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navego_plot.m
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navego_plot.m
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function navego_plot (ref, gnss, nav_e, gnss_ref, nav_ref, ref_g, ref_n)
% navego_plot: plots results from INS/GNSS integration dataset.
%
% INPUT:
% ref, reference dataset.
% gnss, GNSS dataset.
% nav_e, INS/GNSS integration dataset.
% gnss_ref, GNSS dataset interpolated by reference time vector.
% nav_ref, INS/GNSS dataset interpolated by reference time vector.
% ref_n, reference dataset adjusted by INS/GNSS interpolation.
% ref_g, reference dataset interpolated by GNSS interpolation.
%
% OUTPUT
% several figures.
%
% Copyright (C) 2014, Rodrigo Gonzalez, all rights reserved.
%
% This file is part of NaveGo, an open-source MATLAB toolbox for
% simulation of integrated navigation systems.
%
% NaveGo is free software: you can redistribute it and/or modify
% it under the terms of the GNU Lesser General Public License (LGPL)
% version 3 as published by the Free Software Foundation.
%
% This program is distributed in the hope that it will be useful,
% but WITHOUT ANY WARRANTY; without even the implied warranty of
% MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
% GNU Lesser General Public License for more details.
%
% You should have received a copy of the GNU Lesser General Public
% License along with this program. If not, see
% <http://www.gnu.org/licenses/>.
%
% Version: 008
% Date: 2019/01/14
% Author: Rodrigo Gonzalez <[email protected]>
% URL: https://github.com/rodralez/navego
% D2R = (pi/180); % degrees to radians
R2D = (180/pi); % radians to degrees
% Standard deviation * 3 vector from navigation estimates
sig3_v = abs(nav_e.Pp(:, 1:16:end).^(0.5)) .* 3; % Only take diagonal elements from Pp
% TRAJECTORY
figure;
plot3(ref_n.lon.*R2D, ref_n.lat.*R2D, ref_n.h, '--k')
hold on
plot3(nav_ref.lon.*R2D, nav_ref.lat.*R2D, nav_ref.h, '-.b')
plot3(ref_n.lon(1).*R2D, ref_n.lat(1).*R2D, ref_n.h(1), 'or', 'MarkerSize', 10, 'LineWidth', 2)
axis tight
title('TRAJECTORY')
xlabel('Longitude [deg]')
ylabel('Latitude [deg]')
zlabel('Altitude [m]')
view(0, 90)
legend('REF', 'INS/GNSS', 'Location','best');
grid
% ATTITUDE
figure;
subplot(311)
plot(ref.t, R2D.*ref.roll, '--k', nav_e.t, R2D.*nav_e.roll,'-.b');
ylabel('[deg]')
xlabel('Time [s]')
legend('REF', 'INS/GNSS');
title('ROLL');
grid
subplot(312)
plot(ref.t, R2D.*ref.pitch, '--k', nav_e.t, R2D.*nav_e.pitch,'-.b');
ylabel('[deg]')
xlabel('Time [s]')
legend('REF', 'INS/GNSS')
title('PITCH');
grid
subplot(313)
plot(ref.t, R2D.* ref.yaw, '--k', nav_e.t, R2D.*nav_e.yaw,'-.b');
ylabel('[deg]')
xlabel('Time [s]')
legend('REF', 'INS/GNSS')
title('YAW');
grid
% ATTITUDE ERRORS
figure;
subplot(311)
plot(nav_ref.t, (nav_ref.roll - ref_n.roll).*R2D, '-.b' );
hold on
plot (nav_e.tg, R2D.*sig3_v(:,1), '--k', nav_e.tg, -R2D.*sig3_v(:,1), '--k' )
ylabel('[deg]')
xlabel('Time [s]')
legend('INS/GNSS', '3\sigma');
title('ROLL ERROR');
grid
subplot(312)
plot(nav_ref.t, (nav_ref.pitch - ref_n.pitch).*R2D, '-.b' );
hold on
plot (nav_e.tg, R2D.*sig3_v(:,2), '--k', nav_e.tg, -R2D.*sig3_v(:,2), '--k' )
ylabel('[deg]')
xlabel('Time [s]')
legend('INS/GNSS', '3\sigma');
title('PITCH ERROR');
grid
subplot(313)
yaw_err = correct_yaw(nav_ref.yaw - ref_n.yaw);
plot(nav_ref.t, yaw_err.*R2D, '-.b' );
hold on
plot (nav_e.tg, R2D.*sig3_v(:,3), '--k', nav_e.tg, -R2D.*sig3_v(:,3), '--k' )
ylabel('[deg]')
xlabel('Time [s]')
legend('INS/GNSS', '3\sigma');
title('YAW ERROR');
grid
% VELOCITIES
figure;
subplot(311)
plot(ref.t, ref.vel(:,1), '--k', gnss.t, gnss.vel(:,1),'-c', nav_e.t, nav_e.vel(:,1),'-.b' );
xlabel('Time [s]')
ylabel('[m/s]')
legend('REF', 'GNSS', 'INS/GNSS');
title('NORTH VELOCITY');
grid
subplot(312)
plot(ref.t, ref.vel(:,2), '--k', gnss.t, gnss.vel(:,2),'-c', nav_e.t, nav_e.vel(:,2),'-.b' );
xlabel('Time [s]')
ylabel('[m/s]')
legend('REF', 'GNSS', 'INS/GNSS');
title('EAST VELOCITY');
grid
subplot(313)
plot(ref.t, ref.vel(:,3), '--k', gnss.t, gnss.vel(:,3),'-c', nav_e.t, nav_e.vel(:,3),'-.b' );
xlabel('Time [s]')
ylabel('[m/s]')
legend('REF', 'GNSS', 'INS/GNSS');
title('DOWN VELOCITY');
grid
% VELOCITIES ERRORS
figure;
subplot(311)
plot(gnss_ref.t, (gnss_ref.vel(:,1) - ref_g.vel(:,1)), '-c');
hold on
plot(nav_ref.t, (nav_ref.vel(:,1) - ref_n.vel(:,1)), '-.b' );
plot (nav_e.tg, sig3_v(:,4), '--k', nav_e.tg, -sig3_v(:,4), '--k' )
xlabel('Time [s]')
ylabel('[m/s]')
legend('GNSS', 'INS/GNSS', '3\sigma');
title('VELOCITY NORTH ERROR');
grid
subplot(312)
plot(gnss_ref.t, (gnss_ref.vel(:,2) - ref_g.vel(:,2)), '-c');
hold on
plot(nav_ref.t, (nav_ref.vel(:,2) - ref_n.vel(:,2)), '-.b' );
plot (nav_e.tg, sig3_v(:,5), '--k', nav_e.tg, -sig3_v(:,5), '--k' )
xlabel('Time [s]')
ylabel('[m/s]')
legend('GNSS', 'INS/GNSS', '3\sigma');
title('VELOCITY EAST ERROR');
grid
subplot(313)
plot(gnss_ref.t, (gnss_ref.vel(:,3) - ref_g.vel(:,3)), '-c');
hold on
plot(nav_ref.t, (nav_ref.vel(:,3) - ref_n.vel(:,3)), '-.b' );
plot (nav_e.tg, sig3_v(:,6), '--k', nav_e.tg, -sig3_v(:,6), '--k' )
xlabel('Time [s]')
ylabel('[m/s]')
legend('GNSS', 'INS/GNSS', '3\sigma');
title('VELOCITY DOWN ERROR');
grid
% POSITION
figure;
subplot(311)
plot(ref.t, ref.lat .*R2D, '--k', gnss.t, gnss.lat.*R2D, '-c', nav_e.t, nav_e.lat.*R2D, '-.b');
xlabel('Time [s]')
ylabel('[deg]')
legend('REF', 'GNSS', 'INS/GNSS' );
title('LATITUDE');
grid
subplot(312)
plot(ref.t, ref.lon .*R2D, '--k', gnss.t, gnss.lon.*R2D, '-c', nav_e.t, nav_e.lon.*R2D, '-.b');
xlabel('Time [s]')
ylabel('[deg]')
legend('REF', 'GNSS', 'INS/GNSS' );
title('LONGITUDE');
grid
subplot(313)
plot(ref.t, ref.h, '--k', gnss.t, gnss.h, '-c', nav_e.t, nav_e.h, '-.b')
xlabel('Time [s]')
ylabel('[m]')
legend('REF', 'GNSS', 'INS/GNSS');
title('ALTITUDE');
grid
% POSITION ERRORS
[RN,RE] = radius(nav_ref.lat);
LAT2M_1 = RN + nav_ref.h;
LON2M_1 = (RE + nav_ref.h).*cos(nav_ref.lat);
[RN,RE] = radius(gnss.lat);
LAT2M_G = RN + gnss.h;
LON2M_G = (RE + gnss.h).*cos(gnss.lat);
[RN,RE] = radius(gnss_ref.lat);
LAT2M_GR = RN + gnss_ref.h;
LON2M_GR = (RE + gnss_ref.h).*cos(gnss_ref.lat);
figure;
subplot(311)
plot(gnss_ref.t, LAT2M_GR.*(gnss_ref.lat - ref_g.lat), '-c')
hold on
plot(nav_ref.t, LAT2M_1.*(nav_ref.lat - ref_n.lat), '-.b')
plot (nav_e.tg, LAT2M_G.*sig3_v(:,7), '--k', nav_e.tg, -LAT2M_G.*sig3_v(:,7), '--k' )
xlabel('Time [s]')
ylabel('[m]')
legend('GNSS', 'INS/GNSS', '3\sigma');
title('LATITUDE ERROR');
grid
subplot(312)
plot(gnss_ref.t, LON2M_GR.*(gnss_ref.lon - ref_g.lon), '-c')
hold on
plot(nav_ref.t, LON2M_1.*(nav_ref.lon - ref_n.lon), '-.b')
plot(nav_e.tg, LON2M_G.*sig3_v(:,8), '--k', nav_e.tg, -LON2M_G.*sig3_v(:,8), '--k' )
xlabel('Time [s]')
ylabel('[m]')
legend('GNSS', 'INS/GNSS', '3\sigma');
title('LONGITUDE ERROR');
grid
subplot(313)
plot(gnss_ref.t, (gnss_ref.h - ref_g.h), '-c')
hold on
plot(nav_ref.t, (nav_ref.h - ref_n.h), '-.b')
plot(nav_e.tg, sig3_v(:,9), '--k', nav_e.tg, -sig3_v(:,9), '--k' )
xlabel('Time [s]')
ylabel('[m]')
legend('GNSS', 'INS/GNSS', '3\sigma');
title('ALTITUDE ERROR');
grid
% BIAS ESTIMATION
figure;
subplot(311)
plot(nav_e.tg, nav_e.b(:, 1).*R2D, '-.b');
xlabel('Time [s]')
ylabel('[deg]')
title('KF BIAS ESTIMATION X');
grid
subplot(312)
plot(nav_e.tg, nav_e.b(:, 2).*R2D, '-.b');
xlabel('Time [s]')
ylabel('[deg]')
title('KF BIAS ESTIMATION Y');
grid
subplot(313)
plot(nav_e.tg, nav_e.b(:, 3).*R2D, '-.b');
xlabel('Time [s]')
ylabel('[deg]')
title('KF BIAS ESTIMATION Z');
grid