|
|
|
#!/usr/bin/env python2
|
|
|
|
#***************************************************************************
|
|
|
|
#
|
|
|
|
# Copyright (c) 2015-2016 PX4 Development Team. All rights reserved.
|
|
|
|
#
|
|
|
|
# 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.
|
|
|
|
#
|
|
|
|
#***************************************************************************/
|
|
|
|
|
|
|
|
#
|
|
|
|
# @author Andreas Antener <andreas@uaventure.com>
|
|
|
|
#
|
|
|
|
|
|
|
|
# The shebang of this file is currently Python2 because some
|
|
|
|
# dependencies such as pymavlink don't play well with Python3 yet.
|
|
|
|
|
|
|
|
PKG = 'px4'
|
|
|
|
|
|
|
|
import unittest
|
|
|
|
import rospy
|
|
|
|
import math
|
|
|
|
import rosbag
|
|
|
|
import sys
|
|
|
|
import os
|
|
|
|
import time
|
|
|
|
import glob
|
|
|
|
import json
|
|
|
|
|
|
|
|
import mavros
|
|
|
|
from pymavlink import mavutil
|
|
|
|
from mavros import mavlink
|
|
|
|
|
|
|
|
import px4tools
|
|
|
|
|
|
|
|
from geometry_msgs.msg import PoseStamped
|
|
|
|
from mavros_msgs.srv import CommandLong, WaypointPush
|
|
|
|
from mavros_msgs.msg import Mavlink, Waypoint, ExtendedState
|
|
|
|
from sensor_msgs.msg import NavSatFix
|
|
|
|
from mavros.mission import QGroundControlWP
|
|
|
|
#from px4_test_helper import PX4TestHelper
|
|
|
|
|
|
|
|
def get_last_log():
|
|
|
|
try:
|
|
|
|
log_path = os.environ['PX4_LOG_DIR']
|
|
|
|
except KeyError:
|
|
|
|
log_path = os.path.join(os.environ['HOME'], 'ros/rootfs/fs/microsd/log')
|
|
|
|
last_log_dir = sorted(
|
|
|
|
glob.glob(os.path.join(log_path, '*')))[-1]
|
|
|
|
last_log = sorted(glob.glob(os.path.join(last_log_dir, '*.ulg')))[-1]
|
|
|
|
return last_log
|
|
|
|
|
|
|
|
def read_new_mission(f):
|
|
|
|
d = json.load(f)
|
|
|
|
current = True
|
|
|
|
for wp in d['items']:
|
|
|
|
yield Waypoint(
|
|
|
|
is_current = current,
|
|
|
|
frame = int(wp['frame']),
|
|
|
|
command = int(wp['command']),
|
|
|
|
param1 = float(wp['param1']),
|
|
|
|
param2 = float(wp['param2']),
|
|
|
|
param3 = float(wp['param3']),
|
|
|
|
param4 = float(wp['param4']),
|
|
|
|
x_lat = float(wp['coordinate'][0]),
|
|
|
|
y_long = float(wp['coordinate'][1]),
|
|
|
|
z_alt = float(wp['coordinate'][2]),
|
|
|
|
autocontinue = bool(wp['autoContinue']))
|
|
|
|
if current:
|
|
|
|
current = False
|
|
|
|
|
|
|
|
class MavrosMissionTest(unittest.TestCase):
|
|
|
|
"""
|
|
|
|
Run a mission
|
|
|
|
"""
|
|
|
|
|
|
|
|
def setUp(self):
|
|
|
|
rospy.init_node('test_node', anonymous=True)
|
|
|
|
|
|
|
|
self.rate = rospy.Rate(10) # 10hz
|
|
|
|
self.has_global_pos = False
|
|
|
|
self.local_position = PoseStamped()
|
|
|
|
self.global_position = NavSatFix()
|
|
|
|
self.extended_state = ExtendedState()
|
|
|
|
self.home_alt = 0
|
|
|
|
self.mc_rad = 5
|
|
|
|
self.fw_rad = 60
|
|
|
|
self.fw_alt_rad = 10
|
|
|
|
self.last_alt_d = 9999
|
|
|
|
self.last_pos_d = 9999
|
|
|
|
self.mission_name = ""
|
|
|
|
|
|
|
|
# need to simulate heartbeat for datalink loss detection
|
|
|
|
rospy.Timer(rospy.Duration(0.5), self.send_heartbeat)
|
|
|
|
|
|
|
|
rospy.wait_for_service('mavros/cmd/command', 30)
|
|
|
|
self.pub_mavlink = rospy.Publisher('mavlink/to', Mavlink, queue_size=1)
|
|
|
|
self._srv_cmd_long = rospy.ServiceProxy('mavros/cmd/command', CommandLong, persistent=True)
|
|
|
|
self._srv_wp_push = rospy.ServiceProxy('mavros/mission/push', WaypointPush, persistent=True)
|
|
|
|
|
|
|
|
rospy.Subscriber("mavros/local_position/pose", PoseStamped, self.position_callback)
|
|
|
|
rospy.Subscriber("mavros/global_position/global", NavSatFix, self.global_position_callback)
|
|
|
|
rospy.Subscriber("mavros/extended_state", ExtendedState, self.extended_state_callback)
|
|
|
|
|
|
|
|
def tearDown(self):
|
|
|
|
#self.helper.tearDown()
|
|
|
|
pass
|
|
|
|
|
|
|
|
#
|
|
|
|
# General callback functions used in tests
|
|
|
|
#
|
|
|
|
def position_callback(self, data):
|
|
|
|
self.local_position = data
|
|
|
|
|
|
|
|
def global_position_callback(self, data):
|
|
|
|
self.global_position = data
|
|
|
|
|
|
|
|
if not self.has_global_pos:
|
|
|
|
if data.altitude != 0:
|
|
|
|
self.home_alt = data.altitude
|
|
|
|
self.has_global_pos = True
|
|
|
|
|
|
|
|
def extended_state_callback(self, data):
|
|
|
|
|
|
|
|
prev_state = self.extended_state.vtol_state;
|
|
|
|
|
|
|
|
self.extended_state = data
|
|
|
|
if (prev_state != self.extended_state.vtol_state):
|
|
|
|
print("VTOL state change: %d" % self.extended_state.vtol_state);
|
|
|
|
|
|
|
|
#
|
|
|
|
# Helper methods
|
|
|
|
#
|
|
|
|
def is_at_position(self, lat, lon, alt, xy_offset, z_offset):
|
|
|
|
R = 6371000 # metres
|
|
|
|
rlat1 = math.radians(lat)
|
|
|
|
rlat2 = math.radians(self.global_position.latitude)
|
|
|
|
|
|
|
|
rlat_d = math.radians(self.global_position.latitude - lat)
|
|
|
|
rlon_d = math.radians(self.global_position.longitude - lon)
|
|
|
|
|
|
|
|
a = (math.sin(rlat_d / 2) * math.sin(rlat_d / 2) +
|
|
|
|
math.cos(rlat1) * math.cos(rlat2) *
|
|
|
|
math.sin(rlon_d / 2) * math.sin(rlon_d / 2))
|
|
|
|
c = 2 * math.atan2(math.sqrt(a), math.sqrt(1-a))
|
|
|
|
|
|
|
|
d = R * c
|
|
|
|
alt_d = abs(alt - self.global_position.altitude)
|
|
|
|
|
|
|
|
#rospy.loginfo("d: %f, alt_d: %f", d, alt_d)
|
|
|
|
|
|
|
|
# remember best distances
|
|
|
|
if self.last_pos_d > d:
|
|
|
|
self.last_pos_d = d
|
|
|
|
if self.last_alt_d > alt_d:
|
|
|
|
self.last_alt_d = alt_d
|
|
|
|
|
|
|
|
return d < xy_offset and alt_d < z_offset
|
|
|
|
|
|
|
|
def reach_position(self, lat, lon, alt, timeout, index):
|
|
|
|
# reset best distances
|
|
|
|
self.last_alt_d = 9999
|
|
|
|
self.last_pos_d = 9999
|
|
|
|
|
|
|
|
rospy.loginfo("trying to reach waypoint " +
|
|
|
|
"lat: %13.9f, lon: %13.9f, alt: %6.2f, timeout: %d, index: %d" %
|
|
|
|
(lat, lon, alt, timeout, index))
|
|
|
|
|
|
|
|
# does it reach the position in X seconds?
|
|
|
|
count = 0
|
|
|
|
while count < timeout:
|
|
|
|
# use MC radius by default
|
|
|
|
# FIXME: also check MAV_TYPE from system status, otherwise pure fixed-wing won't work
|
|
|
|
xy_radius = self.mc_rad
|
|
|
|
z_radius = self.mc_rad
|
|
|
|
|
|
|
|
# use FW radius if in FW or in transition
|
|
|
|
if (self.extended_state.vtol_state == ExtendedState.VTOL_STATE_FW or
|
|
|
|
self.extended_state.vtol_state == ExtendedState.VTOL_STATE_TRANSITION_TO_MC or
|
|
|
|
self.extended_state.vtol_state == ExtendedState.VTOL_STATE_TRANSITION_TO_FW):
|
|
|
|
xy_radius = self.fw_rad
|
|
|
|
z_radius = self.fw_alt_rad
|
|
|
|
|
|
|
|
if self.is_at_position(lat, lon, alt, xy_radius, z_radius):
|
|
|
|
rospy.loginfo("position reached, index: %d, count: %d, pos_d: %f, alt_d: %f" %
|
|
|
|
(index, count, self.last_pos_d, self.last_alt_d))
|
|
|
|
break
|
|
|
|
|
|
|
|
count = count + 1
|
|
|
|
self.rate.sleep()
|
|
|
|
|
|
|
|
vtol_state_string = "VTOL undefined"
|
|
|
|
|
|
|
|
if (self.extended_state.vtol_state == ExtendedState.VTOL_STATE_MC):
|
|
|
|
vtol_state_string = "VTOL MC"
|
|
|
|
if (self.extended_state.vtol_state == ExtendedState.VTOL_STATE_FW):
|
|
|
|
vtol_state_string = "VTOL FW"
|
|
|
|
if (self.extended_state.vtol_state == ExtendedState.VTOL_STATE_TRANSITION_TO_MC):
|
|
|
|
vtol_state_string = "VTOL FW->MC"
|
|
|
|
if (self.extended_state.vtol_state == ExtendedState.VTOL_STATE_TRANSITION_TO_FW):
|
|
|
|
vtol_state_string = "VTOL MC->FW"
|
|
|
|
|
|
|
|
self.assertTrue(count < timeout, (("(%s) took too long to get to position " +
|
|
|
|
"lat: %13.9f, lon: %13.9f, alt: %6.2f, xy off: %f, z off: %f, timeout: %d, index: %d, pos_d: %f, alt_d: %f, VTOL state: %s") %
|
|
|
|
(self.mission_name, lat, lon, alt, xy_radius, z_radius, timeout, index, self.last_pos_d, self.last_alt_d, vtol_state_string)))
|
|
|
|
|
|
|
|
def run_mission(self):
|
|
|
|
# Hack to wait until vehicle is ready
|
|
|
|
# TODO better integration with pre-flight status reporting
|
|
|
|
time.sleep(5)
|
|
|
|
"""switch mode: auto and arm"""
|
|
|
|
self._srv_cmd_long(False, 176, False,
|
|
|
|
# custom, auto, mission
|
|
|
|
1, 4, 4, 0, 0, 0, 0)
|
|
|
|
# make sure the first command doesn't get lost
|
|
|
|
time.sleep(1)
|
|
|
|
|
|
|
|
self._srv_cmd_long(False, 400, False,
|
|
|
|
# arm
|
|
|
|
1, 0, 0, 0, 0, 0, 0)
|
|
|
|
|
|
|
|
def wait_until_ready(self):
|
|
|
|
"""FIXME: hack to wait for simulation to be ready"""
|
|
|
|
while not self.has_global_pos:
|
|
|
|
self.rate.sleep()
|
|
|
|
|
|
|
|
def wait_on_landing(self, timeout, index):
|
|
|
|
"""Wait for landed state"""
|
|
|
|
|
|
|
|
rospy.loginfo("waiting for landing " +
|
|
|
|
"timeout: %d, index: %d" %
|
|
|
|
(timeout, index))
|
|
|
|
|
|
|
|
count = 0
|
|
|
|
while count < timeout:
|
|
|
|
if self.extended_state.landed_state == ExtendedState.LANDED_STATE_ON_GROUND:
|
|
|
|
break
|
|
|
|
|
|
|
|
count = count + 1
|
|
|
|
self.rate.sleep()
|
|
|
|
|
|
|
|
self.assertTrue(count < timeout, ("(%s) landing not detected after landing WP " +
|
|
|
|
"timeout: %d, index: %d") %
|
|
|
|
(self.mission_name, timeout, index))
|
|
|
|
|
|
|
|
def wait_on_transition(self, transition, timeout, index):
|
|
|
|
"""Wait for VTOL transition"""
|
|
|
|
|
|
|
|
rospy.loginfo("waiting for VTOL transition " +
|
|
|
|
"transition: %d, timeout: %d, index: %d" %
|
|
|
|
(transition, timeout, index))
|
|
|
|
|
|
|
|
count = 0
|
|
|
|
while count < timeout:
|
|
|
|
# transition to MC
|
|
|
|
if (transition == ExtendedState.VTOL_STATE_MC and
|
|
|
|
self.extended_state.vtol_state == ExtendedState.VTOL_STATE_MC):
|
|
|
|
break
|
|
|
|
|
|
|
|
# transition to FW
|
|
|
|
if (transition == ExtendedState.VTOL_STATE_FW and
|
|
|
|
self.extended_state.vtol_state == ExtendedState.VTOL_STATE_FW):
|
|
|
|
break
|
|
|
|
|
|
|
|
count = count + 1
|
|
|
|
self.rate.sleep()
|
|
|
|
|
|
|
|
self.assertTrue(count < timeout, ("(%s) transition not detected " +
|
|
|
|
"timeout: %d, index: %d") %
|
|
|
|
(self.mission_name, timeout, index))
|
|
|
|
|
|
|
|
def send_heartbeat(self, event=None):
|
|
|
|
# mav type gcs
|
|
|
|
mavmsg = mavutil.mavlink.MAVLink_heartbeat_message(6, 0, 0, 0, 0, 0)
|
|
|
|
# XXX: hack: using header object to set mav properties
|
|
|
|
mavmsg.pack(mavutil.mavlink.MAVLink_header(0, 0, 0, 2, 1))
|
|
|
|
rosmsg = mavlink.convert_to_rosmsg(mavmsg)
|
|
|
|
self.pub_mavlink.publish(rosmsg)
|
|
|
|
|
|
|
|
def test_mission(self):
|
|
|
|
"""Test mission"""
|
|
|
|
|
|
|
|
if len(sys.argv) < 2:
|
|
|
|
self.fail("usage: mission_test.py mission_file")
|
|
|
|
return
|
|
|
|
|
|
|
|
self.mission_name = sys.argv[1]
|
|
|
|
mission_file = os.path.dirname(os.path.realpath(__file__)) + "/" + sys.argv[1]
|
|
|
|
|
|
|
|
rospy.loginfo("reading mission %s", mission_file)
|
|
|
|
wps = []
|
|
|
|
|
|
|
|
with open(mission_file, 'r') as f:
|
|
|
|
mission_ext = os.path.splitext(mission_file)[1]
|
|
|
|
if mission_ext == '.mission':
|
|
|
|
rospy.loginfo("new style mission file detected")
|
|
|
|
for waypoint in read_new_mission(f):
|
|
|
|
wps.append(waypoint)
|
|
|
|
rospy.logdebug(waypoint)
|
|
|
|
elif mission_ext == '.txt':
|
|
|
|
rospy.loginfo("old style mission file detected")
|
|
|
|
mission = QGroundControlWP()
|
|
|
|
for waypoint in mission.read(f):
|
|
|
|
wps.append(waypoint)
|
|
|
|
rospy.logdebug(waypoint)
|
|
|
|
else:
|
|
|
|
raise IOError('unknown mission file extension', mission_ext)
|
|
|
|
|
|
|
|
rospy.loginfo("wait until ready")
|
|
|
|
self.wait_until_ready()
|
|
|
|
|
|
|
|
rospy.loginfo("send mission")
|
|
|
|
res = self._srv_wp_push(wps)
|
|
|
|
rospy.loginfo(res)
|
|
|
|
self.assertTrue(res.success, "(%s) mission could not be transfered" % self.mission_name)
|
|
|
|
|
|
|
|
rospy.loginfo("run mission")
|
|
|
|
self.run_mission()
|
|
|
|
|
|
|
|
index = 0
|
|
|
|
for waypoint in wps:
|
|
|
|
# only check position for waypoints where this makes sense
|
|
|
|
if waypoint.frame == Waypoint.FRAME_GLOBAL_REL_ALT or waypoint.frame == Waypoint.FRAME_GLOBAL:
|
|
|
|
alt = waypoint.z_alt
|
|
|
|
if waypoint.frame == Waypoint.FRAME_GLOBAL_REL_ALT:
|
|
|
|
alt += self.home_alt
|
|
|
|
|
|
|
|
self.reach_position(waypoint.x_lat, waypoint.y_long, alt, 600, index)
|
|
|
|
|
|
|
|
# check if VTOL transition happens if applicable
|
|
|
|
if waypoint.command == 84 or waypoint.command == 85 or waypoint.command == 3000:
|
|
|
|
transition = waypoint.param1
|
|
|
|
|
|
|
|
if waypoint.command == 84: # VTOL takeoff implies transition to FW
|
|
|
|
transition = ExtendedState.VTOL_STATE_FW
|
|
|
|
|
|
|
|
if waypoint.command == 85: # VTOL takeoff implies transition to MC
|
|
|
|
transition = ExtendedState.VTOL_STATE_MC
|
|
|
|
|
|
|
|
self.wait_on_transition(transition, 600, index)
|
|
|
|
|
|
|
|
# after reaching position, wait for landing detection if applicable
|
|
|
|
if waypoint.command == 85 or waypoint.command == 21:
|
|
|
|
self.wait_on_landing(600, index)
|
|
|
|
|
|
|
|
index += 1
|
|
|
|
|
|
|
|
rospy.loginfo("mission done, calculating performance metrics")
|
|
|
|
last_log = get_last_log()
|
|
|
|
rospy.loginfo("log file %s", last_log)
|
|
|
|
data = px4tools.ulog.read_ulog(last_log).concat(dt=0.1)
|
|
|
|
data = px4tools.ulog.compute_data(data)
|
|
|
|
res = px4tools.estimator_analysis(data, False)
|
|
|
|
|
|
|
|
# enforce performance
|
|
|
|
self.assertTrue(abs(res['roll_error_mean']) < 5.0, str(res))
|
|
|
|
self.assertTrue(abs(res['pitch_error_mean']) < 5.0, str(res))
|
|
|
|
self.assertTrue(abs(res['yaw_error_mean']) < 5.0, str(res))
|
|
|
|
self.assertTrue(res['roll_error_std'] < 5.0, str(res))
|
|
|
|
self.assertTrue(res['pitch_error_std'] < 5.0, str(res))
|
|
|
|
self.assertTrue(res['yaw_error_std'] < 5.0, str(res))
|
|
|
|
|
|
|
|
if __name__ == '__main__':
|
|
|
|
import rostest
|
|
|
|
name = "mavros_mission_test"
|
|
|
|
if len(sys.argv) > 1:
|
|
|
|
name += "-%s" % sys.argv[1]
|
|
|
|
rostest.rosrun(PKG, name, MavrosMissionTest)
|