mirror of https://github.com/ArduPilot/ardupilot
AP_Math: split out double precision location functions
this allows ALLOW_DOUBLE_MATH_FUNCTIONS to be used
This commit is contained in:
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a575608110
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61c8dfac31
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@ -2,6 +2,8 @@
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// Unit tests for the AP_Math polygon code
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//
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#define ALLOW_DOUBLE_MATH_FUNCTIONS
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#include <AP_HAL/AP_HAL.h>
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#include <AP_Math/AP_Math.h>
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@ -211,113 +211,6 @@ void print_latlon(AP_HAL::BetterStream *s, int32_t lat_or_lon)
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s->printf("%ld.%07ld",(long)dec_portion,(long)frac_portion);
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}
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#ifdef ALLOW_DOUBLE_MATH_FUNCTIONS
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/*
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these are not currently used. They should be moved to location_double.cpp if we do enable them in the future
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*/
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void wgsllh2ecef(const Vector3d &llh, Vector3d &ecef) {
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double d = WGS84_E * sin(llh[0]);
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double N = WGS84_A / sqrt(1 - d*d);
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ecef[0] = (N + llh[2]) * cos(llh[0]) * cos(llh[1]);
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ecef[1] = (N + llh[2]) * cos(llh[0]) * sin(llh[1]);
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ecef[2] = ((1 - WGS84_E*WGS84_E)*N + llh[2]) * sin(llh[0]);
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}
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void wgsecef2llh(const Vector3d &ecef, Vector3d &llh) {
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/* Distance from polar axis. */
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const double p = sqrt(ecef[0]*ecef[0] + ecef[1]*ecef[1]);
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/* Compute longitude first, this can be done exactly. */
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if (!is_zero(p))
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llh[1] = atan2(ecef[1], ecef[0]);
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else
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llh[1] = 0;
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/* If we are close to the pole then convergence is very slow, treat this is a
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* special case. */
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if (p < WGS84_A * double(1e-16)) {
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llh[0] = copysign(M_PI_2, ecef[2]);
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llh[2] = fabs(ecef[2]) - WGS84_B;
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return;
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}
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/* Calculate some other constants as defined in the Fukushima paper. */
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const double P = p / WGS84_A;
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const double e_c = sqrt(1 - WGS84_E*WGS84_E);
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const double Z = fabs(ecef[2]) * e_c / WGS84_A;
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/* Initial values for S and C correspond to a zero height solution. */
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double S = Z;
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double C = e_c * P;
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/* Neither S nor C can be negative on the first iteration so
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* starting prev = -1 will not cause and early exit. */
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double prev_C = -1;
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double prev_S = -1;
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double A_n, B_n, D_n, F_n;
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/* Iterate a maximum of 10 times. This should be way more than enough for all
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* sane inputs */
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for (int i=0; i<10; i++)
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{
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/* Calculate some intermmediate variables used in the update step based on
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* the current state. */
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A_n = sqrt(S*S + C*C);
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D_n = Z*A_n*A_n*A_n + WGS84_E*WGS84_E*S*S*S;
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F_n = P*A_n*A_n*A_n - WGS84_E*WGS84_E*C*C*C;
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B_n = double(1.5) * WGS84_E*S*C*C*(A_n*(P*S - Z*C) - WGS84_E*S*C);
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/* Update step. */
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S = D_n*F_n - B_n*S;
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C = F_n*F_n - B_n*C;
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/* The original algorithm as presented in the paper by Fukushima has a
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* problem with numerical stability. S and C can grow very large or small
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* and over or underflow a double. In the paper this is acknowledged and
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* the proposed resolution is to non-dimensionalise the equations for S and
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* C. However, this does not completely solve the problem. The author caps
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* the solution to only a couple of iterations and in this period over or
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* underflow is unlikely but as we require a bit more precision and hence
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* more iterations so this is still a concern for us.
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*
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* As the only thing that is important is the ratio T = S/C, my solution is
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* to divide both S and C by either S or C. The scaling is chosen such that
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* one of S or C is scaled to unity whilst the other is scaled to a value
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* less than one. By dividing by the larger of S or C we ensure that we do
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* not divide by zero as only one of S or C should ever be zero.
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*
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* This incurs an extra division each iteration which the author was
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* explicityl trying to avoid and it may be that this solution is just
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* reverting back to the method of iterating on T directly, perhaps this
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* bears more thought?
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*/
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if (S > C) {
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C = C / S;
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S = 1;
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} else {
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S = S / C;
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C = 1;
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}
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/* Check for convergence and exit early if we have converged. */
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if (fabs(S - prev_S) < double(1e-16) && fabs(C - prev_C) < double(1e-16)) {
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break;
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} else {
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prev_S = S;
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prev_C = C;
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}
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}
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A_n = sqrt(S*S + C*C);
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llh[0] = copysign(1.0, ecef[2]) * atan(S / (e_c*C));
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llh[2] = (p*e_c*C + fabs(ecef[2])*S - WGS84_A*e_c*A_n) / sqrt(e_c*e_c*C*C + S*S);
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}
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#endif // ALLOW_DOUBLE_MATH_FUNCTIONS
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// return true when lat and lng are within range
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bool check_lat(float lat)
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{
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@ -0,0 +1,132 @@
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/*
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* location_double.cpp
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*
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* This file is free software: you can redistribute it and/or modify it
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* under the terms of the GNU General Public License as published by the
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* Free Software Foundation, either version 3 of the License, or
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* (at your option) any later version.
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*
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* This file is distributed in the hope that it will be useful, but
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* WITHOUT ANY WARRANTY; without even the implied warranty of
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* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE.
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* See the GNU General Public License for more details.
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*
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* You should have received a copy of the GNU General Public License along
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* with this program. If not, see <http://www.gnu.org/licenses/>.
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*/
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/*
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this is for double precision functions related to the location structure
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*/
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#define ALLOW_DOUBLE_MATH_FUNCTIONS
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#include <AP_HAL/AP_HAL.h>
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#include <stdlib.h>
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#include "AP_Math.h"
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#include "location.h"
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/*
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these are not currently used. They should be moved to location_double.cpp if we do enable them in the future
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*/
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void wgsllh2ecef(const Vector3d &llh, Vector3d &ecef) {
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double d = WGS84_E * sin(llh[0]);
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double N = WGS84_A / sqrt(1 - d*d);
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ecef[0] = (N + llh[2]) * cos(llh[0]) * cos(llh[1]);
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ecef[1] = (N + llh[2]) * cos(llh[0]) * sin(llh[1]);
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ecef[2] = ((1 - WGS84_E*WGS84_E)*N + llh[2]) * sin(llh[0]);
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}
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void wgsecef2llh(const Vector3d &ecef, Vector3d &llh) {
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/* Distance from polar axis. */
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const double p = sqrt(ecef[0]*ecef[0] + ecef[1]*ecef[1]);
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/* Compute longitude first, this can be done exactly. */
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if (!is_zero(p))
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llh[1] = atan2(ecef[1], ecef[0]);
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else
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llh[1] = 0;
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/* If we are close to the pole then convergence is very slow, treat this is a
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* special case. */
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if (p < WGS84_A * double(1e-16)) {
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llh[0] = copysign(M_PI_2, ecef[2]);
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llh[2] = fabs(ecef[2]) - WGS84_B;
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return;
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}
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/* Calculate some other constants as defined in the Fukushima paper. */
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const double P = p / WGS84_A;
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const double e_c = sqrt(1 - WGS84_E*WGS84_E);
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const double Z = fabs(ecef[2]) * e_c / WGS84_A;
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/* Initial values for S and C correspond to a zero height solution. */
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double S = Z;
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double C = e_c * P;
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/* Neither S nor C can be negative on the first iteration so
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* starting prev = -1 will not cause and early exit. */
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double prev_C = -1;
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double prev_S = -1;
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double A_n, B_n, D_n, F_n;
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/* Iterate a maximum of 10 times. This should be way more than enough for all
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* sane inputs */
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for (int i=0; i<10; i++)
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{
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/* Calculate some intermmediate variables used in the update step based on
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* the current state. */
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A_n = sqrt(S*S + C*C);
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D_n = Z*A_n*A_n*A_n + WGS84_E*WGS84_E*S*S*S;
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F_n = P*A_n*A_n*A_n - WGS84_E*WGS84_E*C*C*C;
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B_n = double(1.5) * WGS84_E*S*C*C*(A_n*(P*S - Z*C) - WGS84_E*S*C);
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/* Update step. */
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S = D_n*F_n - B_n*S;
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C = F_n*F_n - B_n*C;
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/* The original algorithm as presented in the paper by Fukushima has a
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* problem with numerical stability. S and C can grow very large or small
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* and over or underflow a double. In the paper this is acknowledged and
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* the proposed resolution is to non-dimensionalise the equations for S and
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* C. However, this does not completely solve the problem. The author caps
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* the solution to only a couple of iterations and in this period over or
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* underflow is unlikely but as we require a bit more precision and hence
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* more iterations so this is still a concern for us.
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*
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* As the only thing that is important is the ratio T = S/C, my solution is
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* to divide both S and C by either S or C. The scaling is chosen such that
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* one of S or C is scaled to unity whilst the other is scaled to a value
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* less than one. By dividing by the larger of S or C we ensure that we do
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* not divide by zero as only one of S or C should ever be zero.
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*
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* This incurs an extra division each iteration which the author was
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* explicityl trying to avoid and it may be that this solution is just
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* reverting back to the method of iterating on T directly, perhaps this
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* bears more thought?
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*/
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if (S > C) {
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C = C / S;
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S = 1;
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} else {
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S = S / C;
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C = 1;
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}
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/* Check for convergence and exit early if we have converged. */
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if (fabs(S - prev_S) < double(1e-16) && fabs(C - prev_C) < double(1e-16)) {
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break;
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} else {
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prev_S = S;
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prev_C = C;
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}
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}
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A_n = sqrt(S*S + C*C);
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llh[0] = copysign(1.0, ecef[2]) * atan(S / (e_c*C));
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llh[2] = (p*e_c*C + fabs(ecef[2])*S - WGS84_A*e_c*A_n) / sqrt(e_c*e_c*C*C + S*S);
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}
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