov[4] = msg.covariance[18];
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vel_cov[5] = msg.covariance[19];
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vel_cov[6] = msg.covariance[17];
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vel_cov[7] = msg.covariance[19];
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vel_cov[8] = msg.covariance[20];
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}
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/* FALLTHROUGH */
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case 36: {
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// Full matrix 6x6.
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// This code has been carefully optimized by hand. We could use unpackSquareMatrix(), but it's slow.
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// Sub-matrix indexes (empty squares contain velocity-position covariance data):
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// 0 1 2
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// 6 7 8
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// 12 13 14
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// 21 22 23
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// 27 28 29
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// 33 34 35
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pos_cov[0] = msg.covariance[0];
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pos_cov[1] = msg.covariance[1];
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pos_cov[2] = msg.covariance[2];
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pos_cov[3] = msg.covariance[6];
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pos_cov[4] = msg.covariance[7];
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pos_cov[5] = msg.covariance[8];
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pos_cov[6] = msg.covariance[12];
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pos_cov[7] = msg.covariance[13];
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pos_cov[8] = msg.covariance[14];
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vel_cov[0] = msg.covariance[21];
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vel_cov[1] = msg.covariance[22];
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vel_cov[2] = msg.covariance[23];
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vel_cov[3] = msg.covariance[27];
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vel_cov[4] = msg.covariance[28];
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vel_cov[5] = msg.covariance[29];
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vel_cov[6] = msg.covariance[33];
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vel_cov[7] = msg.covariance[34];
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vel_cov[8] = msg.covariance[35];
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}
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/* FALLTHROUGH */
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default: {
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// Either empty or invalid sized, interpret as zero matrix
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valid_covariances = false;
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break; // Nothing to do
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}
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}
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float heading = NAN;
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float heading_offset = NAN;
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float heading_accuracy = NAN;
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// Use ecef_position_velocity for now... There is no heading field
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if (!msg.ecef_position_velocity.empty()) {
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heading = msg.ecef_position_velocity[0].velocity_xyz[0];
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if (!isnan(msg.ecef_position_velocity[0].velocity_xyz[1])) {
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heading_offset = msg.ecef_position_velocity[0].velocity_xyz[1];
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}
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if (!isnan(msg.ecef_position_velocity[0].velocity_xyz[2])) {
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heading_accuracy = msg.ecef_position_velocity[0].velocity_xyz[2];
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}
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}
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process_fixx(msg, fix_type, pos_cov, vel_cov, valid_covariances, valid_covariances, heading, heading_offset,
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heading_accuracy);
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}
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template <typename FixType>
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void UavcanGnssBridge::process_fixx(const uavcan::ReceivedDataStructure<FixType> &msg,
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uint8_t fix_type,
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const float (&pos_cov)[9], const float (&vel_cov)[9],
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const bool valid_pos_cov, const bool valid_vel_cov,
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const float heading, const float heading_offset,
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const float heading_accuracy)
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{
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sensor_gps_s report{};
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report.device_id = get_device_id();
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/*
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* FIXME HACK
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* There used to be the following line of code:
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* report.timestamp_position = msg.getMonotonicTimestamp().toUSec();
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* It stopped working when the time sync feature has been introduced, because it caused libuavcan
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* to use an independent time source (based on hardware TIM5) instead of HRT.
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* The proper solution is to be developed.
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*/
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report.timestamp = hrt_absolute_time();
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report.lat = msg.latitude_deg_1e8 / 10;
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report.lon = msg.longitude_deg_1e8 / 10;
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report.alt = msg.height_msl_mm;
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report.alt_ellipsoid = msg.height_ellipsoid_mm;
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if (valid_pos_cov) {
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// Horizontal position uncertainty
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const float horizontal_pos_variance = math::max(pos_cov[0], pos_cov[4]);
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report.eph = (horizontal_pos_variance > 0) ? sqrtf(horizontal_pos_variance) : -1.0F;
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// Vertical position uncertainty
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report.epv = (pos_cov[8] > 0) ? sqrtf(pos_cov[8]) : -1.0F;
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} else {
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report.eph = -1.0F;
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report.epv = -1.0F;
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}
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if (valid_vel_cov) {
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report.s_variance_m_s = math::max(math::max(vel_cov[0], vel_cov[4]), vel_cov[8]);
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/* There is a nonlinear relationship between the velocity vector and the heading.
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* Use Jacobian to transform velocity covariance to heading covariance
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*
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* Nonlinear equation:
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* heading = atan2(vel_e_m_s, vel_n_m_s)
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* For math, see http://en.wikipedia.org/wiki/Atan2#Derivative
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*
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* To calculate the variance of heading from the variance of velocity,
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* cov(heading) = J(velocity)*cov(velocity)*J(velocity)^T
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*/
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float vel_n = msg.ned_velocity[0];
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float vel_e = msg.ned_velocity[1];
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float vel_n_sq = vel_n * vel_n;
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float vel_e_sq = vel_e * vel_e;
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report.c_variance_rad =
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(vel_e_sq * vel_cov[0] +
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-2 * vel_n * vel_e * vel_cov[1] + // Covariance matrix is symmetric
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vel_n_sq * vel_cov[4]) / ((vel_n_sq + vel_e_sq) * (vel_n_sq + vel_e_sq));
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} else {
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report.s_variance_m_s = -1.0F;
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report.c_variance_rad = -1.0F;
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}
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report.fix_type = fix_type;
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report.vel_n_m_s = msg.ned_velocity[0];
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report.vel_e_m_s = msg.ned_velocity[1];
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report.vel_d_m_s = msg.ned_velocity[2];
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report.vel_m_s = sqrtf(report.vel_n_m_s * report.vel_n_m_s +
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report.vel_e_m_s * report.vel_e_m_s +
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report.vel_d_m_s * report.vel_d_m_s);
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report.cog_rad = atan2f(report.vel_e_m_s, report.vel_n_m_s);
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report.vel_ned_valid = true;
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report.timestamp_time_relative = 0;
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const uint64_t gnss_ts_usec = uavcan::UtcTime(msg.gnss_timestamp).toUSec();
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switch (msg.gnss_time_standard) {
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case FixType::GNSS_TIME_STANDARD_UTC:
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report.time_utc_usec = gnss_ts_usec;
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break;
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case FixType::GNSS_TIME_STANDARD_GPS:
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if (msg.num_leap_seconds > 0) {
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report.time_utc_usec = gnss_ts_usec - msg.num_leap_seconds + 9;
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}
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break;
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case FixType::GNSS_TIME_STANDARD_TAI:
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if (msg.num_leap_seconds > 0) {
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report.time_utc_usec = gnss_ts_usec - msg.num_leap_seconds - 10;
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}
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break;
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default:
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break;
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}
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// If we haven't already done so, set the system clock using GPS data
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if (valid_pos_cov && !_system_clock_set) {
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timespec ts{};
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// get the whole microseconds
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ts.tv_sec = report.time_utc_usec / 1000000ULL;
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// get the remainder microseconds and convert to nanoseconds
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ts.tv_nsec = (report.time_utc_usec % 1000000ULL) * 1000;
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px4_clock_settime(CLOCK_REALTIME, &ts);
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_system_clock_set = true;
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}
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report.satellites_used = msg.sats_used;
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if (hrt_elapsed_time(&_last_gnss_auxiliary_timestamp) < 2_s) {
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report.hdop = _last_gnss_auxiliary_hdop;
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report.vdop = _last_gnss_auxiliary_vdop;
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} else {
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// Using PDOP for HDOP and VDOP
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// Relevant discussion: https://github.com/PX4/Firmware/issues/5153
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report.hdop = msg.pdop;
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report.vdop = msg.pdop;
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}
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report.heading = heading;
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report.heading_offset = heading_offset;
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report.heading_accuracy = heading_accuracy;
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publish(msg.getSrcNodeID().get(), &report);
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}
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void UavcanGnssBridge::update()
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{
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handleInjectDataTopic();
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}
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// Partially taken from src/drivers/gps/gps.cpp
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// This listens on the gps_inject_data uORB topic for RTCM data
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// sent from a GCS (usually over MAVLINK GPS_RTCM_DATA).
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// Forwarding this data to the UAVCAN bus enables DGPS/RTK GPS
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// to work.
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void UavcanGnssBridge::handleInjectDataTopic()
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{
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bool updated = false;
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// Limit maximum number of GPS injections to 6 since usually
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// GPS injections should consist of 1-4 packets (GPS, Glonass, BeiDou, Galileo).
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// Looking at 6 packets thus guarantees, that at least a full injection
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// data set is evaluated.
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const size_t max_num_injections = 6;
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size_t num_injections = 0;
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do {
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num_injections++;
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updated = _orb_inject_data_sub.updated();
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if (updated) {
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gps_inject_data_s msg;
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if (_orb_inject_data_sub.copy(&msg)) {
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/* Write the message to the gps device. Note that the message could be fragmented.
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* But as we don't write anywhere else to the device during operation, we don't
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* need to assemble the message first.
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*/
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injectData(msg.data, msg.len);
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}
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}
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} while (updated && num_injections < max_num_injections);
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}
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bool UavcanGnssBridge::injectData(const uint8_t *const data, const size_t data_len)
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{
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using ardupilot::gnss::MovingBaselineData;
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perf_count(_rtcm_perf);
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MovingBaselineData msg;
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const size_t capacity = msg.data.capacity();
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size_t written = 0;
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bool result = true;
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while (result && written < data_len) {
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size_t chunk_size = data_len - written;
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if (chunk_size > capacity) {
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chunk_size = capacity;
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}
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for (size_t i = 0; i < chunk_size; ++i) {
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msg.data.push_back(data[written]);
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written += 1;
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}
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result = _pub_rtcm.broadcast(msg) >= 0;
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msg.data.clear();
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}
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return result;
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}
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void UavcanGnssBridge::print_status() const
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{
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UavcanSensorBridgeBase::print_status();
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perf_print_counter(_rtcm_perf);
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}
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