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ekf tools: compare gyro integral with attitude estimate
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src/modules/ekf2/EKF/python/tuning_tools/gyro_integration.py
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#!/usr/bin/env python | ||
# -*- coding: utf-8 -*- | ||
""" | ||
Copyright (c) 2024 PX4 Development Team | ||
Redistribution and use in source and binary forms, with or without | ||
modification, are permitted provided that the following conditions | ||
are met: | ||
1. Redistributions of source code must retain the above copyright | ||
notice, this list of conditions and the following disclaimer. | ||
2. Redistributions in binary form must reproduce the above copyright | ||
notice, this list of conditions and the following disclaimer in | ||
the documentation and/or other materials provided with the | ||
distribution. | ||
3. Neither the name PX4 nor the names of its contributors may be | ||
used to endorse or promote products derived from this software | ||
without specific prior written permission. | ||
THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS | ||
"AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT | ||
LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS | ||
FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE | ||
COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, | ||
INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, | ||
BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS | ||
OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED | ||
AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT | ||
LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN | ||
ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE | ||
POSSIBILITY OF SUCH DAMAGE. | ||
""" | ||
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import matplotlib.pylab as plt | ||
from pyulog import ULog | ||
from pyulog.px4 import PX4ULog | ||
import numpy as np | ||
import sym | ||
import symforce.symbolic as sf | ||
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def getAllData(logfile): | ||
log = ULog(logfile) | ||
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gyro = np.matrix([getData(log, 'sensor_combined', 'gyro_rad[0]'), | ||
getData(log, 'sensor_combined', 'gyro_rad[1]'), | ||
getData(log, 'sensor_combined', 'gyro_rad[2]')]) | ||
t_gyro = getTimestampsSeconds(log, 'sensor_combined') | ||
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t_gyro -= t_gyro[0] | ||
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q = np.matrix([getData(log, 'vehicle_attitude', 'q[0]'), | ||
getData(log, 'vehicle_attitude', 'q[1]'), | ||
getData(log, 'vehicle_attitude', 'q[2]'), | ||
getData(log, 'vehicle_attitude', 'q[3]')]) | ||
t_q = getTimestampsSeconds(log, 'vehicle_attitude') | ||
t_q -= t_q[0] | ||
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return (t_gyro, gyro, t_q, q) | ||
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def getData(log, topic_name, variable_name, instance=0): | ||
variable_data = np.array([]) | ||
for elem in log.data_list: | ||
if elem.name == topic_name: | ||
if instance == elem.multi_id: | ||
variable_data = elem.data[variable_name] | ||
break | ||
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return variable_data | ||
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def us2s(time_us): | ||
return time_us * 1e-6 | ||
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def getTimestampsSeconds(log, topic_name, instance=0): | ||
return us2s(getData(log, topic_name, 'timestamp', instance)) | ||
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def integrateAngularRate(t, angular_rate, rot_init=sym.Rot3()): | ||
R = rot_init | ||
roll = [] | ||
pitch = [] | ||
yaw = [] | ||
t_prev = 0 | ||
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for i in range(len(t)): | ||
dt = t[i] - t_prev | ||
R = R * sym.Rot3.from_tangent(angular_rate[:, i] * dt) | ||
att = R.to_yaw_pitch_roll() | ||
yaw = np.append(yaw, att[0]) | ||
pitch = np.append(pitch, att[1]) | ||
roll = np.append(roll, att[2]) | ||
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t_prev = t[i] | ||
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return (roll, pitch, yaw) | ||
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def quat2RollPitchYaw(t, q): | ||
roll = [] | ||
pitch = [] | ||
yaw = [] | ||
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for i in range(len(t)): | ||
vect = sf.V3(float(q[1, i]), float(q[2, i]), float(q[3, i])) | ||
quat = sf.Quaternion(w=q[0, i], xyz=vect) | ||
R = sf.Rot3(quat) | ||
att = R.to_yaw_pitch_roll() | ||
yaw = np.append(yaw, float(att[0].evalf())) | ||
pitch = np.append(pitch, float(att[1].evalf())) | ||
roll = np.append(roll, float(att[2].evalf())) | ||
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return (roll, pitch, yaw) | ||
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def run(logfile): | ||
(t, gyro, t_q, q) = getAllData(logfile) | ||
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(roll, pitch, yaw) = quat2RollPitchYaw(t_q, q) | ||
(roll_raw, pitch_raw, yaw_raw) = integrateAngularRate(t, gyro, rot_init=sym.Rot3.from_yaw_pitch_roll(yaw[0], pitch[0], roll[0])) | ||
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# Plot data | ||
plt.figure(1) | ||
plt.suptitle(logfile.split('/')[-1]) | ||
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ax1 = plt.subplot(3, 1, 1) | ||
ax1.plot(t_q, np.rad2deg(roll), '-') | ||
ax1.plot(t, np.rad2deg(roll_raw), '--') | ||
ax1.set_ylabel("roll (deg)") | ||
ax1.legend(["estimated", "integrated"]) | ||
ax1.grid() | ||
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ax2 = plt.subplot(3, 1, 2, sharex=ax1) | ||
ax2.plot(t_q, np.rad2deg(pitch)) | ||
ax2.plot(t, np.rad2deg(pitch_raw), '--') | ||
ax2.set_ylabel("pitch (deg)") | ||
ax2.legend(["estimated", "integrated"]) | ||
ax2.grid() | ||
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ax3 = plt.subplot(3, 1, 3, sharex=ax1) | ||
ax3.plot(t_q, np.rad2deg(yaw)) | ||
ax3.plot(t, np.rad2deg(yaw_raw), '--') | ||
ax3.set_xlabel("time (s)") | ||
ax3.set_ylabel("yaw (deg)") | ||
ax3.legend(["estimated", "integrated"]) | ||
ax3.grid() | ||
plt.show() | ||
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if __name__ == '__main__': | ||
import os | ||
import argparse | ||
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script_path = os.path.split(os.path.realpath(__file__))[0] | ||
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parser = argparse.ArgumentParser( | ||
description='Integrate angular velocity to attitude and compare it with attitude estimate') | ||
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parser.add_argument('logfile', help='Full ulog file path, name and extension', type=str) | ||
args = parser.parse_args() | ||
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logfile = os.path.abspath(args.logfile) | ||
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run(logfile) |