mirror of
https://github.com/ArduPilot/ardupilot
synced 2025-01-03 06:28:27 -04:00
Tools: sitl_calibration: add initial implementation
Add initial implementation to interface with SITL calibration model.
This commit is contained in:
parent
b594b5a08b
commit
363f241e9a
33
Tools/mavproxy_modules/README.md
Normal file
33
Tools/mavproxy_modules/README.md
Normal file
@ -0,0 +1,33 @@
|
|||||||
|
# MAVProxy modules #
|
||||||
|
|
||||||
|
This folder contains modules for MAVProxy specifically for ArduPilot. Add the
|
||||||
|
path to this folder to your `PYTHONPATH` in order to use it.
|
||||||
|
|
||||||
|
# Modules #
|
||||||
|
|
||||||
|
## `sitl_calibration` ##
|
||||||
|
This module interfaces with the `calibration` model of SITL. It provides
|
||||||
|
commands to actuate on the vehicle's rotation to simulate a calibration
|
||||||
|
process.
|
||||||
|
|
||||||
|
### Accelerometer Calibration ###
|
||||||
|
The command `sitl_accelcal` listens to the accelerometer calibration status
|
||||||
|
texts and set the vehicle in the desired attitude. Example:
|
||||||
|
```
|
||||||
|
accelcal
|
||||||
|
sitl_accelcal
|
||||||
|
```
|
||||||
|
|
||||||
|
### Compass Calibration ###
|
||||||
|
The command `sitl_magcal` applies angular velocity on the vehicle in order to
|
||||||
|
get the compasses calibrated. Example:
|
||||||
|
```
|
||||||
|
magcal start
|
||||||
|
sitl_magcal
|
||||||
|
```
|
||||||
|
|
||||||
|
### Other commands ###
|
||||||
|
There are other commands you can use with this module:
|
||||||
|
- `sitl_attitude`: set vehicle at a desired attitude
|
||||||
|
- `sitl_angvel`: apply angular velocity on the vehicle
|
||||||
|
- `sitl_stop`: stop any of this module's currently active command
|
201
Tools/mavproxy_modules/sitl_calibration.py
Normal file
201
Tools/mavproxy_modules/sitl_calibration.py
Normal file
@ -0,0 +1,201 @@
|
|||||||
|
# Copyright (C) 2015-2016 Intel Corporation. All rights reserved.
|
||||||
|
#
|
||||||
|
# This file is free software: you can redistribute it and/or modify it
|
||||||
|
# under the terms of the GNU General Public License as published by the
|
||||||
|
# Free Software Foundation, either version 3 of the License, or
|
||||||
|
# (at your option) any later version.
|
||||||
|
#
|
||||||
|
# This file 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 General Public License for more details.
|
||||||
|
#
|
||||||
|
# You should have received a copy of the GNU General Public License along
|
||||||
|
# with this program. If not, see <http://www.gnu.org/licenses/>.
|
||||||
|
'''calibration simulation command handling'''
|
||||||
|
|
||||||
|
from __future__ import division, print_function
|
||||||
|
import math
|
||||||
|
from pymavlink import quaternion
|
||||||
|
|
||||||
|
from MAVProxy.modules.lib import mp_module
|
||||||
|
|
||||||
|
class CalController(object):
|
||||||
|
def __init__(self, mpstate):
|
||||||
|
self.mpstate = mpstate
|
||||||
|
self.active = False
|
||||||
|
self.reset()
|
||||||
|
|
||||||
|
def reset(self):
|
||||||
|
self.desired_quaternion = None
|
||||||
|
self.general_state = 'idle'
|
||||||
|
self.attitude_callback = None
|
||||||
|
self.desired_quaternion_close_count = 0
|
||||||
|
|
||||||
|
def start(self):
|
||||||
|
self.active = True
|
||||||
|
|
||||||
|
def stop(self):
|
||||||
|
self.reset()
|
||||||
|
self.mpstate.functions.process_stdin('servo set 5 1000')
|
||||||
|
self.active = False
|
||||||
|
|
||||||
|
def normalize_attitude_angle(self, angle):
|
||||||
|
if angle < 0:
|
||||||
|
angle = 2 * math.pi + angle % (-2 * math.pi)
|
||||||
|
angle %= 2 * math.pi
|
||||||
|
if angle > math.pi:
|
||||||
|
return angle % -math.pi
|
||||||
|
return angle
|
||||||
|
|
||||||
|
def set_attitute(self, roll, pitch, yaw, callback=None):
|
||||||
|
roll = self.normalize_attitude_angle(roll)
|
||||||
|
pitch = self.normalize_attitude_angle(pitch)
|
||||||
|
yaw = self.normalize_attitude_angle(yaw)
|
||||||
|
|
||||||
|
self.desired_quaternion = quaternion.Quaternion((roll, pitch, yaw))
|
||||||
|
self.desired_quaternion.normalize()
|
||||||
|
|
||||||
|
scale = 500.0 / math.pi
|
||||||
|
|
||||||
|
roll_pwm = 1500 + int(roll * scale)
|
||||||
|
pitch_pwm = 1500 + int(pitch * scale)
|
||||||
|
yaw_pwm = 1500 + int(yaw * scale)
|
||||||
|
|
||||||
|
self.mpstate.functions.process_stdin('servo set 5 1150')
|
||||||
|
self.mpstate.functions.process_stdin('servo set 6 %d' % roll_pwm)
|
||||||
|
self.mpstate.functions.process_stdin('servo set 7 %d' % pitch_pwm)
|
||||||
|
self.mpstate.functions.process_stdin('servo set 8 %d' % yaw_pwm)
|
||||||
|
|
||||||
|
self.general_state = 'attitude'
|
||||||
|
self.desired_quaternion_close_count = 0
|
||||||
|
|
||||||
|
if callback:
|
||||||
|
self.attitude_callback = callback
|
||||||
|
|
||||||
|
def angvel(self, x, y, z, theta):
|
||||||
|
m = max(abs(x), abs(y), abs(z))
|
||||||
|
if not m:
|
||||||
|
x_pwm = y_pwm = z_pwm = 1500
|
||||||
|
else:
|
||||||
|
x_pwm = 1500 + round((x / m) * 500)
|
||||||
|
y_pwm = 1500 + round((y / m) * 500)
|
||||||
|
z_pwm = 1500 + round((z / m) * 500)
|
||||||
|
|
||||||
|
max_theta = 2 * math.pi
|
||||||
|
if theta < 0:
|
||||||
|
theta = 0
|
||||||
|
elif theta > max_theta:
|
||||||
|
theta = max_theta
|
||||||
|
theta_pwm = 1200 + round((theta / max_theta) * 800)
|
||||||
|
|
||||||
|
self.mpstate.functions.process_stdin('servo set 5 %d' % theta_pwm)
|
||||||
|
self.mpstate.functions.process_stdin('servo set 6 %d' % x_pwm)
|
||||||
|
self.mpstate.functions.process_stdin('servo set 7 %d' % y_pwm)
|
||||||
|
self.mpstate.functions.process_stdin('servo set 8 %d' % z_pwm)
|
||||||
|
|
||||||
|
self.general_state = 'angvel'
|
||||||
|
|
||||||
|
def handle_simstate(self, m):
|
||||||
|
if self.general_state == 'attitude':
|
||||||
|
q = quaternion.Quaternion((m.roll, m.pitch, m.yaw))
|
||||||
|
q.normalize()
|
||||||
|
d1 = abs(self.desired_quaternion.q - q.q)
|
||||||
|
d2 = abs(self.desired_quaternion.q + q.q)
|
||||||
|
if (d1 <= 1e-2).all() or (d2 <= 1e-2).all():
|
||||||
|
self.desired_quaternion_close_count += 1
|
||||||
|
else:
|
||||||
|
self.desired_quaternion_close_count = 0
|
||||||
|
|
||||||
|
if self.desired_quaternion_close_count == 5:
|
||||||
|
self.general_state = 'idle'
|
||||||
|
if callable(self.attitude_callback):
|
||||||
|
self.attitude_callback()
|
||||||
|
self.attitude_callback = None
|
||||||
|
|
||||||
|
def mavlink_packet(self, m):
|
||||||
|
if not self.active:
|
||||||
|
return
|
||||||
|
if m.get_type() == 'SIMSTATE':
|
||||||
|
self.handle_simstate(m)
|
||||||
|
|
||||||
|
|
||||||
|
class SitlCalibrationModule(mp_module.MPModule):
|
||||||
|
def __init__(self, mpstate):
|
||||||
|
super(SitlCalibrationModule, self).__init__(mpstate, "sitl_calibration")
|
||||||
|
self.add_command(
|
||||||
|
'sitl_attitude',
|
||||||
|
self.cmd_sitl_attitude,
|
||||||
|
'set the vehicle at the inclination given by ROLL, PITCH and YAW' +
|
||||||
|
' in degrees',
|
||||||
|
)
|
||||||
|
self.add_command(
|
||||||
|
'sitl_angvel',
|
||||||
|
self.cmd_angvel,
|
||||||
|
'apply angular velocity on the vehicle with a rotation axis and a '+
|
||||||
|
'magnitude in degrees/s',
|
||||||
|
)
|
||||||
|
self.add_command(
|
||||||
|
'sitl_stop',
|
||||||
|
self.cmd_sitl_stop,
|
||||||
|
'stop the current calibration control',
|
||||||
|
)
|
||||||
|
|
||||||
|
self.controllers = dict(
|
||||||
|
generic_controller=CalController(mpstate),
|
||||||
|
)
|
||||||
|
|
||||||
|
self.current_controller = None
|
||||||
|
|
||||||
|
def set_controller(self, controller):
|
||||||
|
if self.current_controller:
|
||||||
|
self.current_controller.stop()
|
||||||
|
|
||||||
|
controller = self.controllers.get(controller, None)
|
||||||
|
if controller:
|
||||||
|
controller.start()
|
||||||
|
self.current_controller = controller
|
||||||
|
|
||||||
|
def cmd_sitl_attitude(self, args):
|
||||||
|
if len(args) != 3:
|
||||||
|
print('Usage: sitl_attitude <ROLL> <PITCH> <YAW>')
|
||||||
|
return
|
||||||
|
|
||||||
|
try:
|
||||||
|
roll, pitch, yaw = args
|
||||||
|
roll = math.radians(float(roll))
|
||||||
|
pitch = math.radians(float(pitch))
|
||||||
|
yaw = math.radians(float(yaw))
|
||||||
|
except ValueError:
|
||||||
|
print('Invalid arguments')
|
||||||
|
|
||||||
|
self.set_controller('generic_controller')
|
||||||
|
self.current_controller.set_attitute(roll, pitch, yaw)
|
||||||
|
|
||||||
|
def cmd_angvel(self, args):
|
||||||
|
if len(args) != 4:
|
||||||
|
print('Usage: sitl_angvel <AXIS_X> <AXIS_Y> <AXIS_Z> <THETA>')
|
||||||
|
return
|
||||||
|
|
||||||
|
try:
|
||||||
|
x, y, z, theta = args
|
||||||
|
x = float(x)
|
||||||
|
y = float(y)
|
||||||
|
z = float(z)
|
||||||
|
theta = math.radians(float(theta))
|
||||||
|
except ValueError:
|
||||||
|
print('Invalid arguments')
|
||||||
|
|
||||||
|
self.set_controller('generic_controller')
|
||||||
|
self.current_controller.angvel(x, y, z, theta)
|
||||||
|
|
||||||
|
def cmd_sitl_stop(self, args):
|
||||||
|
self.set_controller('generic_controller')
|
||||||
|
|
||||||
|
def mavlink_packet(self, m):
|
||||||
|
for c in self.controllers.values():
|
||||||
|
c.mavlink_packet(m)
|
||||||
|
|
||||||
|
def init(mpstate):
|
||||||
|
'''initialise module'''
|
||||||
|
return SitlCalibrationModule(mpstate)
|
Loading…
Reference in New Issue
Block a user