forked from Archive/PX4-Autopilot
829 lines
26 KiB
C++
829 lines
26 KiB
C++
/****************************************************************************
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*
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* Copyright (c) 2012-2014 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 geo.c
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*
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* Geo / math functions to perform geodesic calculations
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*
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* @author Thomas Gubler <thomasgubler@student.ethz.ch>
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* @author Julian Oes <joes@student.ethz.ch>
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* @author Lorenz Meier <lm@inf.ethz.ch>
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* @author Anton Babushkin <anton.babushkin@me.com>
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*/
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#ifdef POSIX_SHARED
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#include "ecl.h"
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#include <stdio.h>
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#include <math.h>
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#include <stdbool.h>
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#include <string.h>
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#include <float.h>
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/****************************************************************************
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*
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* Copyright (c) 2014 MAV GEO Library (MAVGEO). 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
|
|
* 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
|
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* distribution.
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* 3. Neither the name MAVGEO 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 geo_mag_declination.c
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*
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* Calculation / lookup table for earth magnetic field declination.
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*
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* Lookup table from Scott Ferguson <scottfromscott@gmail.com>
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*
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* XXX Lookup table currently too coarse in resolution (only full degrees)
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* and lat/lon res - needs extension medium term.
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*
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*/
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#include <stdint.h>
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#include "geo.h"
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/** set this always to the sampling in degrees for the table below */
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#define SAMPLING_RES 10.0f
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#define SAMPLING_MIN_LAT -60.0f
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#define SAMPLING_MAX_LAT 60.0f
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#define SAMPLING_MIN_LON -180.0f
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#define SAMPLING_MAX_LON 180.0f
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static const int8_t declination_table[13][37] = \
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{
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{ 46, 45, 44, 42, 41, 40, 38, 36, 33, 28, 23, 16, 10, 4, -1, -5, -9, -14, -19, -26, -33, -40, -48, -55, -61, -66, -71, -74, -75, -72, -61, -25, 22, 40, 45, 47, 46 },
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{ 30, 30, 30, 30, 29, 29, 29, 29, 27, 24, 18, 11, 3, -3, -9, -12, -15, -17, -21, -26, -32, -39, -45, -51, -55, -57, -56, -53, -44, -31, -14, 0, 13, 21, 26, 29, 30 },
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{ 21, 22, 22, 22, 22, 22, 22, 22, 21, 18, 13, 5, -3, -11, -17, -20, -21, -22, -23, -25, -29, -35, -40, -44, -45, -44, -40, -32, -22, -12, -3, 3, 9, 14, 18, 20, 21 },
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{ 16, 17, 17, 17, 17, 17, 16, 16, 16, 13, 8, 0, -9, -16, -21, -24, -25, -25, -23, -20, -21, -24, -28, -31, -31, -29, -24, -17, -9, -3, 0, 4, 7, 10, 13, 15, 16 },
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{ 12, 13, 13, 13, 13, 13, 12, 12, 11, 9, 3, -4, -12, -19, -23, -24, -24, -22, -17, -12, -9, -10, -13, -17, -18, -16, -13, -8, -3, 0, 1, 3, 6, 8, 10, 12, 12 },
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{ 10, 10, 10, 10, 10, 10, 10, 9, 9, 6, 0, -6, -14, -20, -22, -22, -19, -15, -10, -6, -2, -2, -4, -7, -8, -8, -7, -4, 0, 1, 1, 2, 4, 6, 8, 10, 10 },
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{ 9, 9, 9, 9, 9, 9, 8, 8, 7, 4, -1, -8, -15, -19, -20, -18, -14, -9, -5, -2, 0, 1, 0, -2, -3, -4, -3, -2, 0, 0, 0, 1, 3, 5, 7, 8, 9 },
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{ 8, 8, 8, 9, 9, 9, 8, 8, 6, 2, -3, -9, -15, -18, -17, -14, -10, -6, -2, 0, 1, 2, 2, 0, -1, -1, -2, -1, 0, 0, 0, 0, 1, 3, 5, 7, 8 },
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{ 8, 9, 9, 10, 10, 10, 10, 8, 5, 0, -5, -11, -15, -16, -15, -12, -8, -4, -1, 0, 2, 3, 2, 1, 0, 0, 0, 0, 0, -1, -2, -2, -1, 0, 3, 6, 8 },
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{ 6, 9, 10, 11, 12, 12, 11, 9, 5, 0, -7, -12, -15, -15, -13, -10, -7, -3, 0, 1, 2, 3, 3, 3, 2, 1, 0, 0, -1, -3, -4, -5, -5, -2, 0, 3, 6 },
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{ 5, 8, 11, 13, 15, 15, 14, 11, 5, -1, -9, -14, -17, -16, -14, -11, -7, -3, 0, 1, 3, 4, 5, 5, 5, 4, 3, 1, -1, -4, -7, -8, -8, -6, -2, 1, 5 },
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{ 4, 8, 12, 15, 17, 18, 16, 12, 5, -3, -12, -18, -20, -19, -16, -13, -8, -4, -1, 1, 4, 6, 8, 9, 9, 9, 7, 3, -1, -6, -10, -12, -11, -9, -5, 0, 4 },
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{ 3, 9, 14, 17, 20, 21, 19, 14, 4, -8, -19, -25, -26, -25, -21, -17, -12, -7, -2, 1, 5, 9, 13, 15, 16, 16, 13, 7, 0, -7, -12, -15, -14, -11, -6, -1, 3 },
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};
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static float get_lookup_table_val(unsigned lat, unsigned lon);
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float get_mag_declination(float lat, float lon)
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{
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/*
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* If the values exceed valid ranges, return zero as default
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* as we have no way of knowing what the closest real value
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* would be.
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*/
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if (lat < -90.0f || lat > 90.0f ||
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lon < -180.0f || lon > 180.0f) {
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return 0.0f;
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}
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/* round down to nearest sampling resolution */
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int min_lat = (int)(lat / SAMPLING_RES) * SAMPLING_RES;
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int min_lon = (int)(lon / SAMPLING_RES) * SAMPLING_RES;
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/* for the rare case of hitting the bounds exactly
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* the rounding logic wouldn't fit, so enforce it.
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*/
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/* limit to table bounds - required for maxima even when table spans full globe range */
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if (lat <= SAMPLING_MIN_LAT) {
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min_lat = SAMPLING_MIN_LAT;
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}
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if (lat >= SAMPLING_MAX_LAT) {
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min_lat = (int)(lat / SAMPLING_RES) * SAMPLING_RES - SAMPLING_RES;
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}
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if (lon <= SAMPLING_MIN_LON) {
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min_lon = SAMPLING_MIN_LON;
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}
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if (lon >= SAMPLING_MAX_LON) {
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min_lon = (int)(lon / SAMPLING_RES) * SAMPLING_RES - SAMPLING_RES;
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}
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/* find index of nearest low sampling point */
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unsigned min_lat_index = (-(SAMPLING_MIN_LAT) + min_lat) / SAMPLING_RES;
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unsigned min_lon_index = (-(SAMPLING_MIN_LON) + min_lon) / SAMPLING_RES;
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float declination_sw = get_lookup_table_val(min_lat_index, min_lon_index);
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float declination_se = get_lookup_table_val(min_lat_index, min_lon_index + 1);
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float declination_ne = get_lookup_table_val(min_lat_index + 1, min_lon_index + 1);
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float declination_nw = get_lookup_table_val(min_lat_index + 1, min_lon_index);
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/* perform bilinear interpolation on the four grid corners */
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float declination_min = ((lon - min_lon) / SAMPLING_RES) * (declination_se - declination_sw) + declination_sw;
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float declination_max = ((lon - min_lon) / SAMPLING_RES) * (declination_ne - declination_nw) + declination_nw;
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return ((lat - min_lat) / SAMPLING_RES) * (declination_max - declination_min) + declination_min;
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}
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float get_lookup_table_val(unsigned lat_index, unsigned lon_index)
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{
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return declination_table[lat_index][lon_index];
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}
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/*
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* Azimuthal Equidistant Projection
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* formulas according to: http://mathworld.wolfram.com/AzimuthalEquidistantProjection.html
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*/
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static struct map_projection_reference_s mp_ref = {0.0, 0.0, 0.0, 0.0, false, 0};
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static struct globallocal_converter_reference_s gl_ref = {0.0f, false};
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bool map_projection_global_initialized()
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{
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return map_projection_initialized(&mp_ref);
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}
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bool map_projection_initialized(const struct map_projection_reference_s *ref)
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{
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return ref->init_done;
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}
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uint64_t map_projection_global_timestamp()
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{
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return map_projection_timestamp(&mp_ref);
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}
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uint64_t map_projection_timestamp(const struct map_projection_reference_s *ref)
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{
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return ref->timestamp;
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}
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int map_projection_global_init(double lat_0, double lon_0,
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uint64_t timestamp) //lat_0, lon_0 are expected to be in correct format: -> 47.1234567 and not 471234567
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{
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return map_projection_init_timestamped(&mp_ref, lat_0, lon_0, timestamp);
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}
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int map_projection_init_timestamped(struct map_projection_reference_s *ref, double lat_0, double lon_0,
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uint64_t timestamp) //lat_0, lon_0 are expected to be in correct format: -> 47.1234567 and not 471234567
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{
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ref->lat_rad = lat_0 * M_DEG_TO_RAD;
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ref->lon_rad = lon_0 * M_DEG_TO_RAD;
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ref->sin_lat = sin(ref->lat_rad);
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ref->cos_lat = cos(ref->lat_rad);
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ref->timestamp = timestamp;
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ref->init_done = true;
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return 0;
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}
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int map_projection_global_reference(double *ref_lat_rad, double *ref_lon_rad)
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{
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return map_projection_reference(&mp_ref, ref_lat_rad, ref_lon_rad);
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}
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int map_projection_reference(const struct map_projection_reference_s *ref, double *ref_lat_rad,
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double *ref_lon_rad)
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{
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if (!map_projection_initialized(ref)) {
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return -1;
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}
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*ref_lat_rad = ref->lat_rad;
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*ref_lon_rad = ref->lon_rad;
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return 0;
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}
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int map_projection_global_project(double lat, double lon, float *x, float *y)
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{
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return map_projection_project(&mp_ref, lat, lon, x, y);
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}
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int map_projection_project(const struct map_projection_reference_s *ref, double lat, double lon, float *x,
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float *y)
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{
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if (!map_projection_initialized(ref)) {
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return -1;
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}
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double lat_rad = lat * M_DEG_TO_RAD;
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double lon_rad = lon * M_DEG_TO_RAD;
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double sin_lat = sin(lat_rad);
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double cos_lat = cos(lat_rad);
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double cos_d_lon = cos(lon_rad - ref->lon_rad);
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double arg = ref->sin_lat * sin_lat + ref->cos_lat * cos_lat * cos_d_lon;
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if (arg > 1.0) {
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arg = 1.0;
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} else if (arg < -1.0) {
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arg = -1.0;
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}
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double c = acos(arg);
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double k = (fabs(c) < DBL_EPSILON) ? 1.0 : (c / sin(c));
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*x = k * (ref->cos_lat * sin_lat - ref->sin_lat * cos_lat * cos_d_lon) * CONSTANTS_RADIUS_OF_EARTH;
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*y = k * cos_lat * sin(lon_rad - ref->lon_rad) * CONSTANTS_RADIUS_OF_EARTH;
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return 0;
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}
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int map_projection_global_reproject(float x, float y, double *lat, double *lon)
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{
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return map_projection_reproject(&mp_ref, x, y, lat, lon);
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}
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int map_projection_reproject(const struct map_projection_reference_s *ref, float x, float y, double *lat,
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double *lon)
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{
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if (!map_projection_initialized(ref)) {
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return -1;
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}
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double x_rad = x / CONSTANTS_RADIUS_OF_EARTH;
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double y_rad = y / CONSTANTS_RADIUS_OF_EARTH;
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double c = sqrtf(x_rad * x_rad + y_rad * y_rad);
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double sin_c = sin(c);
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double cos_c = cos(c);
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double lat_rad;
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double lon_rad;
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if (fabs(c) > DBL_EPSILON) {
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lat_rad = asin(cos_c * ref->sin_lat + (x_rad * sin_c * ref->cos_lat) / c);
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lon_rad = (ref->lon_rad + atan2(y_rad * sin_c, c * ref->cos_lat * cos_c - x_rad * ref->sin_lat * sin_c));
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} else {
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lat_rad = ref->lat_rad;
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lon_rad = ref->lon_rad;
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}
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*lat = lat_rad * 180.0 / M_PI;
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*lon = lon_rad * 180.0 / M_PI;
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return 0;
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}
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int map_projection_global_getref(double *lat_0, double *lon_0)
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{
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if (!map_projection_global_initialized()) {
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return -1;
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}
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if (lat_0 != nullptr) {
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*lat_0 = M_RAD_TO_DEG * mp_ref.lat_rad;
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}
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if (lon_0 != nullptr) {
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*lon_0 = M_RAD_TO_DEG * mp_ref.lon_rad;
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}
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return 0;
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}
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int globallocalconverter_init(double lat_0, double lon_0, float alt_0, uint64_t timestamp)
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{
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gl_ref.alt = alt_0;
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if (!map_projection_global_init(lat_0, lon_0, timestamp)) {
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gl_ref.init_done = true;
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return 0;
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} else {
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gl_ref.init_done = false;
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return -1;
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}
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}
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bool globallocalconverter_initialized()
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{
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return gl_ref.init_done && map_projection_global_initialized();
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}
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int globallocalconverter_tolocal(double lat, double lon, float alt, float *x, float *y, float *z)
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{
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if (!map_projection_global_initialized()) {
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return -1;
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}
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map_projection_global_project(lat, lon, x, y);
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*z = gl_ref.alt - alt;
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return 0;
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}
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int globallocalconverter_toglobal(float x, float y, float z, double *lat, double *lon, float *alt)
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{
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if (!map_projection_global_initialized()) {
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return -1;
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}
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map_projection_global_reproject(x, y, lat, lon);
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*alt = gl_ref.alt - z;
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return 0;
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}
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int globallocalconverter_getref(double *lat_0, double *lon_0, float *alt_0)
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{
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if (!map_projection_global_initialized()) {
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return -1;
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}
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if (map_projection_global_getref(lat_0, lon_0)) {
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return -1;
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}
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if (alt_0 != nullptr) {
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*alt_0 = gl_ref.alt;
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}
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return 0;
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}
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float get_distance_to_next_waypoint(double lat_now, double lon_now, double lat_next, double lon_next)
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{
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double lat_now_rad = lat_now / (double)180.0 * M_PI;
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double lon_now_rad = lon_now / (double)180.0 * M_PI;
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double lat_next_rad = lat_next / (double)180.0 * M_PI;
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double lon_next_rad = lon_next / (double)180.0 * M_PI;
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double d_lat = lat_next_rad - lat_now_rad;
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double d_lon = lon_next_rad - lon_now_rad;
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double a = sin(d_lat / (double)2.0) * sin(d_lat / (double)2.0) + sin(d_lon / (double)2.0) * sin(d_lon /
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(double)2.0) * cos(lat_now_rad) * cos(lat_next_rad);
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double c = (double)2.0 * atan2(sqrt(a), sqrt((double)1.0 - a));
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return CONSTANTS_RADIUS_OF_EARTH * c;
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}
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void create_waypoint_from_line_and_dist(double lat_A, double lon_A, double lat_B, double lon_B, float dist,
|
|
double *lat_target, double *lon_target)
|
|
{
|
|
if (fabsf(dist) < FLT_EPSILON) {
|
|
*lat_target = lat_A;
|
|
*lon_target = lon_A;
|
|
|
|
} else if (dist >= FLT_EPSILON) {
|
|
float heading = get_bearing_to_next_waypoint(lat_A, lon_A, lat_B, lon_B);
|
|
waypoint_from_heading_and_distance(lat_A, lon_A, heading, dist, lat_target, lon_target);
|
|
|
|
} else {
|
|
float heading = get_bearing_to_next_waypoint(lat_A, lon_A, lat_B, lon_B);
|
|
heading = _wrap_2pi(heading + M_PI_F);
|
|
waypoint_from_heading_and_distance(lat_A, lon_A, heading, dist, lat_target, lon_target);
|
|
}
|
|
}
|
|
|
|
void waypoint_from_heading_and_distance(double lat_start, double lon_start, float bearing, float dist,
|
|
double *lat_target, double *lon_target)
|
|
{
|
|
bearing = _wrap_2pi(bearing);
|
|
double radius_ratio = (double)(fabs(dist) / CONSTANTS_RADIUS_OF_EARTH);
|
|
|
|
double lat_start_rad = lat_start * M_DEG_TO_RAD;
|
|
double lon_start_rad = lon_start * M_DEG_TO_RAD;
|
|
|
|
*lat_target = asin(sin(lat_start_rad) * cos(radius_ratio) + cos(lat_start_rad) * sin(radius_ratio) * cos((
|
|
double)bearing));
|
|
*lon_target = lon_start_rad + atan2(sin((double)bearing) * sin(radius_ratio) * cos(lat_start_rad),
|
|
cos(radius_ratio) - sin(lat_start_rad) * sin(*lat_target));
|
|
|
|
*lat_target *= M_RAD_TO_DEG;
|
|
*lon_target *= M_RAD_TO_DEG;
|
|
}
|
|
float get_bearing_to_next_waypoint(double lat_now, double lon_now, double lat_next, double lon_next)
|
|
{
|
|
double lat_now_rad = lat_now * M_DEG_TO_RAD;
|
|
double lon_now_rad = lon_now * M_DEG_TO_RAD;
|
|
double lat_next_rad = lat_next * M_DEG_TO_RAD;
|
|
double lon_next_rad = lon_next * M_DEG_TO_RAD;
|
|
|
|
double d_lon = lon_next_rad - lon_now_rad;
|
|
|
|
/* conscious mix of double and float trig function to maximize speed and efficiency */
|
|
float theta = atan2f(sin(d_lon) * cos(lat_next_rad),
|
|
cos(lat_now_rad) * sin(lat_next_rad) - sin(lat_now_rad) * cos(lat_next_rad) * cos(d_lon));
|
|
|
|
theta = _wrap_pi(theta);
|
|
|
|
return theta;
|
|
}
|
|
|
|
void get_vector_to_next_waypoint(double lat_now, double lon_now, double lat_next, double lon_next, float *v_n,
|
|
float *v_e)
|
|
{
|
|
double lat_now_rad = lat_now * M_DEG_TO_RAD;
|
|
double lon_now_rad = lon_now * M_DEG_TO_RAD;
|
|
double lat_next_rad = lat_next * M_DEG_TO_RAD;
|
|
double lon_next_rad = lon_next * M_DEG_TO_RAD;
|
|
|
|
double d_lon = lon_next_rad - lon_now_rad;
|
|
|
|
/* conscious mix of double and float trig function to maximize speed and efficiency */
|
|
*v_n = CONSTANTS_RADIUS_OF_EARTH * (cos(lat_now_rad) * sin(lat_next_rad) - sin(lat_now_rad) * cos(lat_next_rad) * cos(
|
|
d_lon));
|
|
*v_e = CONSTANTS_RADIUS_OF_EARTH * sin(d_lon) * cos(lat_next_rad);
|
|
}
|
|
|
|
void get_vector_to_next_waypoint_fast(double lat_now, double lon_now, double lat_next, double lon_next,
|
|
float *v_n, float *v_e)
|
|
{
|
|
double lat_now_rad = lat_now * M_DEG_TO_RAD;
|
|
double lon_now_rad = lon_now * M_DEG_TO_RAD;
|
|
double lat_next_rad = lat_next * M_DEG_TO_RAD;
|
|
double lon_next_rad = lon_next * M_DEG_TO_RAD;
|
|
|
|
double d_lat = lat_next_rad - lat_now_rad;
|
|
double d_lon = lon_next_rad - lon_now_rad;
|
|
|
|
/* conscious mix of double and float trig function to maximize speed and efficiency */
|
|
*v_n = CONSTANTS_RADIUS_OF_EARTH * d_lat;
|
|
*v_e = CONSTANTS_RADIUS_OF_EARTH * d_lon * cos(lat_now_rad);
|
|
}
|
|
|
|
void add_vector_to_global_position(double lat_now, double lon_now, float v_n, float v_e, double *lat_res,
|
|
double *lon_res)
|
|
{
|
|
double lat_now_rad = lat_now * M_DEG_TO_RAD;
|
|
double lon_now_rad = lon_now * M_DEG_TO_RAD;
|
|
|
|
*lat_res = (lat_now_rad + (double)v_n / CONSTANTS_RADIUS_OF_EARTH) * M_RAD_TO_DEG;
|
|
*lon_res = (lon_now_rad + (double)v_e / (CONSTANTS_RADIUS_OF_EARTH * cos(lat_now_rad))) * M_RAD_TO_DEG;
|
|
}
|
|
|
|
// Additional functions - @author Doug Weibel <douglas.weibel@colorado.edu>
|
|
|
|
int get_distance_to_line(struct crosstrack_error_s *crosstrack_error, double lat_now, double lon_now,
|
|
double lat_start, double lon_start, double lat_end, double lon_end)
|
|
{
|
|
// This function returns the distance to the nearest point on the track line. Distance is positive if current
|
|
// position is right of the track and negative if left of the track as seen from a point on the track line
|
|
// headed towards the end point.
|
|
|
|
float dist_to_end;
|
|
float bearing_end;
|
|
float bearing_track;
|
|
float bearing_diff;
|
|
|
|
int return_value = ERROR; // Set error flag, cleared when valid result calculated.
|
|
crosstrack_error->past_end = false;
|
|
crosstrack_error->distance = 0.0f;
|
|
crosstrack_error->bearing = 0.0f;
|
|
|
|
dist_to_end = get_distance_to_next_waypoint(lat_now, lon_now, lat_end, lon_end);
|
|
|
|
// Return error if arguments are bad
|
|
if (dist_to_end < 0.1f) {
|
|
return ERROR;
|
|
}
|
|
|
|
bearing_end = get_bearing_to_next_waypoint(lat_now, lon_now, lat_end, lon_end);
|
|
bearing_track = get_bearing_to_next_waypoint(lat_start, lon_start, lat_end, lon_end);
|
|
bearing_diff = bearing_track - bearing_end;
|
|
bearing_diff = _wrap_pi(bearing_diff);
|
|
|
|
// Return past_end = true if past end point of line
|
|
if (bearing_diff > M_PI_2_F || bearing_diff < -M_PI_2_F) {
|
|
crosstrack_error->past_end = true;
|
|
return_value = OK;
|
|
return return_value;
|
|
}
|
|
|
|
crosstrack_error->distance = (dist_to_end) * sinf(bearing_diff);
|
|
|
|
if (sin(bearing_diff) >= 0) {
|
|
crosstrack_error->bearing = _wrap_pi(bearing_track - M_PI_2_F);
|
|
|
|
} else {
|
|
crosstrack_error->bearing = _wrap_pi(bearing_track + M_PI_2_F);
|
|
}
|
|
|
|
return_value = OK;
|
|
|
|
return return_value;
|
|
|
|
}
|
|
|
|
|
|
int get_distance_to_arc(struct crosstrack_error_s *crosstrack_error, double lat_now, double lon_now,
|
|
double lat_center, double lon_center,
|
|
float radius, float arc_start_bearing, float arc_sweep)
|
|
{
|
|
// This function returns the distance to the nearest point on the track arc. Distance is positive if current
|
|
// position is right of the arc and negative if left of the arc as seen from the closest point on the arc and
|
|
// headed towards the end point.
|
|
|
|
// Determine if the current position is inside or outside the sector between the line from the center
|
|
// to the arc start and the line from the center to the arc end
|
|
float bearing_sector_start;
|
|
float bearing_sector_end;
|
|
float bearing_now = get_bearing_to_next_waypoint(lat_now, lon_now, lat_center, lon_center);
|
|
bool in_sector;
|
|
|
|
int return_value = ERROR; // Set error flag, cleared when valid result calculated.
|
|
crosstrack_error->past_end = false;
|
|
crosstrack_error->distance = 0.0f;
|
|
crosstrack_error->bearing = 0.0f;
|
|
|
|
// Return error if arguments are bad
|
|
if (radius < 0.1f) { return return_value; }
|
|
|
|
|
|
if (arc_sweep >= 0.0f) {
|
|
bearing_sector_start = arc_start_bearing;
|
|
bearing_sector_end = arc_start_bearing + arc_sweep;
|
|
|
|
if (bearing_sector_end > 2.0f * M_PI_F) { bearing_sector_end -= M_TWOPI_F; }
|
|
|
|
} else {
|
|
bearing_sector_end = arc_start_bearing;
|
|
bearing_sector_start = arc_start_bearing - arc_sweep;
|
|
|
|
if (bearing_sector_start < 0.0f) { bearing_sector_start += M_TWOPI_F; }
|
|
}
|
|
|
|
in_sector = false;
|
|
|
|
// Case where sector does not span zero
|
|
if (bearing_sector_end >= bearing_sector_start && bearing_now >= bearing_sector_start
|
|
&& bearing_now <= bearing_sector_end) { in_sector = true; }
|
|
|
|
// Case where sector does span zero
|
|
if (bearing_sector_end < bearing_sector_start && (bearing_now > bearing_sector_start
|
|
|| bearing_now < bearing_sector_end)) { in_sector = true; }
|
|
|
|
// If in the sector then calculate distance and bearing to closest point
|
|
if (in_sector) {
|
|
crosstrack_error->past_end = false;
|
|
float dist_to_center = get_distance_to_next_waypoint(lat_now, lon_now, lat_center, lon_center);
|
|
|
|
if (dist_to_center <= radius) {
|
|
crosstrack_error->distance = radius - dist_to_center;
|
|
crosstrack_error->bearing = bearing_now + M_PI_F;
|
|
|
|
} else {
|
|
crosstrack_error->distance = dist_to_center - radius;
|
|
crosstrack_error->bearing = bearing_now;
|
|
}
|
|
|
|
// If out of the sector then calculate dist and bearing to start or end point
|
|
|
|
} else {
|
|
|
|
// Use the approximation that 111,111 meters in the y direction is 1 degree (of latitude)
|
|
// and 111,111 * cos(latitude) meters in the x direction is 1 degree (of longitude) to
|
|
// calculate the position of the start and end points. We should not be doing this often
|
|
// as this function generally will not be called repeatedly when we are out of the sector.
|
|
|
|
double start_disp_x = (double)radius * sin(arc_start_bearing);
|
|
double start_disp_y = (double)radius * cos(arc_start_bearing);
|
|
double end_disp_x = (double)radius * sin(_wrap_pi((double)(arc_start_bearing + arc_sweep)));
|
|
double end_disp_y = (double)radius * cos(_wrap_pi((double)(arc_start_bearing + arc_sweep)));
|
|
double lon_start = lon_now + start_disp_x / 111111.0;
|
|
double lat_start = lat_now + start_disp_y * cos(lat_now) / 111111.0;
|
|
double lon_end = lon_now + end_disp_x / 111111.0;
|
|
double lat_end = lat_now + end_disp_y * cos(lat_now) / 111111.0;
|
|
double dist_to_start = get_distance_to_next_waypoint(lat_now, lon_now, lat_start, lon_start);
|
|
double dist_to_end = get_distance_to_next_waypoint(lat_now, lon_now, lat_end, lon_end);
|
|
|
|
|
|
if (dist_to_start < dist_to_end) {
|
|
crosstrack_error->distance = dist_to_start;
|
|
crosstrack_error->bearing = get_bearing_to_next_waypoint(lat_now, lon_now, lat_start, lon_start);
|
|
|
|
} else {
|
|
crosstrack_error->past_end = true;
|
|
crosstrack_error->distance = dist_to_end;
|
|
crosstrack_error->bearing = get_bearing_to_next_waypoint(lat_now, lon_now, lat_end, lon_end);
|
|
}
|
|
|
|
}
|
|
|
|
crosstrack_error->bearing = _wrap_pi((double)crosstrack_error->bearing);
|
|
return_value = OK;
|
|
return return_value;
|
|
}
|
|
|
|
float get_distance_to_point_global_wgs84(double lat_now, double lon_now, float alt_now,
|
|
double lat_next, double lon_next, float alt_next,
|
|
float *dist_xy, float *dist_z)
|
|
{
|
|
double current_x_rad = lat_next / 180.0 * M_PI;
|
|
double current_y_rad = lon_next / 180.0 * M_PI;
|
|
double x_rad = lat_now / 180.0 * M_PI;
|
|
double y_rad = lon_now / 180.0 * M_PI;
|
|
|
|
double d_lat = x_rad - current_x_rad;
|
|
double d_lon = y_rad - current_y_rad;
|
|
|
|
double a = sin(d_lat / 2.0) * sin(d_lat / 2.0) + sin(d_lon / 2.0) * sin(d_lon / 2.0) * cos(current_x_rad) * cos(x_rad);
|
|
double c = 2 * atan2(sqrt(a), sqrt(1 - a));
|
|
|
|
float dxy = CONSTANTS_RADIUS_OF_EARTH * c;
|
|
float dz = alt_now - alt_next;
|
|
|
|
*dist_xy = fabsf(dxy);
|
|
*dist_z = fabsf(dz);
|
|
|
|
return sqrtf(dxy * dxy + dz * dz);
|
|
}
|
|
|
|
|
|
float mavlink_wpm_distance_to_point_local(float x_now, float y_now, float z_now,
|
|
float x_next, float y_next, float z_next,
|
|
float *dist_xy, float *dist_z)
|
|
{
|
|
float dx = x_now - x_next;
|
|
float dy = y_now - y_next;
|
|
float dz = z_now - z_next;
|
|
|
|
*dist_xy = sqrtf(dx * dx + dy * dy);
|
|
*dist_z = fabsf(dz);
|
|
|
|
return sqrtf(dx * dx + dy * dy + dz * dz);
|
|
}
|
|
|
|
float _wrap_pi(float bearing)
|
|
{
|
|
/* value is inf or NaN */
|
|
if (!ISFINITE(bearing)) {
|
|
return bearing;
|
|
}
|
|
|
|
int c = 0;
|
|
|
|
while (bearing >= M_PI_F) {
|
|
bearing -= M_TWOPI_F;
|
|
|
|
if (c++ > 3) {
|
|
return NAN;
|
|
}
|
|
}
|
|
|
|
c = 0;
|
|
|
|
while (bearing < -M_PI_F) {
|
|
bearing += M_TWOPI_F;
|
|
|
|
if (c++ > 3) {
|
|
return NAN;
|
|
}
|
|
}
|
|
|
|
return bearing;
|
|
}
|
|
|
|
float _wrap_2pi(float bearing)
|
|
{
|
|
/* value is inf or NaN */
|
|
if (!ISFINITE(bearing)) {
|
|
return bearing;
|
|
}
|
|
|
|
int c = 0;
|
|
|
|
while (bearing >= M_TWOPI_F) {
|
|
bearing -= M_TWOPI_F;
|
|
|
|
if (c++ > 3) {
|
|
return NAN;
|
|
}
|
|
}
|
|
|
|
c = 0;
|
|
|
|
while (bearing < 0.0f) {
|
|
bearing += M_TWOPI_F;
|
|
|
|
if (c++ > 3) {
|
|
return NAN;
|
|
}
|
|
}
|
|
|
|
return bearing;
|
|
}
|
|
|
|
float _wrap_180(float bearing)
|
|
{
|
|
/* value is inf or NaN */
|
|
if (!ISFINITE(bearing)) {
|
|
return bearing;
|
|
}
|
|
|
|
int c = 0;
|
|
|
|
while (bearing >= 180.0f) {
|
|
bearing -= 360.0f;
|
|
|
|
if (c++ > 3) {
|
|
return NAN;
|
|
}
|
|
}
|
|
|
|
c = 0;
|
|
|
|
while (bearing < -180.0f) {
|
|
bearing += 360.0f;
|
|
|
|
if (c++ > 3) {
|
|
return NAN;
|
|
}
|
|
}
|
|
|
|
return bearing;
|
|
}
|
|
|
|
float _wrap_360(float bearing)
|
|
{
|
|
/* value is inf or NaN */
|
|
if (!ISFINITE(bearing)) {
|
|
return bearing;
|
|
}
|
|
|
|
int c = 0;
|
|
|
|
while (bearing >= 360.0f) {
|
|
bearing -= 360.0f;
|
|
|
|
if (c++ > 3) {
|
|
return NAN;
|
|
}
|
|
}
|
|
|
|
c = 0;
|
|
|
|
while (bearing < 0.0f) {
|
|
bearing += 360.0f;
|
|
|
|
if (c++ > 3) {
|
|
return NAN;
|
|
}
|
|
}
|
|
|
|
return bearing;
|
|
}
|
|
#endif //POSIX_SHARED
|