Merge branch 'master' of github.com:PX4/Firmware into fw_autoland

This commit is contained in:
Lorenz Meier 2013-10-24 22:45:43 +02:00
commit 20728e83f5
67 changed files with 3017 additions and 718 deletions

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@ -0,0 +1,110 @@
#!nsh
#
# USB HIL start
#
echo "[HIL] HILS quadrotor + starting.."
#
# Load default params for this platform
#
if param compare SYS_AUTOCONFIG 1
then
# Set all params here, then disable autoconfig
param set SYS_AUTOCONFIG 0
param set MC_ATTRATE_D 0.0
param set MC_ATTRATE_I 0.0
param set MC_ATTRATE_P 0.05
param set MC_ATT_D 0.0
param set MC_ATT_I 0.0
param set MC_ATT_P 3.0
param set MC_YAWPOS_D 0.0
param set MC_YAWPOS_I 0.0
param set MC_YAWPOS_P 2.1
param set MC_YAWRATE_D 0.0
param set MC_YAWRATE_I 0.0
param set MC_YAWRATE_P 0.05
param set NAV_TAKEOFF_ALT 3.0
param set MPC_TILT_MAX 0.5
param set MPC_THR_MAX 0.5
param set MPC_THR_MIN 0.1
param set MPC_XY_D 0
param set MPC_XY_P 0.5
param set MPC_XY_VEL_D 0
param set MPC_XY_VEL_I 0
param set MPC_XY_VEL_MAX 3
param set MPC_XY_VEL_P 0.2
param set MPC_Z_D 0
param set MPC_Z_P 1
param set MPC_Z_VEL_D 0
param set MPC_Z_VEL_I 0.1
param set MPC_Z_VEL_MAX 2
param set MPC_Z_VEL_P 0.20
param save
fi
# Allow USB some time to come up
sleep 1
# Tell MAVLink that this link is "fast"
mavlink start -b 230400 -d /dev/ttyACM0
# Create a fake HIL /dev/pwm_output interface
hil mode_pwm
#
# Force some key parameters to sane values
# MAV_TYPE 1 = fixed wing, 2 = quadrotor, 13 = hexarotor
# see https://pixhawk.ethz.ch/mavlink/
#
param set MAV_TYPE 2
#
# Start the commander (depends on orb, mavlink)
#
commander start
#
# Check if we got an IO
#
if px4io start
then
echo "IO started"
else
fmu mode_serial
echo "FMU started"
fi
#
# Start the sensors (depends on orb, px4io)
#
sh /etc/init.d/rc.sensors
#
# Start the attitude estimator (depends on orb)
#
att_pos_estimator_ekf start
#
# Load mixer and start controllers (depends on px4io)
#
mixer load /dev/pwm_output /etc/mixers/FMU_quad_+.mix
#
# Start position estimator
#
position_estimator_inav start
#
# Start attitude control
#
multirotor_att_control start
#
# Start position control
#
multirotor_pos_control start
echo "[HIL] setup done, running"

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@ -0,0 +1,103 @@
#!nsh
#
# USB HIL start
#
echo "[HIL] HILStar starting.."
#
# Load default params for this platform
#
if param compare SYS_AUTOCONFIG 1
then
# Set all params here, then disable autoconfig
param set FW_P_D 0
param set FW_P_I 0
param set FW_P_IMAX 15
param set FW_P_LIM_MAX 50
param set FW_P_LIM_MIN -50
param set FW_P_P 60
param set FW_P_RMAX_NEG 0
param set FW_P_RMAX_POS 0
param set FW_P_ROLLFF 1.1
param set FW_R_D 0
param set FW_R_I 5
param set FW_R_IMAX 20
param set FW_R_P 100
param set FW_R_RMAX 100
param set FW_THR_CRUISE 0.65
param set FW_THR_MAX 1
param set FW_THR_MIN 0
param set FW_T_SINK_MAX 5.0
param set FW_T_SINK_MIN 4.0
param set FW_Y_ROLLFF 1.1
param set FW_L1_PERIOD 16
param set RC_SCALE_ROLL 1.0
param set RC_SCALE_PITCH 1.0
param set SYS_AUTOCONFIG 0
param save
fi
# Allow USB some time to come up
sleep 1
# Tell MAVLink that this link is "fast"
mavlink start -b 230400 -d /dev/ttyACM0
# Create a fake HIL /dev/pwm_output interface
hil mode_pwm
#
# Force some key parameters to sane values
# MAV_TYPE 1 = fixed wing, 2 = quadrotor, 13 = hexarotor
# see https://pixhawk.ethz.ch/mavlink/
#
param set MAV_TYPE 1
#
# Start the commander (depends on orb, mavlink)
#
commander start
#
# Check if we got an IO
#
if px4io start
then
echo "IO started"
else
fmu mode_serial
echo "FMU started"
fi
#
# Start the sensors (depends on orb, px4io)
#
sh /etc/init.d/rc.sensors
#
# Start the attitude estimator (depends on orb)
#
att_pos_estimator_ekf start
#
# Load mixer and start controllers (depends on px4io)
#
set MODE autostart
mixer load /dev/pwm_output /etc/mixers/FMU_AERT.mix
if [ -f /fs/microsd/etc/mixers/FMU_AERT.mix ]
then
echo "Using /fs/microsd/etc/mixers/FMU_AERT.mix"
mixer load /dev/pwm_output /fs/microsd/etc/mixers/FMU_AERT.mix
else
echo "Using /etc/mixers/FMU_AERT.mix"
mixer load /dev/pwm_output /etc/mixers/FMU_AERT.mix
fi
fw_pos_control_l1 start
fw_att_control start
echo "[HIL] setup done, running"

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@ -0,0 +1,95 @@
#!nsh
echo "[init] PX4FMU v1, v2 with or without IO on Hex"
#
# Load default params for this platform
#
if param compare SYS_AUTOCONFIG 1
then
# Set all params here, then disable autoconfig
param set SYS_AUTOCONFIG 0
param set MC_ATTRATE_D 0.004
param set MC_ATTRATE_I 0.0
param set MC_ATTRATE_P 0.12
param set MC_ATT_D 0.0
param set MC_ATT_I 0.0
param set MC_ATT_P 7.0
param set MC_YAWPOS_D 0.0
param set MC_YAWPOS_I 0.0
param set MC_YAWPOS_P 2.0
param set MC_YAWRATE_D 0.005
param set MC_YAWRATE_I 0.2
param set MC_YAWRATE_P 0.3
param set NAV_TAKEOFF_ALT 3.0
param set MPC_TILT_MAX 0.5
param set MPC_THR_MAX 0.7
param set MPC_THR_MIN 0.3
param set MPC_XY_D 0
param set MPC_XY_P 0.5
param set MPC_XY_VEL_D 0
param set MPC_XY_VEL_I 0
param set MPC_XY_VEL_MAX 3
param set MPC_XY_VEL_P 0.2
param set MPC_Z_D 0
param set MPC_Z_P 1
param set MPC_Z_VEL_D 0
param set MPC_Z_VEL_I 0.1
param set MPC_Z_VEL_MAX 2
param set MPC_Z_VEL_P 0.20
param save
fi
#
# Force some key parameters to sane values
# MAV_TYPE list: https://pixhawk.ethz.ch/mavlink/
# 13 = hexarotor
#
param set MAV_TYPE 13
set EXIT_ON_END no
#
# Start and configure PX4IO or FMU interface
#
if px4io detect
then
# Start MAVLink (depends on orb)
mavlink start
usleep 5000
sh /etc/init.d/rc.io
# Set PWM values for DJI ESCs
px4io idle 900 900 900 900 900 900
px4io min 1200 1200 1200 1200 1200 1200
px4io max 1900 1900 1900 1900 1900 1900
else
# Start MAVLink (on UART1 / ttyS0)
mavlink start -d /dev/ttyS0
usleep 5000
fmu mode_pwm
param set BAT_V_SCALING 0.004593
set EXIT_ON_END yes
fi
#
# Load mixer
#
mixer load /dev/pwm_output $MIXER
#
# Set PWM output frequency to 400 Hz
#
pwm -u 400 -m 0xff
#
# Start common for all multirotors apps
#
sh /etc/init.d/rc.multirotor
if [ $EXIT_ON_END == yes ]
then
exit
fi

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@ -0,0 +1,86 @@
#!nsh
echo "[init] PX4FMU v1, v2 with or without IO on Skywalker X5"
#
# Load default params for this platform
#
if param compare SYS_AUTOCONFIG 1
then
# Set all params here, then disable autoconfig
# TODO
param set SYS_AUTOCONFIG 0
param save
fi
#
# Force some key parameters to sane values
# MAV_TYPE 1 = fixed wing
#
param set MAV_TYPE 1
set EXIT_ON_END no
#
# Start and configure PX4IO or FMU interface
#
if px4io detect
then
# Start MAVLink (depends on orb)
mavlink start
commander start
sh /etc/init.d/rc.io
# Limit to 100 Hz updates and (implicit) 50 Hz PWM
px4io limit 100
else
# Start MAVLink (on UART1 / ttyS0)
mavlink start -d /dev/ttyS0
commander start
fmu mode_pwm
param set BAT_V_SCALING 0.004593
set EXIT_ON_END yes
fi
#
# Start the sensors and test them.
#
sh /etc/init.d/rc.sensors
#
# Start logging (depends on sensors)
#
sh /etc/init.d/rc.logging
#
# Start GPS interface (depends on orb)
#
gps start
#
# Start the attitude and position estimator
#
att_pos_estimator_ekf start
#
# Load mixer and start controllers (depends on px4io)
#
if [ -f /fs/microsd/etc/mixers/FMU_Q.mix ]
then
echo "Using /fs/microsd/etc/mixers/FMU_Q.mix"
mixer load /dev/pwm_output /fs/microsd/etc/mixers/FMU_Q.mix
else
echo "Using /etc/mixers/FMU_Q.mix"
mixer load /dev/pwm_output /etc/mixers/FMU_Q.mix
fi
fw_att_control start
fw_pos_control_l1 start
if [ $EXIT_ON_END == yes ]
then
exit
fi

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@ -52,5 +52,5 @@ attitude_estimator_ekf start
#
# Load mixer and start controllers (depends on px4io)
#
md25 start 3 0x58
roboclaw start /dev/ttyS2 128 1200
segway start

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@ -58,7 +58,7 @@ usleep 10000
if px4io detect
then
# Start MAVLink (depends on orb)
mavlink start -d /dev/ttyS1 -b 115200
mavlink start -d /dev/ttyS1 -b 57600
usleep 5000
sh /etc/init.d/rc.io
@ -78,7 +78,7 @@ then
else
fmu mode_pwm
# Start MAVLink (on UART1 / ttyS0)
mavlink start -d /dev/ttyS1 -b 115200
mavlink start -d /dev/ttyS1 -b 57600
usleep 5000
param set BAT_V_SCALING 0.004593
set EXIT_ON_END yes

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@ -108,25 +108,41 @@ then
if param compare SYS_AUTOSTART 1000
then
sh /etc/init.d/1000_rc_fw.hil
sh /etc/init.d/1000_rc_fw_easystar.hil
set MODE custom
else
if param compare SYS_AUTOSTART 1001
then
sh /etc/init.d/1001_rc_quad.hil
set MODE custom
else
if param compare SYS_AUTOSTART 1002
then
sh /etc/init.d/1002_rc_fw_state.hil
set MODE custom
else
# Try to get an USB console
nshterm /dev/ttyACM0 &
fi
fi
fi
if param compare SYS_AUTOSTART 1001
then
sh /etc/init.d/1001_rc_quad.hil
set MODE custom
fi
if param compare SYS_AUTOSTART 1002
then
sh /etc/init.d/1002_rc_fw_state.hil
set MODE custom
fi
if param compare SYS_AUTOSTART 1003
then
sh /etc/init.d/1003_rc_quad_+.hil
set MODE custom
fi
if param compare SYS_AUTOSTART 1004
then
sh /etc/init.d/1004_rc_fw_Rascal110.hil
set MODE custom
fi
if [ $MODE != custom ]
then
# Try to get an USB console
nshterm /dev/ttyACM0 &
fi
#
# Upgrade PX4IO firmware
#
@ -177,6 +193,20 @@ then
sh /etc/init.d/11_dji_f450
set MODE custom
fi
if param compare SYS_AUTOSTART 12
then
set MIXER /etc/mixers/FMU_hex_x.mix
sh /etc/init.d/12-13_hex
set MODE custom
fi
if param compare SYS_AUTOSTART 13
then
set MIXER /etc/mixers/FMU_hex_+.mix
sh /etc/init.d/12-13_hex
set MODE custom
fi
if param compare SYS_AUTOSTART 15
then
@ -248,13 +278,25 @@ then
sh /etc/init.d/30_io_camflyer
set MODE custom
fi
if param compare SYS_AUTOSTART 31
then
sh /etc/init.d/31_io_phantom
set MODE custom
fi
if param compare SYS_AUTOSTART 32
then
sh /etc/init.d/32_skywalker_x5
set MODE custom
fi
if param compare SYS_AUTOSTART 40
then
sh /etc/init.d/40_io_segway
set MODE custom
fi
if param compare SYS_AUTOSTART 100
then
sh /etc/init.d/100_mpx_easystar

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@ -62,3 +62,23 @@ range. Inputs below zero are treated as zero.
M: 1
O: 10000 10000 0 -10000 10000
S: 0 3 0 20000 -10000 -10000 10000
Gimbal / flaps / payload mixer for last four channels
-----------------------------------------------------
M: 1
O: 10000 10000 0 -10000 10000
S: 0 4 10000 10000 0 -10000 10000
M: 1
O: 10000 10000 0 -10000 10000
S: 0 5 10000 10000 0 -10000 10000
M: 1
O: 10000 10000 0 -10000 10000
S: 0 6 10000 10000 0 -10000 10000
M: 1
O: 10000 10000 0 -10000 10000
S: 0 7 10000 10000 0 -10000 10000

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@ -58,3 +58,23 @@ range. Inputs below zero are treated as zero.
M: 1
O: 10000 10000 0 -10000 10000
S: 0 3 0 20000 -10000 -10000 10000
Gimbal / flaps / payload mixer for last four channels
-----------------------------------------------------
M: 1
O: 10000 10000 0 -10000 10000
S: 0 4 10000 10000 0 -10000 10000
M: 1
O: 10000 10000 0 -10000 10000
S: 0 5 10000 10000 0 -10000 10000
M: 1
O: 10000 10000 0 -10000 10000
S: 0 6 10000 10000 0 -10000 10000
M: 1
O: 10000 10000 0 -10000 10000
S: 0 7 10000 10000 0 -10000 10000

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@ -50,3 +50,21 @@ M: 1
O: 10000 10000 0 -10000 10000
S: 0 3 0 20000 -10000 -10000 10000
Gimbal / flaps / payload mixer for last four channels
-----------------------------------------------------
M: 1
O: 10000 10000 0 -10000 10000
S: 0 4 10000 10000 0 -10000 10000
M: 1
O: 10000 10000 0 -10000 10000
S: 0 5 10000 10000 0 -10000 10000
M: 1
O: 10000 10000 0 -10000 10000
S: 0 6 10000 10000 0 -10000 10000
M: 1
O: 10000 10000 0 -10000 10000
S: 0 7 10000 10000 0 -10000 10000

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@ -51,3 +51,23 @@ range. Inputs below zero are treated as zero.
M: 1
O: 10000 10000 0 -10000 10000
S: 0 3 0 20000 -10000 -10000 10000
Gimbal / payload mixer for last four channels
-----------------------------------------------------
M: 1
O: 10000 10000 0 -10000 10000
S: 0 4 10000 10000 0 -10000 10000
M: 1
O: 10000 10000 0 -10000 10000
S: 0 5 10000 10000 0 -10000 10000
M: 1
O: 10000 10000 0 -10000 10000
S: 0 6 10000 10000 0 -10000 10000
M: 1
O: 10000 10000 0 -10000 10000
S: 0 7 10000 10000 0 -10000 10000

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@ -48,3 +48,22 @@ M: 1
O: 10000 10000 0 -10000 10000
S: 0 3 0 20000 -10000 -10000 10000
Gimbal / payload mixer for last four channels
-----------------------------------------------------
M: 1
O: 10000 10000 0 -10000 10000
S: 0 4 10000 10000 0 -10000 10000
M: 1
O: 10000 10000 0 -10000 10000
S: 0 5 10000 10000 0 -10000 10000
M: 1
O: 10000 10000 0 -10000 10000
S: 0 6 10000 10000 0 -10000 10000
M: 1
O: 10000 10000 0 -10000 10000
S: 0 7 10000 10000 0 -10000 10000

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@ -48,3 +48,23 @@ M: 1
O: 10000 10000 0 -10000 10000
S: 0 3 0 20000 -10000 -10000 10000
Gimbal / flaps / payload mixer for last four channels
-----------------------------------------------------
M: 1
O: 10000 10000 0 -10000 10000
S: 0 4 10000 10000 0 -10000 10000
M: 1
O: 10000 10000 0 -10000 10000
S: 0 5 10000 10000 0 -10000 10000
M: 1
O: 10000 10000 0 -10000 10000
S: 0 6 10000 10000 0 -10000 10000
M: 1
O: 10000 10000 0 -10000 10000
S: 0 7 10000 10000 0 -10000 10000

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@ -5,3 +5,14 @@ This file defines a single mixer for a hexacopter in the + configuration. All co
are mixed 100%.
R: 6+ 10000 10000 10000 0
Gimbal / payload mixer for last two channels
-----------------------------------------------------
M: 1
O: 10000 10000 0 -10000 10000
S: 0 6 10000 10000 0 -10000 10000
M: 1
O: 10000 10000 0 -10000 10000
S: 0 7 10000 10000 0 -10000 10000

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@ -5,3 +5,14 @@ This file defines a single mixer for a hexacopter in the X configuration. All c
are mixed 100%.
R: 6x 10000 10000 10000 0
Gimbal / payload mixer for last two channels
-----------------------------------------------------
M: 1
O: 10000 10000 0 -10000 10000
S: 0 6 10000 10000 0 -10000 10000
M: 1
O: 10000 10000 0 -10000 10000
S: 0 7 10000 10000 0 -10000 10000

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@ -5,3 +5,23 @@ This file defines a single mixer for a quadrotor in the + configuration. All con
are mixed 100%.
R: 4+ 10000 10000 10000 0
Gimbal / payload mixer for last four channels
-----------------------------------------------------
M: 1
O: 10000 10000 0 -10000 10000
S: 0 4 10000 10000 0 -10000 10000
M: 1
O: 10000 10000 0 -10000 10000
S: 0 5 10000 10000 0 -10000 10000
M: 1
O: 10000 10000 0 -10000 10000
S: 0 6 10000 10000 0 -10000 10000
M: 1
O: 10000 10000 0 -10000 10000
S: 0 7 10000 10000 0 -10000 10000

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@ -5,3 +5,22 @@ This file defines a single mixer for a quadrotor in the V configuration. All co
are mixed 100%.
R: 4v 10000 10000 10000 0
Gimbal / payload mixer for last four channels
-----------------------------------------------------
M: 1
O: 10000 10000 0 -10000 10000
S: 0 4 10000 10000 0 -10000 10000
M: 1
O: 10000 10000 0 -10000 10000
S: 0 5 10000 10000 0 -10000 10000
M: 1
O: 10000 10000 0 -10000 10000
S: 0 6 10000 10000 0 -10000 10000
M: 1
O: 10000 10000 0 -10000 10000
S: 0 7 10000 10000 0 -10000 10000

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@ -4,3 +4,22 @@ Multirotor mixer for PX4FMU
This file defines a single mixer for a quadrotor with a wide configuration. All controls are mixed 100%.
R: 4w 10000 10000 10000 0
Gimbal / payload mixer for last four channels
-----------------------------------------------------
M: 1
O: 10000 10000 0 -10000 10000
S: 0 4 10000 10000 0 -10000 10000
M: 1
O: 10000 10000 0 -10000 10000
S: 0 5 10000 10000 0 -10000 10000
M: 1
O: 10000 10000 0 -10000 10000
S: 0 6 10000 10000 0 -10000 10000
M: 1
O: 10000 10000 0 -10000 10000
S: 0 7 10000 10000 0 -10000 10000

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@ -5,3 +5,22 @@ This file defines a single mixer for a quadrotor in the X configuration. All co
are mixed 100%.
R: 4x 10000 10000 10000 0
Gimbal / payload mixer for last four channels
-----------------------------------------------------
M: 1
O: 10000 10000 0 -10000 10000
S: 0 4 10000 10000 0 -10000 10000
M: 1
O: 10000 10000 0 -10000 10000
S: 0 5 10000 10000 0 -10000 10000
M: 1
O: 10000 10000 0 -10000 10000
S: 0 6 10000 10000 0 -10000 10000
M: 1
O: 10000 10000 0 -10000 10000
S: 0 7 10000 10000 0 -10000 10000

2
Tools/px4params/.gitignore vendored Normal file
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@ -0,0 +1,2 @@
parameters.wiki
parameters.xml

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@ -0,0 +1,9 @@
h1. PX4 Parameters Processor
It's designed to scan PX4 source codes, find declarations of tunable parameters,
and generate the list in various formats.
Currently supported formats are:
* XML for the parametric UI generator
* Human-readable description in DokuWiki format

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@ -0,0 +1,27 @@
import output
class DokuWikiOutput(output.Output):
def Generate(self, groups):
result = ""
for group in groups:
result += "==== %s ====\n\n" % group.GetName()
for param in group.GetParams():
code = param.GetFieldValue("code")
name = param.GetFieldValue("short_desc")
if code != name:
name = "%s (%s)" % (name, code)
result += "=== %s ===\n\n" % name
long_desc = param.GetFieldValue("long_desc")
if long_desc is not None:
result += "%s\n\n" % long_desc
min_val = param.GetFieldValue("min")
if min_val is not None:
result += "* Minimal value: %s\n" % min_val
max_val = param.GetFieldValue("max")
if max_val is not None:
result += "* Maximal value: %s\n" % max_val
def_val = param.GetFieldValue("default")
if def_val is not None:
result += "* Default value: %s\n" % def_val
result += "\n"
return result

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@ -0,0 +1,5 @@
class Output(object):
def Save(self, groups, fn):
data = self.Generate(groups)
with open(fn, 'w') as f:
f.write(data)

220
Tools/px4params/parser.py Normal file
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@ -0,0 +1,220 @@
import sys
import re
class ParameterGroup(object):
"""
Single parameter group
"""
def __init__(self, name):
self.name = name
self.params = []
def AddParameter(self, param):
"""
Add parameter to the group
"""
self.params.append(param)
def GetName(self):
"""
Get parameter group name
"""
return self.name
def GetParams(self):
"""
Returns the parsed list of parameters. Every parameter is a Parameter
object. Note that returned object is not a copy. Modifications affect
state of the parser.
"""
return sorted(self.params,
cmp=lambda x, y: cmp(x.GetFieldValue("code"),
y.GetFieldValue("code")))
class Parameter(object):
"""
Single parameter
"""
# Define sorting order of the fields
priority = {
"code": 10,
"type": 9,
"short_desc": 8,
"long_desc": 7,
"default": 6,
"min": 5,
"max": 4,
# all others == 0 (sorted alphabetically)
}
def __init__(self):
self.fields = {}
def SetField(self, code, value):
"""
Set named field value
"""
self.fields[code] = value
def GetFieldCodes(self):
"""
Return list of existing field codes in convenient order
"""
return sorted(self.fields.keys(),
cmp=lambda x, y: cmp(self.priority.get(y, 0),
self.priority.get(x, 0)) or cmp(x, y))
def GetFieldValue(self, code):
"""
Return value of the given field code or None if not found.
"""
return self.fields.get(code)
class Parser(object):
"""
Parses provided data and stores all found parameters internally.
"""
re_split_lines = re.compile(r'[\r\n]+')
re_comment_start = re.compile(r'^\/\*\*')
re_comment_content = re.compile(r'^\*\s*(.*)')
re_comment_tag = re.compile(r'@([a-zA-Z][a-zA-Z0-9_]*)\s*(.*)')
re_comment_end = re.compile(r'(.*?)\s*\*\/')
re_parameter_definition = re.compile(r'PARAM_DEFINE_([A-Z_][A-Z0-9_]*)\s*\(([A-Z_][A-Z0-9_]*)\s*,\s*([^ ,\)]+)\s*\)\s*;')
re_cut_type_specifier = re.compile(r'[a-z]+$')
re_is_a_number = re.compile(r'^-?[0-9\.]')
re_remove_dots = re.compile(r'\.+$')
valid_tags = set(["min", "max", "group"])
# Order of parameter groups
priority = {
# All other groups = 0 (sort alphabetically)
"Miscellaneous": -10
}
def __init__(self):
self.param_groups = {}
def GetSupportedExtensions(self):
"""
Returns list of supported file extensions that can be parsed by this
parser.
"""
return ["cpp", "c"]
def Parse(self, contents):
"""
Incrementally parse program contents and append all found parameters
to the list.
"""
# This code is essentially a comment-parsing grammar. "state"
# represents parser state. It contains human-readable state
# names.
state = None
for line in self.re_split_lines.split(contents):
line = line.strip()
# Ignore empty lines
if line == "":
continue
if self.re_comment_start.match(line):
state = "wait-short"
short_desc = None
long_desc = None
tags = {}
elif state is not None and state != "comment-processed":
m = self.re_comment_end.search(line)
if m:
line = m.group(1)
last_comment_line = True
else:
last_comment_line = False
m = self.re_comment_content.match(line)
if m:
comment_content = m.group(1)
if comment_content == "":
# When short comment ends with empty comment line,
# start waiting for the next part - long comment.
if state == "wait-short-end":
state = "wait-long"
else:
m = self.re_comment_tag.match(comment_content)
if m:
tag, desc = m.group(1, 2)
tags[tag] = desc
current_tag = tag
state = "wait-tag-end"
elif state == "wait-short":
# Store first line of the short description
short_desc = comment_content
state = "wait-short-end"
elif state == "wait-short-end":
# Append comment line to the short description
short_desc += "\n" + comment_content
elif state == "wait-long":
# Store first line of the long description
long_desc = comment_content
state = "wait-long-end"
elif state == "wait-long-end":
# Append comment line to the long description
long_desc += "\n" + comment_content
elif state == "wait-tag-end":
# Append comment line to the tag text
tags[current_tag] += "\n" + comment_content
else:
raise AssertionError(
"Invalid parser state: %s" % state)
elif not last_comment_line:
# Invalid comment line (inside comment, but not starting with
# "*" or "*/". Reset parsed content.
state = None
if last_comment_line:
state = "comment-processed"
else:
# Non-empty line outside the comment
m = self.re_parameter_definition.match(line)
if m:
tp, code, defval = m.group(1, 2, 3)
# Remove trailing type specifier from numbers: 0.1f => 0.1
if self.re_is_a_number.match(defval):
defval = self.re_cut_type_specifier.sub('', defval)
param = Parameter()
param.SetField("code", code)
param.SetField("short_desc", code)
param.SetField("type", tp)
param.SetField("default", defval)
# If comment was found before the parameter declaration,
# inject its data into the newly created parameter.
group = "Miscellaneous"
if state == "comment-processed":
if short_desc is not None:
param.SetField("short_desc",
self.re_remove_dots.sub('', short_desc))
if long_desc is not None:
param.SetField("long_desc", long_desc)
for tag in tags:
if tag == "group":
group = tags[tag]
elif tag not in self.valid_tags:
sys.stderr.write("Skipping invalid"
"documentation tag: '%s'\n" % tag)
else:
param.SetField(tag, tags[tag])
# Store the parameter
if group not in self.param_groups:
self.param_groups[group] = ParameterGroup(group)
self.param_groups[group].AddParameter(param)
# Reset parsed comment.
state = None
def GetParamGroups(self):
"""
Returns the parsed list of parameters. Every parameter is a Parameter
object. Note that returned object is not a copy. Modifications affect
state of the parser.
"""
return sorted(self.param_groups.values(),
cmp=lambda x, y: cmp(self.priority.get(y.GetName(), 0),
self.priority.get(x.GetName(), 0)) or cmp(x.GetName(),
y.GetName()))

View File

@ -0,0 +1,61 @@
#!/usr/bin/env python
############################################################################
#
# Copyright (C) 2013 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.
#
############################################################################
#
# PX4 paramers processor (main executable file)
#
# It scans src/ subdirectory of the project, collects all parameters
# definitions, and outputs list of parameters in XML and DokuWiki formats.
#
import scanner
import parser
import xmlout
import dokuwikiout
# Initialize parser
prs = parser.Parser()
# Scan directories, and parse the files
sc = scanner.Scanner()
sc.ScanDir("../../src", prs)
output = prs.GetParamGroups()
# Output into XML
out = xmlout.XMLOutput()
out.Save(output, "parameters.xml")
# Output into DokuWiki
out = dokuwikiout.DokuWikiOutput()
out.Save(output, "parameters.wiki")

View File

@ -0,0 +1,34 @@
import os
import re
class Scanner(object):
"""
Traverses directory tree, reads all source files, and passes their contents
to the Parser.
"""
re_file_extension = re.compile(r'\.([^\.]+)$')
def ScanDir(self, srcdir, parser):
"""
Scans provided path and passes all found contents to the parser using
parser.Parse method.
"""
extensions = set(parser.GetSupportedExtensions())
for dirname, dirnames, filenames in os.walk(srcdir):
for filename in filenames:
m = self.re_file_extension.search(filename)
if m:
ext = m.group(1)
if ext in extensions:
path = os.path.join(dirname, filename)
self.ScanFile(path, parser)
def ScanFile(self, path, parser):
"""
Scans provided file and passes its contents to the parser using
parser.Parse method.
"""
with open(path, 'r') as f:
contents = f.read()
parser.Parse(contents)

22
Tools/px4params/xmlout.py Normal file
View File

@ -0,0 +1,22 @@
import output
from xml.dom.minidom import getDOMImplementation
class XMLOutput(output.Output):
def Generate(self, groups):
impl = getDOMImplementation()
xml_document = impl.createDocument(None, "parameters", None)
xml_parameters = xml_document.documentElement
for group in groups:
xml_group = xml_document.createElement("group")
xml_group.setAttribute("name", group.GetName())
xml_parameters.appendChild(xml_group)
for param in group.GetParams():
xml_param = xml_document.createElement("parameter")
xml_group.appendChild(xml_param)
for code in param.GetFieldCodes():
value = param.GetFieldValue(code)
xml_field = xml_document.createElement(code)
xml_param.appendChild(xml_field)
xml_value = xml_document.createTextNode(value)
xml_field.appendChild(xml_value)
return xml_document.toprettyxml(indent=" ", newl="\n", encoding="utf-8")

View File

@ -25,8 +25,12 @@ import struct, sys
if sys.hexversion >= 0x030000F0:
runningPython3 = True
def _parseCString(cstr):
return str(cstr, 'ascii').split('\0')[0]
else:
runningPython3 = False
def _parseCString(cstr):
return str(cstr).split('\0')[0]
class SDLog2Parser:
BLOCK_SIZE = 8192
@ -175,9 +179,9 @@ class SDLog2Parser:
self.__csv_columns.append(full_label)
self.__csv_data[full_label] = None
if self.__file != None:
print(self.__csv_delim.join(self.__csv_columns), file=self.__file)
print(self.__csv_delim.join(self.__csv_columns), file=self.__file)
else:
print(self.__csv_delim.join(self.__csv_columns))
print(self.__csv_delim.join(self.__csv_columns))
def __printCSVRow(self):
s = []
@ -190,9 +194,9 @@ class SDLog2Parser:
s.append(v)
if self.__file != None:
print(self.__csv_delim.join(s), file=self.__file)
print(self.__csv_delim.join(s), file=self.__file)
else:
print(self.__csv_delim.join(s))
print(self.__csv_delim.join(s))
def __parseMsgDescr(self):
if runningPython3:
@ -202,14 +206,9 @@ class SDLog2Parser:
msg_type = data[0]
if msg_type != self.MSG_TYPE_FORMAT:
msg_length = data[1]
if runningPython3:
msg_name = str(data[2], 'ascii').strip("\0")
msg_format = str(data[3], 'ascii').strip("\0")
msg_labels = str(data[4], 'ascii').strip("\0").split(",")
else:
msg_name = str(data[2]).strip("\0")
msg_format = str(data[3]).strip("\0")
msg_labels = str(data[4]).strip("\0").split(",")
msg_name = _parseCString(data[2])
msg_format = _parseCString(data[3])
msg_labels = _parseCString(data[4]).split(",")
# Convert msg_format to struct.unpack format string
msg_struct = ""
msg_mults = []
@ -243,7 +242,7 @@ class SDLog2Parser:
data = list(struct.unpack(msg_struct, str(self.__buffer[self.__ptr+self.MSG_HEADER_LEN:self.__ptr+msg_length])))
for i in range(len(data)):
if type(data[i]) is str:
data[i] = data[i].strip("\0")
data[i] = _parseCString(data[i])
m = msg_mults[i]
if m != None:
data[i] = data[i] * m

View File

@ -33,7 +33,7 @@ MODULES += drivers/hott/hott_sensors
MODULES += drivers/blinkm
MODULES += drivers/rgbled
MODULES += drivers/mkblctrl
MODULES += drivers/md25
MODULES += drivers/roboclaw
MODULES += drivers/airspeed
MODULES += drivers/ets_airspeed
MODULES += drivers/meas_airspeed
@ -79,7 +79,7 @@ MODULES += examples/flow_position_estimator
#
# Vehicle Control
#
#MODULES += modules/segway # XXX needs state machine update
MODULES += modules/segway
MODULES += modules/fw_pos_control_l1
MODULES += modules/fw_att_control
MODULES += modules/multirotor_att_control
@ -115,6 +115,7 @@ MODULES += lib/mathlib/math/filter
MODULES += lib/ecl
MODULES += lib/external_lgpl
MODULES += lib/geo
MODULES += lib/conversion
#
# Demo apps

View File

@ -31,6 +31,7 @@ MODULES += drivers/hil
MODULES += drivers/hott/hott_telemetry
MODULES += drivers/hott/hott_sensors
MODULES += drivers/blinkm
MODULES += drivers/roboclaw
MODULES += drivers/airspeed
MODULES += drivers/ets_airspeed
MODULES += drivers/meas_airspeed
@ -77,7 +78,7 @@ MODULES += examples/flow_position_estimator
#
# Vehicle Control
#
#MODULES += modules/segway # XXX needs state machine update
MODULES += modules/segway
MODULES += modules/fw_pos_control_l1
MODULES += modules/fw_att_control
MODULES += modules/multirotor_att_control
@ -111,6 +112,7 @@ MODULES += lib/mathlib/math/filter
MODULES += lib/ecl
MODULES += lib/external_lgpl
MODULES += lib/geo
MODULES += lib/conversion
#
# Demo apps

View File

@ -9,6 +9,10 @@
#endif
#include <math.h>
#ifndef M_PI_2
#define M_PI_2 ((float)asin(1))
#endif
/**
* @file mavlink_conversions.h
*
@ -49,12 +53,12 @@ MAVLINK_HELPER void mavlink_dcm_to_euler(const float dcm[3][3], float* roll, flo
float phi, theta, psi;
theta = asin(-dcm[2][0]);
if (fabs(theta - M_PI_2) < 1.0e-3f) {
if (fabsf(theta - (float)M_PI_2) < 1.0e-3f) {
phi = 0.0f;
psi = (atan2(dcm[1][2] - dcm[0][1],
psi = (atan2f(dcm[1][2] - dcm[0][1],
dcm[0][2] + dcm[1][1]) + phi);
} else if (fabs(theta + M_PI_2) < 1.0e-3f) {
} else if (fabsf(theta + (float)M_PI_2) < 1.0e-3f) {
phi = 0.0f;
psi = atan2f(dcm[1][2] - dcm[0][1],
dcm[0][2] + dcm[1][1] - phi);
@ -128,4 +132,4 @@ MAVLINK_HELPER void mavlink_euler_to_dcm(float roll, float pitch, float yaw, flo
dcm[2][2] = cosPhi * cosThe;
}
#endif
#endif

View File

@ -66,7 +66,7 @@ struct accel_report {
int16_t temperature_raw;
};
/** accel scaling factors; Vout = (Vin * Vscale) + Voffset */
/** accel scaling factors; Vout = Vscale * (Vin + Voffset) */
struct accel_scale {
float x_offset;
float x_scale;

View File

@ -132,11 +132,8 @@ ETSAirspeed::measure()
if (OK != ret) {
perf_count(_comms_errors);
log("i2c::transfer returned %d", ret);
return ret;
}
ret = OK;
return ret;
}

View File

@ -138,11 +138,8 @@ MEASAirspeed::measure()
if (OK != ret) {
perf_count(_comms_errors);
return ret;
}
ret = OK;
return ret;
}

View File

@ -172,7 +172,20 @@ RGBLED::probe()
bool on, powersave;
uint8_t r, g, b;
ret = get(on, powersave, r, g, b);
/**
this may look strange, but is needed. There is a serial
EEPROM (Microchip-24aa01) on the PX4FMU-v1 that responds to
a bunch of I2C addresses, including the 0x55 used by this
LED device. So we need to do enough operations to be sure
we are talking to the right device. These 3 operations seem
to be enough, as the 3rd one consistently fails if no
RGBLED is on the bus.
*/
if ((ret=get(on, powersave, r, g, b)) != OK ||
(ret=send_led_enable(false) != OK) ||
(ret=send_led_enable(false) != OK)) {
return ret;
}
return ret;
}
@ -561,7 +574,7 @@ rgbled_main(int argc, char *argv[])
int ch;
/* jump over start/off/etc and look at options first */
while ((ch = getopt(argc - 1, &argv[1], "a:b:")) != EOF) {
while ((ch = getopt(argc, argv, "a:b:")) != EOF) {
switch (ch) {
case 'a':
rgbledadr = strtol(optarg, NULL, 0);
@ -577,7 +590,12 @@ rgbled_main(int argc, char *argv[])
}
}
const char *verb = argv[1];
if (optind >= argc) {
rgbled_usage();
exit(1);
}
const char *verb = argv[optind];
int fd;
int ret;
@ -598,6 +616,9 @@ rgbled_main(int argc, char *argv[])
if (g_rgbled == nullptr) {
// fall back to default bus
if (PX4_I2C_BUS_LED == PX4_I2C_BUS_EXPANSION) {
errx(1, "init failed");
}
i2cdevice = PX4_I2C_BUS_LED;
}
}

View File

@ -0,0 +1,328 @@
/****************************************************************************
*
* Copyright (c) 2013 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.
*
****************************************************************************/
/**
* @file RoboClaw.cpp
*
* RoboClaw Motor Driver
*
* references:
* http://downloads.orionrobotics.com/downloads/datasheets/motor_controller_robo_claw_R0401.pdf
*
*/
#include "RoboClaw.hpp"
#include <poll.h>
#include <stdio.h>
#include <math.h>
#include <string.h>
#include <fcntl.h>
#include <termios.h>
#include <systemlib/err.h>
#include <arch/board/board.h>
#include <mavlink/mavlink_log.h>
#include <controllib/uorb/UOrbPublication.hpp>
#include <uORB/topics/debug_key_value.h>
#include <drivers/drv_hrt.h>
uint8_t RoboClaw::checksum_mask = 0x7f;
RoboClaw::RoboClaw(const char *deviceName, uint16_t address,
uint16_t pulsesPerRev):
_address(address),
_pulsesPerRev(pulsesPerRev),
_uart(0),
_controlPoll(),
_actuators(NULL, ORB_ID(actuator_controls_0), 20),
_motor1Position(0),
_motor1Speed(0),
_motor1Overflow(0),
_motor2Position(0),
_motor2Speed(0),
_motor2Overflow(0)
{
// setup control polling
_controlPoll.fd = _actuators.getHandle();
_controlPoll.events = POLLIN;
// start serial port
_uart = open(deviceName, O_RDWR | O_NOCTTY);
if (_uart < 0) err(1, "could not open %s", deviceName);
int ret = 0;
struct termios uart_config;
ret = tcgetattr(_uart, &uart_config);
if (ret < 0) err (1, "failed to get attr");
uart_config.c_oflag &= ~ONLCR; // no CR for every LF
ret = cfsetispeed(&uart_config, B38400);
if (ret < 0) err (1, "failed to set input speed");
ret = cfsetospeed(&uart_config, B38400);
if (ret < 0) err (1, "failed to set output speed");
ret = tcsetattr(_uart, TCSANOW, &uart_config);
if (ret < 0) err (1, "failed to set attr");
// setup default settings, reset encoders
resetEncoders();
}
RoboClaw::~RoboClaw()
{
setMotorDutyCycle(MOTOR_1, 0.0);
setMotorDutyCycle(MOTOR_2, 0.0);
close(_uart);
}
int RoboClaw::readEncoder(e_motor motor)
{
uint16_t sum = 0;
if (motor == MOTOR_1) {
_sendCommand(CMD_READ_ENCODER_1, nullptr, 0, sum);
} else if (motor == MOTOR_2) {
_sendCommand(CMD_READ_ENCODER_2, nullptr, 0, sum);
}
uint8_t rbuf[50];
usleep(5000);
int nread = read(_uart, rbuf, 50);
if (nread < 6) {
printf("failed to read\n");
return -1;
}
//printf("received: \n");
//for (int i=0;i<nread;i++) {
//printf("%d\t", rbuf[i]);
//}
//printf("\n");
uint32_t count = 0;
uint8_t * countBytes = (uint8_t *)(&count);
countBytes[3] = rbuf[0];
countBytes[2] = rbuf[1];
countBytes[1] = rbuf[2];
countBytes[0] = rbuf[3];
uint8_t status = rbuf[4];
uint8_t checksum = rbuf[5];
uint8_t checksum_computed = (sum + _sumBytes(rbuf, 5)) &
checksum_mask;
// check if checksum is valid
if (checksum != checksum_computed) {
printf("checksum failed: expected %d got %d\n",
checksum, checksum_computed);
return -1;
}
int overFlow = 0;
if (status & STATUS_REVERSE) {
//printf("roboclaw: reverse\n");
}
if (status & STATUS_UNDERFLOW) {
//printf("roboclaw: underflow\n");
overFlow = -1;
} else if (status & STATUS_OVERFLOW) {
//printf("roboclaw: overflow\n");
overFlow = +1;
}
static int64_t overflowAmount = 0x100000000LL;
if (motor == MOTOR_1) {
_motor1Overflow += overFlow;
_motor1Position = float(int64_t(count) +
_motor1Overflow*overflowAmount)/_pulsesPerRev;
} else if (motor == MOTOR_2) {
_motor2Overflow += overFlow;
_motor2Position = float(int64_t(count) +
_motor2Overflow*overflowAmount)/_pulsesPerRev;
}
return 0;
}
void RoboClaw::printStatus(char *string, size_t n)
{
snprintf(string, n,
"pos1,spd1,pos2,spd2: %10.2f %10.2f %10.2f %10.2f\n",
double(getMotorPosition(MOTOR_1)),
double(getMotorSpeed(MOTOR_1)),
double(getMotorPosition(MOTOR_2)),
double(getMotorSpeed(MOTOR_2)));
}
float RoboClaw::getMotorPosition(e_motor motor)
{
if (motor == MOTOR_1) {
return _motor1Position;
} else if (motor == MOTOR_2) {
return _motor2Position;
}
}
float RoboClaw::getMotorSpeed(e_motor motor)
{
if (motor == MOTOR_1) {
return _motor1Speed;
} else if (motor == MOTOR_2) {
return _motor2Speed;
}
}
int RoboClaw::setMotorSpeed(e_motor motor, float value)
{
uint16_t sum = 0;
// bound
if (value > 1) value = 1;
if (value < -1) value = -1;
uint8_t speed = fabs(value)*127;
// send command
if (motor == MOTOR_1) {
if (value > 0) {
return _sendCommand(CMD_DRIVE_FWD_1, &speed, 1, sum);
} else {
return _sendCommand(CMD_DRIVE_REV_1, &speed, 1, sum);
}
} else if (motor == MOTOR_2) {
if (value > 0) {
return _sendCommand(CMD_DRIVE_FWD_2, &speed, 1, sum);
} else {
return _sendCommand(CMD_DRIVE_REV_2, &speed, 1, sum);
}
}
return -1;
}
int RoboClaw::setMotorDutyCycle(e_motor motor, float value)
{
uint16_t sum = 0;
// bound
if (value > 1) value = 1;
if (value < -1) value = -1;
int16_t duty = 1500*value;
// send command
if (motor == MOTOR_1) {
return _sendCommand(CMD_SIGNED_DUTYCYCLE_1,
(uint8_t *)(&duty), 2, sum);
} else if (motor == MOTOR_2) {
return _sendCommand(CMD_SIGNED_DUTYCYCLE_2,
(uint8_t *)(&duty), 2, sum);
}
return -1;
}
int RoboClaw::resetEncoders()
{
uint16_t sum = 0;
return _sendCommand(CMD_RESET_ENCODERS,
nullptr, 0, sum);
}
int RoboClaw::update()
{
// wait for an actuator publication,
// check for exit condition every second
// note "::poll" is required to distinguish global
// poll from member function for driver
if (::poll(&_controlPoll, 1, 1000) < 0) return -1; // poll error
// if new data, send to motors
if (_actuators.updated()) {
_actuators.update();
setMotorDutyCycle(MOTOR_1,_actuators.control[CH_VOLTAGE_LEFT]);
setMotorDutyCycle(MOTOR_2,_actuators.control[CH_VOLTAGE_RIGHT]);
}
return 0;
}
uint16_t RoboClaw::_sumBytes(uint8_t * buf, size_t n)
{
uint16_t sum = 0;
//printf("sum\n");
for (size_t i=0;i<n;i++) {
sum += buf[i];
//printf("%d\t", buf[i]);
}
//printf("total sum %d\n", sum);
return sum;
}
int RoboClaw::_sendCommand(e_command cmd, uint8_t * data,
size_t n_data, uint16_t & prev_sum)
{
tcflush(_uart, TCIOFLUSH); // flush buffers
uint8_t buf[n_data + 3];
buf[0] = _address;
buf[1] = cmd;
for (size_t i=0;i<n_data;i++) {
buf[i+2] = data[n_data - i - 1]; // MSB
}
uint16_t sum = _sumBytes(buf, n_data + 2);
prev_sum += sum;
buf[n_data + 2] = sum & checksum_mask;
//printf("\nmessage:\n");
//for (size_t i=0;i<n_data+3;i++) {
//printf("%d\t", buf[i]);
//}
//printf("\n");
return write(_uart, buf, n_data + 3);
}
int roboclawTest(const char *deviceName, uint8_t address,
uint16_t pulsesPerRev)
{
printf("roboclaw test: starting\n");
// setup
RoboClaw roboclaw(deviceName, address, pulsesPerRev);
roboclaw.setMotorDutyCycle(RoboClaw::MOTOR_1, 0.3);
roboclaw.setMotorDutyCycle(RoboClaw::MOTOR_2, 0.3);
char buf[200];
for (int i=0; i<10; i++) {
usleep(100000);
roboclaw.readEncoder(RoboClaw::MOTOR_1);
roboclaw.readEncoder(RoboClaw::MOTOR_2);
roboclaw.printStatus(buf,200);
printf("%s", buf);
}
roboclaw.setMotorDutyCycle(RoboClaw::MOTOR_1, -0.3);
roboclaw.setMotorDutyCycle(RoboClaw::MOTOR_2, -0.3);
for (int i=0; i<10; i++) {
usleep(100000);
roboclaw.readEncoder(RoboClaw::MOTOR_1);
roboclaw.readEncoder(RoboClaw::MOTOR_2);
roboclaw.printStatus(buf,200);
printf("%s", buf);
}
printf("Test complete\n");
return 0;
}
// vi:noet:smarttab:autoindent:ts=4:sw=4:tw=78

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@ -0,0 +1,192 @@
/****************************************************************************
*
* Copyright (C) 2013 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.
*
****************************************************************************/
/**
* @file RoboClas.hpp
*
* RoboClaw Motor Driver
*
* references:
* http://downloads.orionrobotics.com/downloads/datasheets/motor_controller_robo_claw_R0401.pdf
*
*/
#pragma once
#include <poll.h>
#include <stdio.h>
#include <controllib/uorb/UOrbSubscription.hpp>
#include <uORB/topics/actuator_controls.h>
#include <drivers/device/i2c.h>
/**
* This is a driver for the RoboClaw motor controller
*/
class RoboClaw
{
public:
/** control channels */
enum e_channel {
CH_VOLTAGE_LEFT = 0,
CH_VOLTAGE_RIGHT
};
/** motors */
enum e_motor {
MOTOR_1 = 0,
MOTOR_2
};
/**
* constructor
* @param deviceName the name of the
* serial port e.g. "/dev/ttyS2"
* @param address the adddress of the motor
* (selectable on roboclaw)
* @param pulsesPerRev # of encoder
* pulses per revolution of wheel
*/
RoboClaw(const char *deviceName, uint16_t address,
uint16_t pulsesPerRev);
/**
* deconstructor
*/
virtual ~RoboClaw();
/**
* @return position of a motor, rev
*/
float getMotorPosition(e_motor motor);
/**
* @return speed of a motor, rev/sec
*/
float getMotorSpeed(e_motor motor);
/**
* set the speed of a motor, rev/sec
*/
int setMotorSpeed(e_motor motor, float value);
/**
* set the duty cycle of a motor, rev/sec
*/
int setMotorDutyCycle(e_motor motor, float value);
/**
* reset the encoders
* @return status
*/
int resetEncoders();
/**
* main update loop that updates RoboClaw motor
* dutycycle based on actuator publication
*/
int update();
/**
* read data from serial
*/
int readEncoder(e_motor motor);
/**
* print status
*/
void printStatus(char *string, size_t n);
private:
// Quadrature status flags
enum e_quadrature_status_flags {
STATUS_UNDERFLOW = 1 << 0, /**< encoder went below 0 **/
STATUS_REVERSE = 1 << 1, /**< motor doing in reverse dir **/
STATUS_OVERFLOW = 1 << 2, /**< encoder went above 2^32 **/
};
// commands
// We just list the commands we want from the manual here.
enum e_command {
// simple
CMD_DRIVE_FWD_1 = 0,
CMD_DRIVE_REV_1 = 1,
CMD_DRIVE_FWD_2 = 4,
CMD_DRIVE_REV_2 = 5,
// encoder commands
CMD_READ_ENCODER_1 = 16,
CMD_READ_ENCODER_2 = 17,
CMD_RESET_ENCODERS = 20,
// advanced motor control
CMD_READ_SPEED_HIRES_1 = 30,
CMD_READ_SPEED_HIRES_2 = 31,
CMD_SIGNED_DUTYCYCLE_1 = 32,
CMD_SIGNED_DUTYCYCLE_2 = 33,
};
static uint8_t checksum_mask;
uint16_t _address;
uint16_t _pulsesPerRev;
int _uart;
/** poll structure for control packets */
struct pollfd _controlPoll;
/** actuator controls subscription */
control::UOrbSubscription<actuator_controls_s> _actuators;
// private data
float _motor1Position;
float _motor1Speed;
int16_t _motor1Overflow;
float _motor2Position;
float _motor2Speed;
int16_t _motor2Overflow;
// private methods
uint16_t _sumBytes(uint8_t * buf, size_t n);
int _sendCommand(e_command cmd, uint8_t * data, size_t n_data, uint16_t & prev_sum);
};
// unit testing
int roboclawTest(const char *deviceName, uint8_t address,
uint16_t pulsesPerRev);
// vi:noet:smarttab:autoindent:ts=4:sw=4:tw=78

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@ -0,0 +1,41 @@
############################################################################
#
# Copyright (c) 2013 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.
#
############################################################################
#
# RoboClaw Motor Controller
#
MODULE_COMMAND = roboclaw
SRCS = roboclaw_main.cpp \
RoboClaw.cpp

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@ -0,0 +1,195 @@
/****************************************************************************
*
* Copyright (c) 2013 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.
*
****************************************************************************/
/**
* @ file roboclaw_main.cpp
*
* RoboClaw Motor Driver
*
* references:
* http://downloads.orionrobotics.com/downloads/datasheets/motor_controller_robo_claw_R0401.pdf
*
*/
#include <nuttx/config.h>
#include <unistd.h>
#include <stdio.h>
#include <stdlib.h>
#include <string.h>
#include <math.h>
#include <systemlib/systemlib.h>
#include <systemlib/param/param.h>
#include <arch/board/board.h>
#include "RoboClaw.hpp"
static bool thread_should_exit = false; /**< Deamon exit flag */
static bool thread_running = false; /**< Deamon status flag */
static int deamon_task; /**< Handle of deamon task / thread */
/**
* Deamon management function.
*/
extern "C" __EXPORT int roboclaw_main(int argc, char *argv[]);
/**
* Mainloop of deamon.
*/
int roboclaw_thread_main(int argc, char *argv[]);
/**
* Print the correct usage.
*/
static void usage();
static void usage()
{
fprintf(stderr, "usage: roboclaw "
"{start|stop|status|test}\n\n");
}
/**
* The deamon app only briefly exists to start
* the background job. The stack size assigned in the
* Makefile does only apply to this management task.
*
* The actual stack size should be set in the call
* to task_create().
*/
int roboclaw_main(int argc, char *argv[])
{
if (argc < 1)
usage();
if (!strcmp(argv[1], "start")) {
if (thread_running) {
printf("roboclaw already running\n");
/* this is not an error */
exit(0);
}
thread_should_exit = false;
deamon_task = task_spawn_cmd("roboclaw",
SCHED_DEFAULT,
SCHED_PRIORITY_MAX - 10,
2048,
roboclaw_thread_main,
(const char **)argv);
exit(0);
} else if (!strcmp(argv[1], "test")) {
const char * deviceName = "/dev/ttyS2";
uint8_t address = 128;
uint16_t pulsesPerRev = 1200;
if (argc == 2) {
printf("testing with default settings\n");
} else if (argc != 4) {
printf("usage: roboclaw test device address pulses_per_rev\n");
exit(-1);
} else {
deviceName = argv[2];
address = strtoul(argv[3], nullptr, 0);
pulsesPerRev = strtoul(argv[4], nullptr, 0);
}
printf("device:\t%s\taddress:\t%d\tpulses per rev:\t%ld\n",
deviceName, address, pulsesPerRev);
roboclawTest(deviceName, address, pulsesPerRev);
thread_should_exit = true;
exit(0);
} else if (!strcmp(argv[1], "stop")) {
thread_should_exit = true;
exit(0);
} else if (!strcmp(argv[1], "status")) {
if (thread_running) {
printf("\troboclaw app is running\n");
} else {
printf("\troboclaw app not started\n");
}
exit(0);
}
usage();
exit(1);
}
int roboclaw_thread_main(int argc, char *argv[])
{
printf("[roboclaw] starting\n");
// skip parent process args
argc -=2;
argv +=2;
if (argc < 3) {
printf("usage: roboclaw start device address\n");
return -1;
}
const char *deviceName = argv[1];
uint8_t address = strtoul(argv[2], nullptr, 0);
uint16_t pulsesPerRev = strtoul(argv[3], nullptr, 0);
printf("device:\t%s\taddress:\t%d\tpulses per rev:\t%ld\n",
deviceName, address, pulsesPerRev);
// start
RoboClaw roboclaw(deviceName, address, pulsesPerRev);
thread_running = true;
// loop
while (!thread_should_exit) {
roboclaw.update();
}
// exit
printf("[roboclaw] exiting.\n");
thread_running = false;
return 0;
}
// vi:noet:smarttab:autoindent:ts=4:sw=4:tw=78

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@ -0,0 +1,38 @@
############################################################################
#
# Copyright (C) 2013 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.
#
############################################################################
#
# Conversion library
#
SRCS = rotation.cpp

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@ -0,0 +1,62 @@
/****************************************************************************
*
* Copyright (C) 2013 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.
*
****************************************************************************/
/**
* @file rotation.cpp
*
* Vector rotation library
*/
#include "math.h"
#include "rotation.h"
__EXPORT void
get_rot_matrix(enum Rotation rot, math::Matrix *rot_matrix)
{
/* first set to zero */
rot_matrix->Matrix::zero(3, 3);
float roll = M_DEG_TO_RAD_F * (float)rot_lookup[rot].roll;
float pitch = M_DEG_TO_RAD_F * (float)rot_lookup[rot].pitch;
float yaw = M_DEG_TO_RAD_F * (float)rot_lookup[rot].yaw;
math::EulerAngles euler(roll, pitch, yaw);
math::Dcm R(euler);
for (int i = 0; i < 3; i++) {
for (int j = 0; j < 3; j++) {
(*rot_matrix)(i, j) = R(i, j);
}
}
}

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@ -0,0 +1,121 @@
/****************************************************************************
*
* Copyright (C) 2013 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.
*
****************************************************************************/
/**
* @file rotation.h
*
* Vector rotation library
*/
#ifndef ROTATION_H_
#define ROTATION_H_
#include <unistd.h>
#include <mathlib/mathlib.h>
/**
* Enum for board and external compass rotations.
* This enum maps from board attitude to airframe attitude.
*/
enum Rotation {
ROTATION_NONE = 0,
ROTATION_YAW_45 = 1,
ROTATION_YAW_90 = 2,
ROTATION_YAW_135 = 3,
ROTATION_YAW_180 = 4,
ROTATION_YAW_225 = 5,
ROTATION_YAW_270 = 6,
ROTATION_YAW_315 = 7,
ROTATION_ROLL_180 = 8,
ROTATION_ROLL_180_YAW_45 = 9,
ROTATION_ROLL_180_YAW_90 = 10,
ROTATION_ROLL_180_YAW_135 = 11,
ROTATION_PITCH_180 = 12,
ROTATION_ROLL_180_YAW_225 = 13,
ROTATION_ROLL_180_YAW_270 = 14,
ROTATION_ROLL_180_YAW_315 = 15,
ROTATION_ROLL_90 = 16,
ROTATION_ROLL_90_YAW_45 = 17,
ROTATION_ROLL_90_YAW_90 = 18,
ROTATION_ROLL_90_YAW_135 = 19,
ROTATION_ROLL_270 = 20,
ROTATION_ROLL_270_YAW_45 = 21,
ROTATION_ROLL_270_YAW_90 = 22,
ROTATION_ROLL_270_YAW_135 = 23,
ROTATION_PITCH_90 = 24,
ROTATION_PITCH_270 = 25,
ROTATION_MAX
};
typedef struct {
uint16_t roll;
uint16_t pitch;
uint16_t yaw;
} rot_lookup_t;
const rot_lookup_t rot_lookup[] = {
{ 0, 0, 0 },
{ 0, 0, 45 },
{ 0, 0, 90 },
{ 0, 0, 135 },
{ 0, 0, 180 },
{ 0, 0, 225 },
{ 0, 0, 270 },
{ 0, 0, 315 },
{180, 0, 0 },
{180, 0, 45 },
{180, 0, 90 },
{180, 0, 135 },
{ 0, 180, 0 },
{180, 0, 225 },
{180, 0, 270 },
{180, 0, 315 },
{ 90, 0, 0 },
{ 90, 0, 45 },
{ 90, 0, 90 },
{ 90, 0, 135 },
{270, 0, 0 },
{270, 0, 45 },
{270, 0, 90 },
{270, 0, 135 },
{ 0, 90, 0 },
{ 0, 270, 0 }
};
/**
* Get the rotation matrix
*/
__EXPORT void
get_rot_matrix(enum Rotation rot, math::Matrix *rot_matrix);
#endif /* ROTATION_H_ */

View File

@ -43,7 +43,7 @@
float ECL_L1_Pos_Controller::nav_roll()
{
float ret = atanf(_lateral_accel * 1.0f / CONSTANTS_ONE_G);
ret = math::constrain(ret, (-M_PI_F) / 2.0f, M_PI_F / 2.0f);
ret = math::constrain(ret, -_roll_lim_rad, _roll_lim_rad);
return ret;
}

View File

@ -222,6 +222,15 @@ public:
_K_L1 = 4.0f * _L1_damping * _L1_damping;
}
/**
* Set the maximum roll angle output in radians
*
*/
void set_l1_roll_limit(float roll_lim_rad) {
_roll_lim_rad = roll_lim_rad;
}
private:
float _lateral_accel; ///< Lateral acceleration setpoint in m/s^2
@ -238,6 +247,8 @@ private:
float _K_L1; ///< L1 control gain for _L1_damping
float _heading_omega; ///< Normalized frequency
float _roll_lim_rad; ///<maximum roll angle
/**
* Convert a 2D vector from WGS84 to planar coordinates.
*

View File

@ -100,10 +100,29 @@
* accel_T = A^-1 * g
* g = 9.80665
*
* ===== Rotation =====
*
* Calibrating using model:
* accel_corr = accel_T_r * (rot * accel_raw - accel_offs_r)
*
* Actual correction:
* accel_corr = rot * accel_T * (accel_raw - accel_offs)
*
* Known: accel_T_r, accel_offs_r, rot
* Unknown: accel_T, accel_offs
*
* Solution:
* accel_T_r * (rot * accel_raw - accel_offs_r) = rot * accel_T * (accel_raw - accel_offs)
* rot^-1 * accel_T_r * (rot * accel_raw - accel_offs_r) = accel_T * (accel_raw - accel_offs)
* rot^-1 * accel_T_r * rot * accel_raw - rot^-1 * accel_T_r * accel_offs_r = accel_T * accel_raw - accel_T * accel_offs)
* => accel_T = rot^-1 * accel_T_r * rot
* => accel_offs = rot^-1 * accel_offs_r
*
* @author Anton Babushkin <anton.babushkin@me.com>
*/
#include "accelerometer_calibration.h"
#include "calibration_messages.h"
#include "commander_helper.h"
#include <unistd.h>
@ -112,11 +131,13 @@
#include <fcntl.h>
#include <sys/prctl.h>
#include <math.h>
#include <mathlib/mathlib.h>
#include <string.h>
#include <drivers/drv_hrt.h>
#include <uORB/topics/sensor_combined.h>
#include <drivers/drv_accel.h>
#include <geo/geo.h>
#include <conversion/rotation.h>
#include <systemlib/param/param.h>
#include <systemlib/err.h>
#include <mavlink/mavlink_log.h>
@ -127,75 +148,19 @@
#endif
static const int ERROR = -1;
int do_accel_calibration_measurements(int mavlink_fd, float accel_offs[3], float accel_scale[3]);
static const char *sensor_name = "accel";
int do_accel_calibration_measurements(int mavlink_fd, float accel_offs[3], float accel_T[3][3]);
int detect_orientation(int mavlink_fd, int sub_sensor_combined);
int read_accelerometer_avg(int sensor_combined_sub, float accel_avg[3], int samples_num);
int mat_invert3(float src[3][3], float dst[3][3]);
int calculate_calibration_values(float accel_ref[6][3], float accel_T[3][3], float accel_offs[3], float g);
int do_accel_calibration(int mavlink_fd) {
/* announce change */
mavlink_log_info(mavlink_fd, "accel calibration started");
mavlink_log_info(mavlink_fd, "accel cal progress <0> percent");
int do_accel_calibration(int mavlink_fd)
{
mavlink_log_info(mavlink_fd, CAL_STARTED_MSG, sensor_name);
/* measure and calculate offsets & scales */
float accel_offs[3];
float accel_scale[3];
int res = do_accel_calibration_measurements(mavlink_fd, accel_offs, accel_scale);
if (res == OK) {
/* measurements complete successfully, set parameters */
if (param_set(param_find("SENS_ACC_XOFF"), &(accel_offs[0]))
|| param_set(param_find("SENS_ACC_YOFF"), &(accel_offs[1]))
|| param_set(param_find("SENS_ACC_ZOFF"), &(accel_offs[2]))
|| param_set(param_find("SENS_ACC_XSCALE"), &(accel_scale[0]))
|| param_set(param_find("SENS_ACC_YSCALE"), &(accel_scale[1]))
|| param_set(param_find("SENS_ACC_ZSCALE"), &(accel_scale[2]))) {
mavlink_log_critical(mavlink_fd, "ERROR: setting offs or scale failed");
}
int fd = open(ACCEL_DEVICE_PATH, 0);
struct accel_scale ascale = {
accel_offs[0],
accel_scale[0],
accel_offs[1],
accel_scale[1],
accel_offs[2],
accel_scale[2],
};
if (OK != ioctl(fd, ACCELIOCSSCALE, (long unsigned int)&ascale))
warn("WARNING: failed to set scale / offsets for accel");
close(fd);
/* auto-save to EEPROM */
int save_ret = param_save_default();
if (save_ret != 0) {
warn("WARNING: auto-save of params to storage failed");
}
mavlink_log_info(mavlink_fd, "accel calibration done");
return OK;
} else {
/* measurements error */
mavlink_log_info(mavlink_fd, "accel calibration aborted");
return ERROR;
}
/* exit accel calibration mode */
}
int do_accel_calibration_measurements(int mavlink_fd, float accel_offs[3], float accel_scale[3]) {
const int samples_num = 2500;
float accel_ref[6][3];
bool data_collected[6] = { false, false, false, false, false, false };
const char *orientation_strs[6] = { "x+", "x-", "y+", "y-", "z+", "z-" };
/* reset existing calibration */
int fd = open(ACCEL_DEVICE_PATH, 0);
struct accel_scale ascale_null = {
struct accel_scale accel_scale = {
0.0f,
1.0f,
0.0f,
@ -203,17 +168,102 @@ int do_accel_calibration_measurements(int mavlink_fd, float accel_offs[3], float
0.0f,
1.0f,
};
int ioctl_res = ioctl(fd, ACCELIOCSSCALE, (long unsigned int)&ascale_null);
int res = OK;
/* reset all offsets to zero and all scales to one */
int fd = open(ACCEL_DEVICE_PATH, 0);
res = ioctl(fd, ACCELIOCSSCALE, (long unsigned int)&accel_scale);
close(fd);
if (OK != ioctl_res) {
warn("ERROR: failed to set scale / offsets for accel");
return ERROR;
if (res != OK) {
mavlink_log_critical(mavlink_fd, CAL_FAILED_RESET_CAL_MSG);
}
float accel_offs[3];
float accel_T[3][3];
if (res == OK) {
/* measure and calculate offsets & scales */
res = do_accel_calibration_measurements(mavlink_fd, accel_offs, accel_T);
}
if (res == OK) {
/* measurements completed successfully, rotate calibration values */
param_t board_rotation_h = param_find("SENS_BOARD_ROT");
int32_t board_rotation_int;
param_get(board_rotation_h, &(board_rotation_int));
enum Rotation board_rotation_id = (enum Rotation)board_rotation_int;
math::Matrix board_rotation(3, 3);
get_rot_matrix(board_rotation_id, &board_rotation);
math::Matrix board_rotation_t = board_rotation.transpose();
math::Vector3 accel_offs_vec;
accel_offs_vec.set(&accel_offs[0]);
math::Vector3 accel_offs_rotated = board_rotation_t * accel_offs_vec;
math::Matrix accel_T_mat(3, 3);
accel_T_mat.set(&accel_T[0][0]);
math::Matrix accel_T_rotated = board_rotation_t * accel_T_mat * board_rotation;
accel_scale.x_offset = accel_offs_rotated(0);
accel_scale.x_scale = accel_T_rotated(0, 0);
accel_scale.y_offset = accel_offs_rotated(1);
accel_scale.y_scale = accel_T_rotated(1, 1);
accel_scale.z_offset = accel_offs_rotated(2);
accel_scale.z_scale = accel_T_rotated(2, 2);
/* set parameters */
if (param_set(param_find("SENS_ACC_XOFF"), &(accel_scale.x_offset))
|| param_set(param_find("SENS_ACC_YOFF"), &(accel_scale.y_offset))
|| param_set(param_find("SENS_ACC_ZOFF"), &(accel_scale.z_offset))
|| param_set(param_find("SENS_ACC_XSCALE"), &(accel_scale.x_scale))
|| param_set(param_find("SENS_ACC_YSCALE"), &(accel_scale.y_scale))
|| param_set(param_find("SENS_ACC_ZSCALE"), &(accel_scale.z_scale))) {
mavlink_log_critical(mavlink_fd, CAL_FAILED_SET_PARAMS_MSG);
res = ERROR;
}
}
if (res == OK) {
/* apply new scaling and offsets */
int fd = open(ACCEL_DEVICE_PATH, 0);
res = ioctl(fd, ACCELIOCSSCALE, (long unsigned int)&accel_scale);
close(fd);
if (res != OK) {
mavlink_log_critical(mavlink_fd, CAL_FAILED_APPLY_CAL_MSG);
}
}
if (res == OK) {
/* auto-save to EEPROM */
res = param_save_default();
if (res != OK) {
mavlink_log_critical(mavlink_fd, CAL_FAILED_SAVE_PARAMS_MSG);
}
}
if (res == OK) {
mavlink_log_info(mavlink_fd, CAL_DONE_MSG, sensor_name);
} else {
mavlink_log_info(mavlink_fd, CAL_FAILED_MSG, sensor_name);
}
return res;
}
int do_accel_calibration_measurements(int mavlink_fd, float accel_offs[3], float accel_T[3][3])
{
const int samples_num = 2500;
float accel_ref[6][3];
bool data_collected[6] = { false, false, false, false, false, false };
const char *orientation_strs[6] = { "x+", "x-", "y+", "y-", "z+", "z-" };
int sensor_combined_sub = orb_subscribe(ORB_ID(sensor_combined));
unsigned done_count = 0;
int res = OK;
while (true) {
bool done = true;
@ -221,64 +271,63 @@ int do_accel_calibration_measurements(int mavlink_fd, float accel_offs[3], float
done_count = 0;
for (int i = 0; i < 6; i++) {
if (!data_collected[i]) {
if (data_collected[i]) {
done_count++;
} else {
done = false;
}
}
mavlink_log_info(mavlink_fd, "directions left: %s%s%s%s%s%s",
(!data_collected[0]) ? "x+ " : "",
(!data_collected[1]) ? "x- " : "",
(!data_collected[2]) ? "y+ " : "",
(!data_collected[3]) ? "y- " : "",
(!data_collected[4]) ? "z+ " : "",
(!data_collected[5]) ? "z- " : "");
if (old_done_count != done_count)
mavlink_log_info(mavlink_fd, "accel cal progress <%u> percent", 17 * done_count);
mavlink_log_info(mavlink_fd, CAL_PROGRESS_MSG, sensor_name, 17 * done_count);
if (done)
break;
mavlink_log_info(mavlink_fd, "directions left: %s%s%s%s%s%s",
(!data_collected[0]) ? "x+ " : "",
(!data_collected[1]) ? "x- " : "",
(!data_collected[2]) ? "y+ " : "",
(!data_collected[3]) ? "y- " : "",
(!data_collected[4]) ? "z+ " : "",
(!data_collected[5]) ? "z- " : "");
int orient = detect_orientation(mavlink_fd, sensor_combined_sub);
if (orient < 0) {
close(sensor_combined_sub);
return ERROR;
res = ERROR;
break;
}
if (data_collected[orient]) {
mavlink_log_info(mavlink_fd, "%s done, please rotate to a different axis", orientation_strs[orient]);
mavlink_log_info(mavlink_fd, "%s done, rotate to a different axis", orientation_strs[orient]);
continue;
}
mavlink_log_info(mavlink_fd, "accel measurement started: %s axis", orientation_strs[orient]);
read_accelerometer_avg(sensor_combined_sub, &(accel_ref[orient][0]), samples_num);
mavlink_log_info(mavlink_fd, "result for %s axis: [ %.2f %.2f %.2f ]", orientation_strs[orient],
(double)accel_ref[orient][0],
(double)accel_ref[orient][1],
(double)accel_ref[orient][2]);
(double)accel_ref[orient][0],
(double)accel_ref[orient][1],
(double)accel_ref[orient][2]);
data_collected[orient] = true;
tune_neutral();
}
close(sensor_combined_sub);
/* calculate offsets and rotation+scale matrix */
float accel_T[3][3];
int res = calculate_calibration_values(accel_ref, accel_T, accel_offs, CONSTANTS_ONE_G);
if (res != 0) {
mavlink_log_info(mavlink_fd, "ERROR: calibration values calculation error");
return ERROR;
if (res == OK) {
/* calculate offsets and transform matrix */
res = calculate_calibration_values(accel_ref, accel_T, accel_offs, CONSTANTS_ONE_G);
if (res != OK) {
mavlink_log_info(mavlink_fd, "ERROR: calibration values calculation error");
}
}
/* convert accel transform matrix to scales,
* rotation part of transform matrix is not used by now
*/
for (int i = 0; i < 3; i++) {
accel_scale[i] = accel_T[i][i];
}
return OK;
return res;
}
/*
@ -287,14 +336,15 @@ int do_accel_calibration_measurements(int mavlink_fd, float accel_offs[3], float
* @return 0..5 according to orientation when vehicle is still and ready for measurements,
* ERROR if vehicle is not still after 30s or orientation error is more than 5m/s^2
*/
int detect_orientation(int mavlink_fd, int sub_sensor_combined) {
int detect_orientation(int mavlink_fd, int sub_sensor_combined)
{
struct sensor_combined_s sensor;
/* exponential moving average of accel */
float accel_ema[3] = { 0.0f, 0.0f, 0.0f };
/* max-hold dispersion of accel */
float accel_disp[3] = { 0.0f, 0.0f, 0.0f };
/* EMA time constant in seconds*/
float ema_len = 0.2f;
float ema_len = 0.5f;
/* set "still" threshold to 0.25 m/s^2 */
float still_thr2 = pow(0.25f, 2);
/* set accel error threshold to 5m/s^2 */
@ -318,30 +368,38 @@ int detect_orientation(int mavlink_fd, int sub_sensor_combined) {
while (true) {
/* wait blocking for new data */
int poll_ret = poll(fds, 1, 1000);
if (poll_ret) {
orb_copy(ORB_ID(sensor_combined), sub_sensor_combined, &sensor);
t = hrt_absolute_time();
float dt = (t - t_prev) / 1000000.0f;
t_prev = t;
float w = dt / ema_len;
for (int i = 0; i < 3; i++) {
accel_ema[i] = accel_ema[i] * (1.0f - w) + sensor.accelerometer_m_s2[i] * w;
float d = (float) sensor.accelerometer_m_s2[i] - accel_ema[i];
float d = sensor.accelerometer_m_s2[i] - accel_ema[i];
accel_ema[i] += d * w;
d = d * d;
accel_disp[i] = accel_disp[i] * (1.0f - w);
if (d > still_thr2 * 8.0f)
d = still_thr2 * 8.0f;
if (d > accel_disp[i])
accel_disp[i] = d;
}
/* still detector with hysteresis */
if ( accel_disp[0] < still_thr2 &&
accel_disp[1] < still_thr2 &&
accel_disp[2] < still_thr2 ) {
if (accel_disp[0] < still_thr2 &&
accel_disp[1] < still_thr2 &&
accel_disp[2] < still_thr2) {
/* is still now */
if (t_still == 0) {
/* first time */
mavlink_log_info(mavlink_fd, "detected rest position, waiting...");
t_still = t;
t_timeout = t + timeout;
} else {
/* still since t_still */
if (t > t_still + still_time) {
@ -349,62 +407,71 @@ int detect_orientation(int mavlink_fd, int sub_sensor_combined) {
break;
}
}
} else if ( accel_disp[0] > still_thr2 * 2.0f ||
accel_disp[1] > still_thr2 * 2.0f ||
accel_disp[2] > still_thr2 * 2.0f) {
} else if (accel_disp[0] > still_thr2 * 4.0f ||
accel_disp[1] > still_thr2 * 4.0f ||
accel_disp[2] > still_thr2 * 4.0f) {
/* not still, reset still start time */
if (t_still != 0) {
mavlink_log_info(mavlink_fd, "detected motion, please hold still...");
mavlink_log_info(mavlink_fd, "detected motion, hold still...");
t_still = 0;
}
}
} else if (poll_ret == 0) {
poll_errcount++;
}
if (t > t_timeout) {
poll_errcount++;
}
if (poll_errcount > 1000) {
mavlink_log_info(mavlink_fd, "ERROR: Failed reading sensor");
return -1;
mavlink_log_critical(mavlink_fd, CAL_FAILED_SENSOR_MSG);
return ERROR;
}
}
if ( fabsf(accel_ema[0] - CONSTANTS_ONE_G) < accel_err_thr &&
fabsf(accel_ema[1]) < accel_err_thr &&
fabsf(accel_ema[2]) < accel_err_thr )
if (fabsf(accel_ema[0] - CONSTANTS_ONE_G) < accel_err_thr &&
fabsf(accel_ema[1]) < accel_err_thr &&
fabsf(accel_ema[2]) < accel_err_thr)
return 0; // [ g, 0, 0 ]
if ( fabsf(accel_ema[0] + CONSTANTS_ONE_G) < accel_err_thr &&
fabsf(accel_ema[1]) < accel_err_thr &&
fabsf(accel_ema[2]) < accel_err_thr )
if (fabsf(accel_ema[0] + CONSTANTS_ONE_G) < accel_err_thr &&
fabsf(accel_ema[1]) < accel_err_thr &&
fabsf(accel_ema[2]) < accel_err_thr)
return 1; // [ -g, 0, 0 ]
if ( fabsf(accel_ema[0]) < accel_err_thr &&
fabsf(accel_ema[1] - CONSTANTS_ONE_G) < accel_err_thr &&
fabsf(accel_ema[2]) < accel_err_thr )
if (fabsf(accel_ema[0]) < accel_err_thr &&
fabsf(accel_ema[1] - CONSTANTS_ONE_G) < accel_err_thr &&
fabsf(accel_ema[2]) < accel_err_thr)
return 2; // [ 0, g, 0 ]
if ( fabsf(accel_ema[0]) < accel_err_thr &&
fabsf(accel_ema[1] + CONSTANTS_ONE_G) < accel_err_thr &&
fabsf(accel_ema[2]) < accel_err_thr )
if (fabsf(accel_ema[0]) < accel_err_thr &&
fabsf(accel_ema[1] + CONSTANTS_ONE_G) < accel_err_thr &&
fabsf(accel_ema[2]) < accel_err_thr)
return 3; // [ 0, -g, 0 ]
if ( fabsf(accel_ema[0]) < accel_err_thr &&
fabsf(accel_ema[1]) < accel_err_thr &&
fabsf(accel_ema[2] - CONSTANTS_ONE_G) < accel_err_thr )
if (fabsf(accel_ema[0]) < accel_err_thr &&
fabsf(accel_ema[1]) < accel_err_thr &&
fabsf(accel_ema[2] - CONSTANTS_ONE_G) < accel_err_thr)
return 4; // [ 0, 0, g ]
if ( fabsf(accel_ema[0]) < accel_err_thr &&
fabsf(accel_ema[1]) < accel_err_thr &&
fabsf(accel_ema[2] + CONSTANTS_ONE_G) < accel_err_thr )
if (fabsf(accel_ema[0]) < accel_err_thr &&
fabsf(accel_ema[1]) < accel_err_thr &&
fabsf(accel_ema[2] + CONSTANTS_ONE_G) < accel_err_thr)
return 5; // [ 0, 0, -g ]
mavlink_log_info(mavlink_fd, "ERROR: invalid orientation");
mavlink_log_critical(mavlink_fd, "ERROR: invalid orientation");
return -2; // Can't detect orientation
return ERROR; // Can't detect orientation
}
/*
* Read specified number of accelerometer samples, calculate average and dispersion.
*/
int read_accelerometer_avg(int sensor_combined_sub, float accel_avg[3], int samples_num) {
int read_accelerometer_avg(int sensor_combined_sub, float accel_avg[3], int samples_num)
{
struct pollfd fds[1];
fds[0].fd = sensor_combined_sub;
fds[0].events = POLLIN;
@ -415,12 +482,16 @@ int read_accelerometer_avg(int sensor_combined_sub, float accel_avg[3], int samp
while (count < samples_num) {
int poll_ret = poll(fds, 1, 1000);
if (poll_ret == 1) {
struct sensor_combined_s sensor;
orb_copy(ORB_ID(sensor_combined), sensor_combined_sub, &sensor);
for (int i = 0; i < 3; i++)
accel_sum[i] += sensor.accelerometer_m_s2[i];
count++;
} else {
errcount++;
continue;
@ -437,10 +508,12 @@ int read_accelerometer_avg(int sensor_combined_sub, float accel_avg[3], int samp
return OK;
}
int mat_invert3(float src[3][3], float dst[3][3]) {
int mat_invert3(float src[3][3], float dst[3][3])
{
float det = src[0][0] * (src[1][1] * src[2][2] - src[1][2] * src[2][1]) -
src[0][1] * (src[1][0] * src[2][2] - src[1][2] * src[2][0]) +
src[0][2] * (src[1][0] * src[2][1] - src[1][1] * src[2][0]);
src[0][1] * (src[1][0] * src[2][2] - src[1][2] * src[2][0]) +
src[0][2] * (src[1][0] * src[2][1] - src[1][1] * src[2][0]);
if (det == 0.0f)
return ERROR; // Singular matrix
@ -457,7 +530,8 @@ int mat_invert3(float src[3][3], float dst[3][3]) {
return OK;
}
int calculate_calibration_values(float accel_ref[6][3], float accel_T[3][3], float accel_offs[3], float g) {
int calculate_calibration_values(float accel_ref[6][3], float accel_T[3][3], float accel_offs[3], float g)
{
/* calculate offsets */
for (int i = 0; i < 3; i++) {
accel_offs[i] = (accel_ref[i * 2][i] + accel_ref[i * 2 + 1][i]) / 2;
@ -466,6 +540,7 @@ int calculate_calibration_values(float accel_ref[6][3], float accel_T[3][3], flo
/* fill matrix A for linear equations system*/
float mat_A[3][3];
memset(mat_A, 0, sizeof(mat_A));
for (int i = 0; i < 3; i++) {
for (int j = 0; j < 3; j++) {
float a = accel_ref[i * 2][j] - accel_offs[j];
@ -475,6 +550,7 @@ int calculate_calibration_values(float accel_ref[6][3], float accel_T[3][3], flo
/* calculate inverse matrix for A */
float mat_A_inv[3][3];
if (mat_invert3(mat_A, mat_A_inv) != OK)
return ERROR;

View File

@ -0,0 +1,57 @@
/****************************************************************************
*
* Copyright (C) 2013 PX4 Development Team. All rights reserved.
* Author: Anton Babushkin <anton.babushkin@me.com>
*
* 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.
*
****************************************************************************/
/**
* @file calibration_messages.h
*
* Common calibration messages.
*
* @author Anton Babushkin <anton.babushkin@me.com>
*/
#ifndef CALIBRATION_MESSAGES_H_
#define CALIBRATION_MESSAGES_H_
#define CAL_STARTED_MSG "%s calibration: started"
#define CAL_DONE_MSG "%s calibration: done"
#define CAL_FAILED_MSG "%s calibration: failed"
#define CAL_PROGRESS_MSG "%s calibration: progress <%u>"
#define CAL_FAILED_SENSOR_MSG "ERROR: failed reading sensor"
#define CAL_FAILED_RESET_CAL_MSG "ERROR: failed to reset calibration"
#define CAL_FAILED_APPLY_CAL_MSG "ERROR: failed to apply calibration"
#define CAL_FAILED_SET_PARAMS_MSG "ERROR: failed to set parameters"
#define CAL_FAILED_SAVE_PARAMS_MSG "ERROR: failed to save parameters"
#endif /* CALIBRATION_MESSAGES_H_ */

View File

@ -369,8 +369,10 @@ void handle_command(struct vehicle_status_s *status, const struct safety_s *safe
if (hil_ret == OK && control_mode->flag_system_hil_enabled) {
/* reset the arming mode to disarmed */
arming_res = arming_state_transition(status, safety, control_mode, ARMING_STATE_STANDBY, armed);
if (arming_res != TRANSITION_DENIED) {
mavlink_log_info(mavlink_fd, "[cmd] HIL: Reset ARMED state to standby");
} else {
mavlink_log_info(mavlink_fd, "[cmd] HIL: FAILED resetting armed state");
}
@ -481,27 +483,28 @@ void handle_command(struct vehicle_status_s *status, const struct safety_s *safe
break;
}
case VEHICLE_CMD_COMPONENT_ARM_DISARM:
{
transition_result_t arming_res = TRANSITION_NOT_CHANGED;
if (!armed->armed && ((int)(cmd->param1 + 0.5f)) == 1) {
if (safety->safety_switch_available && !safety->safety_off) {
print_reject_arm("NOT ARMING: Press safety switch first.");
arming_res = TRANSITION_DENIED;
case VEHICLE_CMD_COMPONENT_ARM_DISARM: {
transition_result_t arming_res = TRANSITION_NOT_CHANGED;
} else {
arming_res = arming_state_transition(status, safety, control_mode, ARMING_STATE_ARMED, armed);
}
if (!armed->armed && ((int)(cmd->param1 + 0.5f)) == 1) {
if (safety->safety_switch_available && !safety->safety_off) {
print_reject_arm("NOT ARMING: Press safety switch first.");
arming_res = TRANSITION_DENIED;
if (arming_res == TRANSITION_CHANGED) {
mavlink_log_info(mavlink_fd, "[cmd] ARMED by component arm cmd");
result = VEHICLE_CMD_RESULT_ACCEPTED;
} else {
mavlink_log_info(mavlink_fd, "[cmd] REJECTING component arm cmd");
result = VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED;
} else {
arming_res = arming_state_transition(status, safety, control_mode, ARMING_STATE_ARMED, armed);
}
if (arming_res == TRANSITION_CHANGED) {
mavlink_log_info(mavlink_fd, "[cmd] ARMED by component arm cmd");
result = VEHICLE_CMD_RESULT_ACCEPTED;
} else {
mavlink_log_info(mavlink_fd, "[cmd] REJECTING component arm cmd");
result = VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED;
}
}
}
}
break;
default:
@ -687,7 +690,7 @@ int commander_thread_main(int argc, char *argv[])
bool updated = false;
bool rc_calibration_ok = (OK == rc_calibration_check());
bool rc_calibration_ok = (OK == rc_calibration_check(mavlink_fd));
/* Subscribe to safety topic */
int safety_sub = orb_subscribe(ORB_ID(safety));
@ -802,7 +805,7 @@ int commander_thread_main(int argc, char *argv[])
status_changed = true;
/* re-check RC calibration */
rc_calibration_ok = (OK == rc_calibration_check());
rc_calibration_ok = (OK == rc_calibration_check(mavlink_fd));
/* navigation parameters */
param_get(_param_takeoff_alt, &takeoff_alt);
@ -940,7 +943,7 @@ int commander_thread_main(int argc, char *argv[])
last_idle_time = system_load.tasks[0].total_runtime;
/* check if board is connected via USB */
struct stat statbuf;
//struct stat statbuf;
//on_usb_power = (stat("/dev/ttyACM0", &statbuf) == 0);
}
@ -970,6 +973,7 @@ int commander_thread_main(int argc, char *argv[])
if (armed.armed) {
arming_state_transition(&status, &safety, &control_mode, ARMING_STATE_ARMED_ERROR, &armed);
} else {
arming_state_transition(&status, &safety, &control_mode, ARMING_STATE_STANDBY_ERROR, &armed);
}
@ -1244,12 +1248,14 @@ int commander_thread_main(int argc, char *argv[])
counter++;
int blink_state = blink_msg_state();
if (blink_state > 0) {
/* blinking LED message, don't touch LEDs */
if (blink_state == 2) {
/* blinking LED message completed, restore normal state */
control_status_leds(&status, &armed, true);
}
} else {
/* normal state */
control_status_leds(&status, &armed, status_changed);
@ -1264,7 +1270,7 @@ int commander_thread_main(int argc, char *argv[])
ret = pthread_join(commander_low_prio_thread, NULL);
if (ret) {
warn("join failed", ret);
warn("join failed: %d", ret);
}
rgbled_set_mode(RGBLED_MODE_OFF);
@ -1308,6 +1314,7 @@ control_status_leds(vehicle_status_s *status, actuator_armed_s *armed, bool chan
/* driving rgbled */
if (changed) {
bool set_normal_color = false;
/* set mode */
if (status->arming_state == ARMING_STATE_ARMED) {
rgbled_set_mode(RGBLED_MODE_ON);
@ -1332,6 +1339,7 @@ control_status_leds(vehicle_status_s *status, actuator_armed_s *armed, bool chan
if (status->battery_warning == VEHICLE_BATTERY_WARNING_LOW) {
rgbled_set_color(RGBLED_COLOR_AMBER);
}
/* VEHICLE_BATTERY_WARNING_CRITICAL handled as ARMING_STATE_ARMED_ERROR / ARMING_STATE_STANDBY_ERROR */
} else {
@ -1694,11 +1702,10 @@ void *commander_low_prio_loop(void *arg)
fds[0].events = POLLIN;
while (!thread_should_exit) {
/* wait for up to 100ms for data */
/* wait for up to 200ms for data */
int pret = poll(&fds[0], (sizeof(fds) / sizeof(fds[0])), 200);
/* timed out - periodic check for _task_should_exit, etc. */
/* timed out - periodic check for thread_should_exit, etc. */
if (pret == 0)
continue;
@ -1773,7 +1780,7 @@ void *commander_low_prio_loop(void *arg)
} else if ((int)(cmd.param4) == 1) {
/* RC calibration */
answer_command(cmd, VEHICLE_CMD_RESULT_DENIED);
answer_command(cmd, VEHICLE_CMD_RESULT_ACCEPTED);
calib_ret = do_rc_calibration(mavlink_fd);
} else if ((int)(cmd.param5) == 1) {
@ -1854,7 +1861,6 @@ void *commander_low_prio_loop(void *arg)
/* send acknowledge command */
// XXX TODO
}
}
close(cmd_sub);

View File

@ -33,10 +33,12 @@
/**
* @file gyro_calibration.cpp
*
* Gyroscope calibration routine
*/
#include "gyro_calibration.h"
#include "calibration_messages.h"
#include "commander_helper.h"
#include <stdio.h>
@ -56,21 +58,14 @@
#endif
static const int ERROR = -1;
static const char *sensor_name = "gyro";
int do_gyro_calibration(int mavlink_fd)
{
mavlink_log_info(mavlink_fd, "Gyro calibration starting, do not move unit.");
mavlink_log_info(mavlink_fd, CAL_STARTED_MSG, sensor_name);
mavlink_log_info(mavlink_fd, "don't move system");
const unsigned calibration_count = 5000;
int sub_sensor_combined = orb_subscribe(ORB_ID(sensor_combined));
struct sensor_combined_s raw;
unsigned calibration_counter = 0;
float gyro_offset[3] = {0.0f, 0.0f, 0.0f};
/* set offsets to zero */
int fd = open(GYRO_DEVICE_PATH, 0);
struct gyro_scale gscale_null = {
struct gyro_scale gyro_scale = {
0.0f,
1.0f,
0.0f,
@ -79,98 +74,101 @@ int do_gyro_calibration(int mavlink_fd)
1.0f,
};
if (OK != ioctl(fd, GYROIOCSSCALE, (long unsigned int)&gscale_null))
warn("WARNING: failed to set scale / offsets for gyro");
int res = OK;
/* reset all offsets to zero and all scales to one */
int fd = open(GYRO_DEVICE_PATH, 0);
res = ioctl(fd, GYROIOCSSCALE, (long unsigned int)&gyro_scale);
close(fd);
unsigned poll_errcount = 0;
if (res != OK) {
mavlink_log_critical(mavlink_fd, CAL_FAILED_RESET_CAL_MSG);
}
while (calibration_counter < calibration_count) {
if (res == OK) {
/* determine gyro mean values */
const unsigned calibration_count = 5000;
unsigned calibration_counter = 0;
unsigned poll_errcount = 0;
/* wait blocking for new data */
struct pollfd fds[1];
fds[0].fd = sub_sensor_combined;
fds[0].events = POLLIN;
/* subscribe to gyro sensor topic */
int sub_sensor_gyro = orb_subscribe(ORB_ID(sensor_gyro));
struct gyro_report gyro_report;
int poll_ret = poll(fds, 1, 1000);
while (calibration_counter < calibration_count) {
/* wait blocking for new data */
struct pollfd fds[1];
fds[0].fd = sub_sensor_gyro;
fds[0].events = POLLIN;
if (poll_ret > 0) {
orb_copy(ORB_ID(sensor_combined), sub_sensor_combined, &raw);
gyro_offset[0] += raw.gyro_rad_s[0];
gyro_offset[1] += raw.gyro_rad_s[1];
gyro_offset[2] += raw.gyro_rad_s[2];
calibration_counter++;
if (calibration_counter % (calibration_count / 20) == 0)
mavlink_log_info(mavlink_fd, "gyro cal progress <%u> percent", (calibration_counter * 100) / calibration_count);
int poll_ret = poll(fds, 1, 1000);
} else {
poll_errcount++;
if (poll_ret > 0) {
orb_copy(ORB_ID(sensor_gyro), sub_sensor_gyro, &gyro_report);
gyro_scale.x_offset += gyro_report.x;
gyro_scale.y_offset += gyro_report.y;
gyro_scale.z_offset += gyro_report.z;
calibration_counter++;
if (calibration_counter % (calibration_count / 20) == 0)
mavlink_log_info(mavlink_fd, CAL_PROGRESS_MSG, sensor_name, (calibration_counter * 100) / calibration_count);
} else {
poll_errcount++;
}
if (poll_errcount > 1000) {
mavlink_log_critical(mavlink_fd, CAL_FAILED_SENSOR_MSG);
res = ERROR;
break;
}
}
if (poll_errcount > 1000) {
mavlink_log_info(mavlink_fd, "ERROR: Failed reading gyro sensor");
close(sub_sensor_combined);
return ERROR;
close(sub_sensor_gyro);
gyro_scale.x_offset /= calibration_count;
gyro_scale.y_offset /= calibration_count;
gyro_scale.z_offset /= calibration_count;
}
if (res == OK) {
/* check offsets */
if (!isfinite(gyro_scale.x_offset) || !isfinite(gyro_scale.y_offset) || !isfinite(gyro_scale.z_offset)) {
mavlink_log_critical(mavlink_fd, "ERROR: offset is NaN");
res = ERROR;
}
}
gyro_offset[0] = gyro_offset[0] / calibration_count;
gyro_offset[1] = gyro_offset[1] / calibration_count;
gyro_offset[2] = gyro_offset[2] / calibration_count;
if (isfinite(gyro_offset[0]) && isfinite(gyro_offset[1]) && isfinite(gyro_offset[2])) {
if (param_set(param_find("SENS_GYRO_XOFF"), &(gyro_offset[0]))
|| param_set(param_find("SENS_GYRO_YOFF"), &(gyro_offset[1]))
|| param_set(param_find("SENS_GYRO_ZOFF"), &(gyro_offset[2]))) {
mavlink_log_critical(mavlink_fd, "Setting gyro offsets failed!");
if (res == OK) {
/* set offset parameters to new values */
if (param_set(param_find("SENS_GYRO_XOFF"), &(gyro_scale.x_offset))
|| param_set(param_find("SENS_GYRO_YOFF"), &(gyro_scale.y_offset))
|| param_set(param_find("SENS_GYRO_ZOFF"), &(gyro_scale.z_offset))) {
mavlink_log_critical(mavlink_fd, "ERROR: failed to set offset params");
res = ERROR;
}
/* set offsets to actual value */
fd = open(GYRO_DEVICE_PATH, 0);
struct gyro_scale gscale = {
gyro_offset[0],
1.0f,
gyro_offset[1],
1.0f,
gyro_offset[2],
1.0f,
};
if (OK != ioctl(fd, GYROIOCSSCALE, (long unsigned int)&gscale))
warn("WARNING: failed to set scale / offsets for gyro");
close(fd);
/* auto-save to EEPROM */
int save_ret = param_save_default();
if (save_ret != 0) {
warnx("WARNING: auto-save of params to storage failed");
mavlink_log_critical(mavlink_fd, "gyro store failed");
close(sub_sensor_combined);
return ERROR;
}
tune_neutral();
/* third beep by cal end routine */
} else {
mavlink_log_info(mavlink_fd, "offset cal FAILED (NaN)");
close(sub_sensor_combined);
return ERROR;
}
mavlink_log_info(mavlink_fd, "offset calibration done.");
#if 0
/*** --- SCALING --- ***/
/* beep on offset calibration end */
mavlink_log_info(mavlink_fd, "gyro offset calibration done");
tune_neutral();
/* scale calibration */
/* this was only a proof of concept and is currently not working. scaling will be set to 1.0 for now. */
mavlink_log_info(mavlink_fd, "offset done. Rotate for scale 30x or wait 5s to skip.");
warnx("offset calibration finished. Rotate for scale 30x, or do not rotate and wait for 5 seconds to skip.");
/* apply new offsets */
fd = open(GYRO_DEVICE_PATH, 0);
if (OK != ioctl(fd, GYROIOCSSCALE, (long unsigned int)&gyro_scale))
warn("WARNING: failed to apply new offsets for gyro");
close(fd);
unsigned rotations_count = 30;
float gyro_integral = 0.0f;
float baseline_integral = 0.0f;
@ -178,9 +176,11 @@ int do_gyro_calibration(int mavlink_fd)
// XXX change to mag topic
orb_copy(ORB_ID(sensor_combined), sub_sensor_combined, &raw);
float mag_last = -atan2f(raw.magnetometer_ga[1],raw.magnetometer_ga[0]);
if (mag_last > M_PI_F) mag_last -= 2*M_PI_F;
if (mag_last < -M_PI_F) mag_last += 2*M_PI_F;
float mag_last = -atan2f(raw.magnetometer_ga[1], raw.magnetometer_ga[0]);
if (mag_last > M_PI_F) mag_last -= 2 * M_PI_F;
if (mag_last < -M_PI_F) mag_last += 2 * M_PI_F;
uint64_t last_time = hrt_absolute_time();
@ -190,7 +190,7 @@ int do_gyro_calibration(int mavlink_fd)
/* abort this loop if not rotated more than 180 degrees within 5 seconds */
if ((fabsf(baseline_integral / (2.0f * M_PI_F)) < 0.6f)
&& (hrt_absolute_time() - start_time > 5 * 1e6)) {
&& (hrt_absolute_time() - start_time > 5 * 1e6)) {
mavlink_log_info(mavlink_fd, "scale skipped, gyro calibration done");
close(sub_sensor_combined);
return OK;
@ -218,14 +218,17 @@ int do_gyro_calibration(int mavlink_fd)
// calculate error between estimate and measurement
// apply declination correction for true heading as well.
//float mag = -atan2f(magNav(1),magNav(0));
float mag = -atan2f(raw.magnetometer_ga[1],raw.magnetometer_ga[0]);
if (mag > M_PI_F) mag -= 2*M_PI_F;
if (mag < -M_PI_F) mag += 2*M_PI_F;
float mag = -atan2f(raw.magnetometer_ga[1], raw.magnetometer_ga[0]);
if (mag > M_PI_F) mag -= 2 * M_PI_F;
if (mag < -M_PI_F) mag += 2 * M_PI_F;
float diff = mag - mag_last;
if (diff > M_PI_F) diff -= 2*M_PI_F;
if (diff < -M_PI_F) diff += 2*M_PI_F;
if (diff > M_PI_F) diff -= 2 * M_PI_F;
if (diff < -M_PI_F) diff += 2 * M_PI_F;
baseline_integral += diff;
mag_last = mag;
@ -235,63 +238,68 @@ int do_gyro_calibration(int mavlink_fd)
// warnx("dbg: b: %6.4f, g: %6.4f", (double)baseline_integral, (double)gyro_integral);
// } else if (poll_ret == 0) {
// /* any poll failure for 1s is a reason to abort */
// mavlink_log_info(mavlink_fd, "gyro calibration aborted, retry");
// return;
// } else if (poll_ret == 0) {
// /* any poll failure for 1s is a reason to abort */
// mavlink_log_info(mavlink_fd, "gyro calibration aborted, retry");
// return;
}
}
float gyro_scale = baseline_integral / gyro_integral;
warnx("gyro scale: yaw (z): %6.4f", (double)gyro_scale);
mavlink_log_info(mavlink_fd, "gyro scale: yaw (z): %6.4f", (double)gyro_scale);
#else
float gyro_scales[] = { 1.0f, 1.0f, 1.0f };
#endif
if (isfinite(gyro_scales[0]) && isfinite(gyro_scales[1]) && isfinite(gyro_scales[2])) {
if (param_set(param_find("SENS_GYRO_XSCALE"), &(gyro_scales[0]))
|| param_set(param_find("SENS_GYRO_YSCALE"), &(gyro_scales[1]))
|| param_set(param_find("SENS_GYRO_ZSCALE"), &(gyro_scales[2]))) {
mavlink_log_critical(mavlink_fd, "Setting gyro scale failed!");
}
/* set offsets to actual value */
fd = open(GYRO_DEVICE_PATH, 0);
struct gyro_scale gscale = {
gyro_offset[0],
gyro_scales[0],
gyro_offset[1],
gyro_scales[1],
gyro_offset[2],
gyro_scales[2],
};
if (OK != ioctl(fd, GYROIOCSSCALE, (long unsigned int)&gscale))
warn("WARNING: failed to set scale / offsets for gyro");
close(fd);
/* auto-save to EEPROM */
int save_ret = param_save_default();
if (save_ret != 0) {
warn("WARNING: auto-save of params to storage failed");
}
mavlink_log_info(mavlink_fd, "gyro calibration done");
/* third beep by cal end routine */
close(sub_sensor_combined);
return OK;
} else {
mavlink_log_info(mavlink_fd, "gyro calibration FAILED (NaN)");
close(sub_sensor_combined);
if (!isfinite(gyro_scale.x_scale) || !isfinite(gyro_scale.y_scale) || !isfinite(gyro_scale.z_scale)) {
mavlink_log_info(mavlink_fd, "gyro scale calibration FAILED (NaN)");
close(sub_sensor_gyro);
mavlink_log_critical(mavlink_fd, "gyro calibration failed");
return ERROR;
}
/* beep on calibration end */
mavlink_log_info(mavlink_fd, "gyro scale calibration done");
tune_neutral();
#endif
if (res == OK) {
/* set scale parameters to new values */
if (param_set(param_find("SENS_GYRO_XSCALE"), &(gyro_scale.x_scale))
|| param_set(param_find("SENS_GYRO_YSCALE"), &(gyro_scale.y_scale))
|| param_set(param_find("SENS_GYRO_ZSCALE"), &(gyro_scale.z_scale))) {
mavlink_log_critical(mavlink_fd, "ERROR: failed to set scale params");
res = ERROR;
}
}
if (res == OK) {
/* apply new scaling and offsets */
fd = open(GYRO_DEVICE_PATH, 0);
res = ioctl(fd, GYROIOCSSCALE, (long unsigned int)&gyro_scale);
close(fd);
if (res != OK) {
mavlink_log_critical(mavlink_fd, CAL_FAILED_APPLY_CAL_MSG);
}
}
if (res == OK) {
/* auto-save to EEPROM */
res = param_save_default();
if (res != OK) {
mavlink_log_critical(mavlink_fd, CAL_FAILED_SAVE_PARAMS_MSG);
}
}
if (res == OK) {
mavlink_log_info(mavlink_fd, CAL_DONE_MSG, sensor_name);
} else {
mavlink_log_info(mavlink_fd, CAL_FAILED_MSG, sensor_name);
}
return res;
}

View File

@ -33,12 +33,14 @@
/**
* @file mag_calibration.cpp
*
* Magnetometer calibration routine
*/
#include "mag_calibration.h"
#include "commander_helper.h"
#include "calibration_routines.h"
#include "calibration_messages.h"
#include <stdio.h>
#include <stdlib.h>
@ -59,26 +61,20 @@
#endif
static const int ERROR = -1;
static const char *sensor_name = "mag";
int do_mag_calibration(int mavlink_fd)
{
mavlink_log_info(mavlink_fd, "please put the system in a rest position and wait.");
int sub_mag = orb_subscribe(ORB_ID(sensor_mag));
struct mag_report mag;
mavlink_log_info(mavlink_fd, CAL_STARTED_MSG, sensor_name);
mavlink_log_info(mavlink_fd, "don't move system");
/* 45 seconds */
uint64_t calibration_interval = 45 * 1000 * 1000;
/* maximum 2000 values */
/* maximum 500 values */
const unsigned int calibration_maxcount = 500;
unsigned int calibration_counter = 0;
/* limit update rate to get equally spaced measurements over time (in ms) */
orb_set_interval(sub_mag, (calibration_interval / 1000) / calibration_maxcount);
int fd = open(MAG_DEVICE_PATH, O_RDONLY);
/* erase old calibration */
struct mag_scale mscale_null = {
0.0f,
1.0f,
@ -88,97 +84,92 @@ int do_mag_calibration(int mavlink_fd)
1.0f,
};
if (OK != ioctl(fd, MAGIOCSSCALE, (long unsigned int)&mscale_null)) {
warn("WARNING: failed to set scale / offsets for mag");
mavlink_log_info(mavlink_fd, "failed to set scale / offsets for mag");
int res = OK;
/* erase old calibration */
int fd = open(MAG_DEVICE_PATH, O_RDONLY);
res = ioctl(fd, MAGIOCSSCALE, (long unsigned int)&mscale_null);
if (res != OK) {
mavlink_log_critical(mavlink_fd, CAL_FAILED_RESET_CAL_MSG);
}
/* calibrate range */
if (OK != ioctl(fd, MAGIOCCALIBRATE, fd)) {
warnx("failed to calibrate scale");
if (res == OK) {
/* calibrate range */
res = ioctl(fd, MAGIOCCALIBRATE, fd);
if (res != OK) {
mavlink_log_critical(mavlink_fd, "ERROR: failed to calibrate scale");
}
}
close(fd);
mavlink_log_info(mavlink_fd, "mag cal progress <20> percent");
float *x;
float *y;
float *z;
/* calibrate offsets */
if (res == OK) {
/* allocate memory */
mavlink_log_info(mavlink_fd, CAL_PROGRESS_MSG, sensor_name, 20);
// uint64_t calibration_start = hrt_absolute_time();
x = (float *)malloc(sizeof(float) * calibration_maxcount);
y = (float *)malloc(sizeof(float) * calibration_maxcount);
z = (float *)malloc(sizeof(float) * calibration_maxcount);
uint64_t axis_deadline = hrt_absolute_time();
uint64_t calibration_deadline = hrt_absolute_time() + calibration_interval;
const char axislabels[3] = { 'X', 'Y', 'Z'};
int axis_index = -1;
float *x = (float *)malloc(sizeof(float) * calibration_maxcount);
float *y = (float *)malloc(sizeof(float) * calibration_maxcount);
float *z = (float *)malloc(sizeof(float) * calibration_maxcount);
if (x == NULL || y == NULL || z == NULL) {
warnx("mag cal failed: out of memory");
mavlink_log_info(mavlink_fd, "mag cal failed: out of memory");
warnx("x:%p y:%p z:%p\n", x, y, z);
return ERROR;
if (x == NULL || y == NULL || z == NULL) {
mavlink_log_critical(mavlink_fd, "ERROR: out of memory");
res = ERROR;
}
}
mavlink_log_info(mavlink_fd, "scale calibration completed, dynamic calibration starting..");
if (res == OK) {
int sub_mag = orb_subscribe(ORB_ID(sensor_mag));
struct mag_report mag;
unsigned poll_errcount = 0;
/* limit update rate to get equally spaced measurements over time (in ms) */
orb_set_interval(sub_mag, (calibration_interval / 1000) / calibration_maxcount);
while (hrt_absolute_time() < calibration_deadline &&
calibration_counter < calibration_maxcount) {
/* calibrate offsets */
uint64_t calibration_deadline = hrt_absolute_time() + calibration_interval;
unsigned poll_errcount = 0;
/* wait blocking for new data */
struct pollfd fds[1];
fds[0].fd = sub_mag;
fds[0].events = POLLIN;
mavlink_log_info(mavlink_fd, "rotate in a figure 8 around all axis");
/* user guidance */
if (hrt_absolute_time() >= axis_deadline &&
axis_index < 3) {
while (hrt_absolute_time() < calibration_deadline &&
calibration_counter < calibration_maxcount) {
axis_index++;
/* wait blocking for new data */
struct pollfd fds[1];
fds[0].fd = sub_mag;
fds[0].events = POLLIN;
mavlink_log_info(mavlink_fd, "please rotate in a figure 8 or around %c axis.", axislabels[axis_index]);
tune_neutral();
int poll_ret = poll(fds, 1, 1000);
axis_deadline += calibration_interval / 3;
if (poll_ret > 0) {
orb_copy(ORB_ID(sensor_mag), sub_mag, &mag);
x[calibration_counter] = mag.x;
y[calibration_counter] = mag.y;
z[calibration_counter] = mag.z;
calibration_counter++;
if (calibration_counter % (calibration_maxcount / 20) == 0)
mavlink_log_info(mavlink_fd, CAL_PROGRESS_MSG, sensor_name, 20 + (calibration_counter * 50) / calibration_maxcount);
} else {
poll_errcount++;
}
if (poll_errcount > 1000) {
mavlink_log_critical(mavlink_fd, CAL_FAILED_SENSOR_MSG);
res = ERROR;
break;
}
}
if (!(axis_index < 3)) {
break;
}
int poll_ret = poll(fds, 1, 1000);
if (poll_ret > 0) {
orb_copy(ORB_ID(sensor_mag), sub_mag, &mag);
x[calibration_counter] = mag.x;
y[calibration_counter] = mag.y;
z[calibration_counter] = mag.z;
calibration_counter++;
if (calibration_counter % (calibration_maxcount / 20) == 0)
mavlink_log_info(mavlink_fd, "mag cal progress <%u> percent", 20 + (calibration_counter * 50) / calibration_maxcount);
} else {
poll_errcount++;
}
if (poll_errcount > 1000) {
mavlink_log_info(mavlink_fd, "ERROR: Failed reading mag sensor");
close(sub_mag);
free(x);
free(y);
free(z);
return ERROR;
}
close(sub_mag);
}
float sphere_x;
@ -186,93 +177,100 @@ int do_mag_calibration(int mavlink_fd)
float sphere_z;
float sphere_radius;
mavlink_log_info(mavlink_fd, "mag cal progress <70> percent");
sphere_fit_least_squares(x, y, z, calibration_counter, 100, 0.0f, &sphere_x, &sphere_y, &sphere_z, &sphere_radius);
mavlink_log_info(mavlink_fd, "mag cal progress <80> percent");
if (res == OK) {
/* sphere fit */
mavlink_log_info(mavlink_fd, CAL_PROGRESS_MSG, sensor_name, 70);
sphere_fit_least_squares(x, y, z, calibration_counter, 100, 0.0f, &sphere_x, &sphere_y, &sphere_z, &sphere_radius);
mavlink_log_info(mavlink_fd, CAL_PROGRESS_MSG, sensor_name, 80);
free(x);
free(y);
free(z);
if (!isfinite(sphere_x) || !isfinite(sphere_y) || !isfinite(sphere_z)) {
mavlink_log_critical(mavlink_fd, "ERROR: NaN in sphere fit");
res = ERROR;
}
}
if (isfinite(sphere_x) && isfinite(sphere_y) && isfinite(sphere_z)) {
if (x != NULL)
free(x);
fd = open(MAG_DEVICE_PATH, 0);
if (y != NULL)
free(y);
if (z != NULL)
free(z);
if (res == OK) {
/* apply calibration and set parameters */
struct mag_scale mscale;
if (OK != ioctl(fd, MAGIOCGSCALE, (long unsigned int)&mscale))
warn("WARNING: failed to get scale / offsets for mag");
fd = open(MAG_DEVICE_PATH, 0);
res = ioctl(fd, MAGIOCGSCALE, (long unsigned int)&mscale);
mscale.x_offset = sphere_x;
mscale.y_offset = sphere_y;
mscale.z_offset = sphere_z;
if (res != OK) {
mavlink_log_critical(mavlink_fd, "ERROR: failed to get current calibration");
}
if (OK != ioctl(fd, MAGIOCSSCALE, (long unsigned int)&mscale))
warn("WARNING: failed to set scale / offsets for mag");
if (res == OK) {
mscale.x_offset = sphere_x;
mscale.y_offset = sphere_y;
mscale.z_offset = sphere_z;
res = ioctl(fd, MAGIOCSSCALE, (long unsigned int)&mscale);
if (res != OK) {
mavlink_log_critical(mavlink_fd, CAL_FAILED_APPLY_CAL_MSG);
}
}
close(fd);
/* announce and set new offset */
if (res == OK) {
/* set parameters */
if (param_set(param_find("SENS_MAG_XOFF"), &(mscale.x_offset)))
res = ERROR;
if (param_set(param_find("SENS_MAG_XOFF"), &(mscale.x_offset))) {
warnx("Setting X mag offset failed!\n");
if (param_set(param_find("SENS_MAG_YOFF"), &(mscale.y_offset)))
res = ERROR;
if (param_set(param_find("SENS_MAG_ZOFF"), &(mscale.z_offset)))
res = ERROR;
if (param_set(param_find("SENS_MAG_XSCALE"), &(mscale.x_scale)))
res = ERROR;
if (param_set(param_find("SENS_MAG_YSCALE"), &(mscale.y_scale)))
res = ERROR;
if (param_set(param_find("SENS_MAG_ZSCALE"), &(mscale.z_scale)))
res = ERROR;
if (res != OK) {
mavlink_log_critical(mavlink_fd, CAL_FAILED_SET_PARAMS_MSG);
}
mavlink_log_info(mavlink_fd, CAL_PROGRESS_MSG, sensor_name, 90);
}
if (param_set(param_find("SENS_MAG_YOFF"), &(mscale.y_offset))) {
warnx("Setting Y mag offset failed!\n");
if (res == OK) {
/* auto-save to EEPROM */
res = param_save_default();
if (res != OK) {
mavlink_log_critical(mavlink_fd, CAL_FAILED_SAVE_PARAMS_MSG);
}
}
if (param_set(param_find("SENS_MAG_ZOFF"), &(mscale.z_offset))) {
warnx("Setting Z mag offset failed!\n");
mavlink_log_info(mavlink_fd, "mag off: x:%.2f y:%.2f z:%.2f Ga", (double)mscale.x_offset,
(double)mscale.y_offset, (double)mscale.z_offset);
mavlink_log_info(mavlink_fd, "mag scale: x:%.2f y:%.2f z:%.2f", (double)mscale.x_scale,
(double)mscale.y_scale, (double)mscale.z_scale);
if (res == OK) {
mavlink_log_info(mavlink_fd, CAL_DONE_MSG, sensor_name);
} else {
mavlink_log_info(mavlink_fd, CAL_FAILED_MSG, sensor_name);
}
if (param_set(param_find("SENS_MAG_XSCALE"), &(mscale.x_scale))) {
warnx("Setting X mag scale failed!\n");
}
if (param_set(param_find("SENS_MAG_YSCALE"), &(mscale.y_scale))) {
warnx("Setting Y mag scale failed!\n");
}
if (param_set(param_find("SENS_MAG_ZSCALE"), &(mscale.z_scale))) {
warnx("Setting Z mag scale failed!\n");
}
mavlink_log_info(mavlink_fd, "mag cal progress <90> percent");
/* auto-save to EEPROM */
int save_ret = param_save_default();
if (save_ret != 0) {
warn("WARNING: auto-save of params to storage failed");
mavlink_log_info(mavlink_fd, "FAILED storing calibration");
close(sub_mag);
return ERROR;
}
warnx("\tscale: %.6f %.6f %.6f\n \toffset: %.6f %.6f %.6f\nradius: %.6f GA\n",
(double)mscale.x_scale, (double)mscale.y_scale, (double)mscale.z_scale,
(double)mscale.x_offset, (double)mscale.y_offset, (double)mscale.z_offset, (double)sphere_radius);
char buf[52];
sprintf(buf, "mag off: x:%.2f y:%.2f z:%.2f Ga", (double)mscale.x_offset,
(double)mscale.y_offset, (double)mscale.z_offset);
mavlink_log_info(mavlink_fd, buf);
sprintf(buf, "mag scale: x:%.2f y:%.2f z:%.2f", (double)mscale.x_scale,
(double)mscale.y_scale, (double)mscale.z_scale);
mavlink_log_info(mavlink_fd, buf);
mavlink_log_info(mavlink_fd, "magnetometer calibration completed");
mavlink_log_info(mavlink_fd, "mag cal progress <100> percent");
close(sub_mag);
return OK;
/* third beep by cal end routine */
} else {
mavlink_log_info(mavlink_fd, "mag calibration FAILED (NaN in sphere fit)");
close(sub_mag);
return ERROR;
return res;
}
}

View File

@ -47,4 +47,3 @@ SRCS = commander.cpp \
baro_calibration.cpp \
rc_calibration.cpp \
airspeed_calibration.cpp

View File

@ -683,6 +683,10 @@ FixedwingAttitudeControl::task_main()
_actuators.control[4] = _manual.flaps;
}
_actuators.control[5] = _manual.aux1;
_actuators.control[6] = _manual.aux2;
_actuators.control[7] = _manual.aux3;
/* lazily publish the setpoint only once available */
_actuators.timestamp = hrt_absolute_time();

View File

@ -192,6 +192,7 @@ private:
float pitch_limit_min;
float pitch_limit_max;
float roll_limit;
float throttle_min;
float throttle_max;
float throttle_cruise;
@ -225,6 +226,7 @@ private:
param_t pitch_limit_min;
param_t pitch_limit_max;
param_t roll_limit;
param_t throttle_min;
param_t throttle_max;
param_t throttle_cruise;
@ -343,6 +345,7 @@ FixedwingPositionControl::FixedwingPositionControl() :
_parameter_handles.pitch_limit_min = param_find("FW_P_LIM_MIN");
_parameter_handles.pitch_limit_max = param_find("FW_P_LIM_MAX");
_parameter_handles.roll_limit = param_find("FW_R_LIM");
_parameter_handles.throttle_min = param_find("FW_THR_MIN");
_parameter_handles.throttle_max = param_find("FW_THR_MAX");
_parameter_handles.throttle_cruise = param_find("FW_THR_CRUISE");
@ -405,6 +408,7 @@ FixedwingPositionControl::parameters_update()
param_get(_parameter_handles.pitch_limit_min, &(_parameters.pitch_limit_min));
param_get(_parameter_handles.pitch_limit_max, &(_parameters.pitch_limit_max));
param_get(_parameter_handles.roll_limit, &(_parameters.roll_limit));
param_get(_parameter_handles.throttle_min, &(_parameters.throttle_min));
param_get(_parameter_handles.throttle_max, &(_parameters.throttle_max));
param_get(_parameter_handles.throttle_cruise, &(_parameters.throttle_cruise));
@ -426,6 +430,7 @@ FixedwingPositionControl::parameters_update()
_l1_control.set_l1_damping(_parameters.l1_damping);
_l1_control.set_l1_period(_parameters.l1_period);
_l1_control.set_l1_roll_limit(math::radians(_parameters.roll_limit));
_tecs.set_time_const(_parameters.time_const);
_tecs.set_min_sink_rate(_parameters.min_sink_rate);

View File

@ -67,6 +67,9 @@ PARAM_DEFINE_FLOAT(FW_P_LIM_MIN, -45.0f);
PARAM_DEFINE_FLOAT(FW_P_LIM_MAX, 45.0f);
PARAM_DEFINE_FLOAT(FW_R_LIM, 45.0f);
PARAM_DEFINE_FLOAT(FW_THR_MIN, 0.0f);

View File

@ -422,13 +422,13 @@ handle_message(mavlink_message_t *msg)
hil_sensors.accelerometer_counter = hil_counter;
/* differential pressure */
hil_sensors.differential_pressure_pa = imu.diff_pressure;
hil_sensors.differential_pressure_pa = imu.diff_pressure * 1e2f; //from hPa to Pa
hil_sensors.differential_pressure_counter = hil_counter;
/* airspeed from differential pressure, ambient pressure and temp */
struct airspeed_s airspeed;
float ias = calc_indicated_airspeed(imu.diff_pressure);
float ias = calc_indicated_airspeed(hil_sensors.differential_pressure_pa);
// XXX need to fix this
float tas = ias;

View File

@ -368,6 +368,12 @@ mc_thread_main(int argc, char *argv[])
actuators.control[3] = 0.0f;
}
/* fill in manual control values */
actuators.control[4] = manual.flaps;
actuators.control[5] = manual.aux1;
actuators.control[6] = manual.aux2;
actuators.control[7] = manual.aux3;
actuators.timestamp = hrt_absolute_time();
orb_publish(ORB_ID_VEHICLE_ATTITUDE_CONTROLS, actuator_pub, &actuators);

View File

@ -58,6 +58,7 @@
#include <systemlib/err.h>
#include <unistd.h>
#include <drivers/drv_hrt.h>
#include <math.h>
#include <uORB/uORB.h>
#include <uORB/topics/vehicle_status.h>
@ -84,12 +85,14 @@
#include <uORB/topics/esc_status.h>
#include <systemlib/systemlib.h>
#include <systemlib/param/param.h>
#include <mavlink/mavlink_log.h>
#include "logbuffer.h"
#include "sdlog2_format.h"
#include "sdlog2_messages.h"
#include "sdlog2_version.h"
#define LOGBUFFER_WRITE_AND_COUNT(_msg) if (logbuffer_write(&lb, &log_msg, LOG_PACKET_SIZE(_msg))) { \
log_msgs_written++; \
@ -180,8 +183,17 @@ static void sdlog2_stop_log(void);
/**
* Write a header to log file: list of message formats.
*/
static void write_formats(int fd);
static int write_formats(int fd);
/**
* Write version message to log file.
*/
static int write_version(int fd);
/**
* Write parameters to log file.
*/
static int write_parameters(int fd);
static bool file_exist(const char *filename);
@ -237,11 +249,11 @@ int sdlog2_main(int argc, char *argv[])
main_thread_should_exit = false;
deamon_task = task_spawn_cmd("sdlog2",
SCHED_DEFAULT,
SCHED_PRIORITY_DEFAULT - 30,
3000,
sdlog2_thread_main,
(const char **)argv);
SCHED_DEFAULT,
SCHED_PRIORITY_DEFAULT - 30,
3000,
sdlog2_thread_main,
(const char **)argv);
exit(0);
}
@ -354,10 +366,13 @@ static void *logwriter_thread(void *arg)
struct logbuffer_s *logbuf = (struct logbuffer_s *)arg;
int log_file = open_logfile();
int log_fd = open_logfile();
/* write log messages formats */
write_formats(log_file);
/* write log messages formats, version and parameters */
log_bytes_written += write_formats(log_fd);
log_bytes_written += write_version(log_fd);
log_bytes_written += write_parameters(log_fd);
fsync(log_fd);
int poll_count = 0;
@ -396,7 +411,7 @@ static void *logwriter_thread(void *arg)
n = available;
}
n = write(log_file, read_ptr, n);
n = write(log_fd, read_ptr, n);
should_wait = (n == available) && !is_part;
@ -411,21 +426,23 @@ static void *logwriter_thread(void *arg)
} else {
n = 0;
/* exit only with empty buffer */
if (main_thread_should_exit || logwriter_should_exit) {
break;
}
should_wait = true;
}
if (++poll_count == 10) {
fsync(log_file);
fsync(log_fd);
poll_count = 0;
}
}
fsync(log_file);
close(log_file);
fsync(log_fd);
close(log_fd);
return OK;
}
@ -479,34 +496,92 @@ void sdlog2_stop_log()
/* wait for write thread to return */
int ret;
if ((ret = pthread_join(logwriter_pthread, NULL)) != 0) {
warnx("error joining logwriter thread: %i", ret);
}
logwriter_pthread = 0;
sdlog2_status();
}
void write_formats(int fd)
int write_formats(int fd)
{
/* construct message format packet */
struct {
LOG_PACKET_HEADER;
struct log_format_s body;
} log_format_packet = {
} log_msg_format = {
LOG_PACKET_HEADER_INIT(LOG_FORMAT_MSG),
};
/* fill message format packet for each format and write to log */
int i;
int written = 0;
for (i = 0; i < log_formats_num; i++) {
log_format_packet.body = log_formats[i];
log_bytes_written += write(fd, &log_format_packet, sizeof(log_format_packet));
/* fill message format packet for each format and write it */
for (int i = 0; i < log_formats_num; i++) {
log_msg_format.body = log_formats[i];
written += write(fd, &log_msg_format, sizeof(log_msg_format));
}
fsync(fd);
return written;
}
int write_version(int fd)
{
/* construct version message */
struct {
LOG_PACKET_HEADER;
struct log_VER_s body;
} log_msg_VER = {
LOG_PACKET_HEADER_INIT(LOG_VER_MSG),
};
/* fill version message and write it */
strncpy(log_msg_VER.body.fw_git, FW_GIT, sizeof(log_msg_VER.body.fw_git));
strncpy(log_msg_VER.body.arch, HW_ARCH, sizeof(log_msg_VER.body.arch));
return write(fd, &log_msg_VER, sizeof(log_msg_VER));
}
int write_parameters(int fd)
{
/* construct parameter message */
struct {
LOG_PACKET_HEADER;
struct log_PARM_s body;
} log_msg_PARM = {
LOG_PACKET_HEADER_INIT(LOG_PARM_MSG),
};
int written = 0;
param_t params_cnt = param_count();
for (param_t param = 0; param < params_cnt; param++) {
/* fill parameter message and write it */
strncpy(log_msg_PARM.body.name, param_name(param), sizeof(log_msg_PARM.body.name));
float value = NAN;
switch (param_type(param)) {
case PARAM_TYPE_INT32: {
int32_t i;
param_get(param, &i);
value = i; // cast integer to float
break;
}
case PARAM_TYPE_FLOAT:
param_get(param, &value);
break;
default:
break;
}
log_msg_PARM.body.value = value;
written += write(fd, &log_msg_PARM, sizeof(log_msg_PARM));
}
return written;
}
int sdlog2_thread_main(int argc, char *argv[])
@ -584,12 +659,13 @@ int sdlog2_thread_main(int argc, char *argv[])
}
const char *converter_in = "/etc/logging/conv.zip";
char* converter_out = malloc(120);
char *converter_out = malloc(120);
sprintf(converter_out, "%s/conv.zip", folder_path);
if (file_copy(converter_in, converter_out)) {
errx(1, "unable to copy conversion scripts, exiting.");
}
free(converter_out);
/* only print logging path, important to find log file later */
@ -603,6 +679,7 @@ int sdlog2_thread_main(int argc, char *argv[])
}
struct vehicle_status_s buf_status;
memset(&buf_status, 0, sizeof(buf_status));
/* warning! using union here to save memory, elements should be used separately! */
@ -628,6 +705,7 @@ int sdlog2_thread_main(int argc, char *argv[])
struct esc_status_s esc;
struct vehicle_global_velocity_setpoint_s global_vel_sp;
} buf;
memset(&buf, 0, sizeof(buf));
struct {
@ -798,7 +876,7 @@ int sdlog2_thread_main(int argc, char *argv[])
subs.airspeed_sub = orb_subscribe(ORB_ID(airspeed));
fds[fdsc_count].fd = subs.airspeed_sub;
fds[fdsc_count].events = POLLIN;
fdsc_count++;
fdsc_count++;
/* --- ESCs --- */
subs.esc_sub = orb_subscribe(ORB_ID(esc_status));
@ -886,7 +964,7 @@ int sdlog2_thread_main(int argc, char *argv[])
continue;
}
ifds = 1; // Begin from fds[1] again
ifds = 1; // begin from fds[1] again
pthread_mutex_lock(&logbuffer_mutex);
@ -1145,8 +1223,8 @@ int sdlog2_thread_main(int argc, char *argv[])
/* --- ESCs --- */
if (fds[ifds++].revents & POLLIN) {
orb_copy(ORB_ID(esc_status), subs.esc_sub, &buf.esc);
for (uint8_t i=0; i<buf.esc.esc_count; i++)
{
for (uint8_t i = 0; i < buf.esc.esc_count; i++) {
log_msg.msg_type = LOG_ESC_MSG;
log_msg.body.log_ESC.counter = buf.esc.counter;
log_msg.body.log_ESC.esc_count = buf.esc.esc_count;
@ -1294,6 +1372,7 @@ void handle_status(struct vehicle_status_s *status)
{
// TODO use flag from actuator_armed here?
bool armed = status->arming_state == ARMING_STATE_ARMED || status->arming_state == ARMING_STATE_ARMED_ERROR;
if (armed != flag_system_armed) {
flag_system_armed = armed;

View File

@ -85,10 +85,10 @@ struct log_format_s {
#define LOG_FORMAT(_name, _format, _labels) { \
.type = LOG_##_name##_MSG, \
.length = sizeof(struct log_##_name##_s) + LOG_PACKET_HEADER_LEN, \
.name = #_name, \
.format = _format, \
.labels = _labels \
.length = sizeof(struct log_##_name##_s) + LOG_PACKET_HEADER_LEN, \
.name = #_name, \
.format = _format, \
.labels = _labels \
}
#define LOG_FORMAT_MSG 0x80

View File

@ -48,12 +48,6 @@
/* define message formats */
#pragma pack(push, 1)
/* --- TIME - TIME STAMP --- */
#define LOG_TIME_MSG 1
struct log_TIME_s {
uint64_t t;
};
/* --- ATT - ATTITUDE --- */
#define LOG_ATT_MSG 2
struct log_ATT_s {
@ -253,30 +247,31 @@ struct log_GVSP_s {
float vz;
};
/* --- FWRV - FIRMWARE REVISION --- */
#define LOG_FWRV_MSG 20
struct log_FWRV_s {
char fw_revision[64];
/* --- TIME - TIME STAMP --- */
#define LOG_TIME_MSG 129
struct log_TIME_s {
uint64_t t;
};
/* --- VER - VERSION --- */
#define LOG_VER_MSG 130
struct log_VER_s {
char arch[16];
char fw_git[64];
};
/* --- PARM - PARAMETER --- */
#define LOG_PARM_MSG 131
struct log_PARM_s {
char name[16];
float value;
};
#pragma pack(pop)
/*
GIT_VERSION is defined at build time via a Makefile call to the
git command line. We create a fake log message format for
the firmware revision "FWRV" that is written to every log
header. This makes it easier to determine which version
of the firmware was running when a log was created.
*/
#define FREEZE_STR(s) #s
#define STRINGIFY(s) FREEZE_STR(s)
#define FW_VERSION_STR STRINGIFY(GIT_VERSION)
/* construct list of all message formats */
static const struct log_format_s log_formats[] = {
LOG_FORMAT(TIME, "Q", "StartTime"),
/* business-level messages, ID < 0x80 */
LOG_FORMAT(ATT, "ffffff", "Roll,Pitch,Yaw,RollRate,PitchRate,YawRate"),
LOG_FORMAT(ATSP, "ffff", "RollSP,PitchSP,YawSP,ThrustSP"),
LOG_FORMAT(IMU, "fffffffff", "AccX,AccY,AccZ,GyroX,GyroY,GyroZ,MagX,MagY,MagZ"),
@ -295,7 +290,11 @@ static const struct log_format_s log_formats[] = {
LOG_FORMAT(GPSP, "BLLfffbBffff", "AltRel,Lat,Lon,Alt,Yaw,LoiterR,LoiterDir,NavCmd,P1,P2,P3,P4"),
LOG_FORMAT(ESC, "HBBBHHHHHHfH", "Counter,NumESC,Conn,N,Ver,Adr,Volt,Amp,RPM,Temp,SetP,SetPRAW"),
LOG_FORMAT(GVSP, "fff", "VX,VY,VZ"),
LOG_FORMAT(FWRV,"Z",FW_VERSION_STR),
/* system-level messages, ID >= 0x80 */
// FMT: don't write format of format message, it's useless
LOG_FORMAT(TIME, "Q", "StartTime"),
LOG_FORMAT(VER, "NZ", "Arch,FwGit"),
LOG_FORMAT(PARM, "Nf", "Name,Value"),
};
static const int log_formats_num = sizeof(log_formats) / sizeof(struct log_format_s);

View File

@ -0,0 +1,62 @@
/****************************************************************************
*
* Copyright (c) 2013 PX4 Development Team. All rights reserved.
* Author: Anton Babushkin <anton.babushkin@me.com>
*
* 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.
*
****************************************************************************/
/**
* @file sdlog2_version.h
*
* Tools for system version detection.
*
* @author Anton Babushkin <anton.babushkin@me.com>
*/
#ifndef SDLOG2_VERSION_H_
#define SDLOG2_VERSION_H_
/*
GIT_VERSION is defined at build time via a Makefile call to the
git command line.
*/
#define FREEZE_STR(s) #s
#define STRINGIFY(s) FREEZE_STR(s)
#define FW_GIT STRINGIFY(GIT_VERSION)
#ifdef CONFIG_ARCH_BOARD_PX4FMU_V1
#define HW_ARCH "PX4FMU_V1"
#endif
#ifdef CONFIG_ARCH_BOARD_PX4FMU_V2
#define HW_ARCH "PX4FMU_V2"
#endif
#endif /* SDLOG2_VERSION_H_ */

View File

@ -26,7 +26,7 @@ void BlockSegwayController::update() {
_actuators.control[i] = 0.0f;
// only update guidance in auto mode
if (_status.state_machine == SYSTEM_STATE_AUTO) {
if (_status.main_state == MAIN_STATE_AUTO) {
// update guidance
}
@ -34,17 +34,18 @@ void BlockSegwayController::update() {
float spdCmd = -th2v.update(_att.pitch) - q2v.update(_att.pitchspeed);
// handle autopilot modes
if (_status.state_machine == SYSTEM_STATE_AUTO ||
_status.state_machine == SYSTEM_STATE_STABILIZED) {
if (_status.main_state == MAIN_STATE_AUTO ||
_status.main_state == MAIN_STATE_SEATBELT ||
_status.main_state == MAIN_STATE_EASY) {
_actuators.control[0] = spdCmd;
_actuators.control[1] = spdCmd;
} else if (_status.state_machine == SYSTEM_STATE_MANUAL) {
if (_status.manual_control_mode == VEHICLE_MANUAL_CONTROL_MODE_DIRECT) {
} else if (_status.main_state == MAIN_STATE_MANUAL) {
if (_status.navigation_state == NAVIGATION_STATE_DIRECT) {
_actuators.control[CH_LEFT] = _manual.throttle;
_actuators.control[CH_RIGHT] = _manual.pitch;
} else if (_status.manual_control_mode == VEHICLE_MANUAL_CONTROL_MODE_SAS) {
} else if (_status.navigation_state == NAVIGATION_STATE_STABILIZE) {
_actuators.control[0] = spdCmd;
_actuators.control[1] = spdCmd;
}

View File

@ -44,8 +44,34 @@
#include <systemlib/param/param.h>
/**
* Gyro X offset FIXME
*
* This is an X-axis offset for the gyro.
* Adjust it according to the calibration data.
*
* @min -10.0
* @max 10.0
* @group Gyro Config
*/
PARAM_DEFINE_FLOAT(SENS_GYRO_XOFF, 0.0f);
/**
* Gyro Y offset FIXME with dot.
*
* @min -10.0
* @max 10.0
* @group Gyro Config
*/
PARAM_DEFINE_FLOAT(SENS_GYRO_YOFF, 0.0f);
/**
* Gyro Z offset FIXME
*
* @min -5.0
* @max 5.0
* @group Gyro Config
*/
PARAM_DEFINE_FLOAT(SENS_GYRO_ZOFF, 0.0f);
PARAM_DEFINE_FLOAT(SENS_GYRO_XSCALE, 1.0f);
@ -193,8 +219,9 @@ PARAM_DEFINE_INT32(RC_MAP_MISSIO_SW, 0);
PARAM_DEFINE_INT32(RC_MAP_FLAPS, 0);
PARAM_DEFINE_INT32(RC_MAP_AUX1, 0); /**< default function: camera yaw / azimuth */
PARAM_DEFINE_INT32(RC_MAP_AUX2, 0); /**< default function: camera pitch / tilt */
PARAM_DEFINE_INT32(RC_MAP_AUX1, 0); /**< default function: camera pitch */
PARAM_DEFINE_INT32(RC_MAP_AUX2, 0); /**< default function: camera roll */
PARAM_DEFINE_INT32(RC_MAP_AUX3, 0); /**< default function: camera azimuth / yaw */
PARAM_DEFINE_FLOAT(RC_SCALE_ROLL, 0.6f);
PARAM_DEFINE_FLOAT(RC_SCALE_PITCH, 0.6f);

View File

@ -67,6 +67,7 @@
#include <systemlib/param/param.h>
#include <systemlib/err.h>
#include <systemlib/perf_counter.h>
#include <conversion/rotation.h>
#include <systemlib/airspeed.h>
@ -74,6 +75,7 @@
#include <uORB/topics/sensor_combined.h>
#include <uORB/topics/rc_channels.h>
#include <uORB/topics/manual_control_setpoint.h>
#include <uORB/topics/actuator_controls.h>
#include <uORB/topics/vehicle_control_mode.h>
#include <uORB/topics/parameter_update.h>
#include <uORB/topics/battery_status.h>
@ -135,75 +137,6 @@
#define limit_minus_one_to_one(arg) (arg < -1.0f) ? -1.0f : ((arg > 1.0f) ? 1.0f : arg)
/**
* Enum for board and external compass rotations.
* This enum maps from board attitude to airframe attitude.
*/
enum Rotation {
ROTATION_NONE = 0,
ROTATION_YAW_45 = 1,
ROTATION_YAW_90 = 2,
ROTATION_YAW_135 = 3,
ROTATION_YAW_180 = 4,
ROTATION_YAW_225 = 5,
ROTATION_YAW_270 = 6,
ROTATION_YAW_315 = 7,
ROTATION_ROLL_180 = 8,
ROTATION_ROLL_180_YAW_45 = 9,
ROTATION_ROLL_180_YAW_90 = 10,
ROTATION_ROLL_180_YAW_135 = 11,
ROTATION_PITCH_180 = 12,
ROTATION_ROLL_180_YAW_225 = 13,
ROTATION_ROLL_180_YAW_270 = 14,
ROTATION_ROLL_180_YAW_315 = 15,
ROTATION_ROLL_90 = 16,
ROTATION_ROLL_90_YAW_45 = 17,
ROTATION_ROLL_90_YAW_90 = 18,
ROTATION_ROLL_90_YAW_135 = 19,
ROTATION_ROLL_270 = 20,
ROTATION_ROLL_270_YAW_45 = 21,
ROTATION_ROLL_270_YAW_90 = 22,
ROTATION_ROLL_270_YAW_135 = 23,
ROTATION_PITCH_90 = 24,
ROTATION_PITCH_270 = 25,
ROTATION_MAX
};
typedef struct {
uint16_t roll;
uint16_t pitch;
uint16_t yaw;
} rot_lookup_t;
const rot_lookup_t rot_lookup[] = {
{ 0, 0, 0 },
{ 0, 0, 45 },
{ 0, 0, 90 },
{ 0, 0, 135 },
{ 0, 0, 180 },
{ 0, 0, 225 },
{ 0, 0, 270 },
{ 0, 0, 315 },
{180, 0, 0 },
{180, 0, 45 },
{180, 0, 90 },
{180, 0, 135 },
{ 0, 180, 0 },
{180, 0, 225 },
{180, 0, 270 },
{180, 0, 315 },
{ 90, 0, 0 },
{ 90, 0, 45 },
{ 90, 0, 90 },
{ 90, 0, 135 },
{270, 0, 0 },
{270, 0, 45 },
{270, 0, 90 },
{270, 0, 135 },
{ 0, 90, 0 },
{ 0, 270, 0 }
};
/**
* Sensor app start / stop handling function
*
@ -264,6 +197,7 @@ private:
orb_advert_t _sensor_pub; /**< combined sensor data topic */
orb_advert_t _manual_control_pub; /**< manual control signal topic */
orb_advert_t _actuator_group_3_pub; /**< manual control as actuator topic */
orb_advert_t _rc_pub; /**< raw r/c control topic */
orb_advert_t _battery_pub; /**< battery status */
orb_advert_t _airspeed_pub; /**< airspeed */
@ -384,11 +318,6 @@ private:
*/
int parameters_update();
/**
* Get the rotation matrices
*/
void get_rot_matrix(enum Rotation rot, math::Matrix *rot_matrix);
/**
* Do accel-related initialisation.
*/
@ -519,6 +448,7 @@ Sensors::Sensors() :
/* publications */
_sensor_pub(-1),
_manual_control_pub(-1),
_actuator_group_3_pub(-1),
_rc_pub(-1),
_battery_pub(-1),
_airspeed_pub(-1),
@ -803,24 +733,6 @@ Sensors::parameters_update()
return OK;
}
void
Sensors::get_rot_matrix(enum Rotation rot, math::Matrix *rot_matrix)
{
/* first set to zero */
rot_matrix->Matrix::zero(3, 3);
float roll = M_DEG_TO_RAD_F * (float)rot_lookup[rot].roll;
float pitch = M_DEG_TO_RAD_F * (float)rot_lookup[rot].pitch;
float yaw = M_DEG_TO_RAD_F * (float)rot_lookup[rot].yaw;
math::EulerAngles euler(roll, pitch, yaw);
math::Dcm R(euler);
for (int i = 0; i < 3; i++) for (int j = 0; j < 3; j++)
(*rot_matrix)(i, j) = R(i, j);
}
void
Sensors::accel_init()
{
@ -1318,6 +1230,7 @@ Sensors::rc_poll()
orb_copy(ORB_ID(input_rc), _rc_sub, &rc_input);
struct manual_control_setpoint_s manual_control;
struct actuator_controls_s actuator_group_3;
/* initialize to default values */
manual_control.roll = NAN;
@ -1485,6 +1398,16 @@ Sensors::rc_poll()
manual_control.aux5 = limit_minus_one_to_one(_rc.chan[_rc.function[AUX_5]].scaled);
}
/* copy from mapped manual control to control group 3 */
actuator_group_3.control[0] = manual_control.roll;
actuator_group_3.control[1] = manual_control.pitch;
actuator_group_3.control[2] = manual_control.yaw;
actuator_group_3.control[3] = manual_control.throttle;
actuator_group_3.control[4] = manual_control.flaps;
actuator_group_3.control[5] = manual_control.aux1;
actuator_group_3.control[6] = manual_control.aux2;
actuator_group_3.control[7] = manual_control.aux3;
/* check if ready for publishing */
if (_rc_pub > 0) {
orb_publish(ORB_ID(rc_channels), _rc_pub, &_rc);
@ -1501,6 +1424,14 @@ Sensors::rc_poll()
} else {
_manual_control_pub = orb_advertise(ORB_ID(manual_control_setpoint), &manual_control);
}
/* check if ready for publishing */
if (_actuator_group_3_pub > 0) {
orb_publish(ORB_ID(actuator_controls_3), _actuator_group_3_pub, &actuator_group_3);
} else {
_actuator_group_3_pub = orb_advertise(ORB_ID(actuator_controls_3), &actuator_group_3);
}
}
}

View File

@ -508,64 +508,63 @@ param_get_default_file(void)
int
param_save_default(void)
{
int result;
unsigned retries = 0;
/* delete the file in case it exists */
struct stat buffer;
if (stat(param_get_default_file(), &buffer) == 0) {
do {
result = unlink(param_get_default_file());
if (result != 0) {
retries++;
usleep(1000 * retries);
}
} while (result != OK && retries < 10);
if (result != OK)
warnx("unlinking file %s failed.", param_get_default_file());
}
/* create the file */
int res;
int fd;
do {
/* do another attempt in case the unlink call is not synced yet */
fd = open(param_get_default_file(), O_WRONLY | O_CREAT | O_EXCL);
const char *filename = param_get_default_file();
const char *filename_tmp = malloc(strlen(filename) + 5);
sprintf(filename_tmp, "%s.tmp", filename);
/* delete temp file if exist */
res = unlink(filename_tmp);
if (res != OK && errno == ENOENT)
res = OK;
if (res != OK)
warn("failed to delete temp file: %s", filename_tmp);
if (res == OK) {
/* write parameters to temp file */
fd = open(filename_tmp, O_WRONLY | O_CREAT | O_EXCL);
if (fd < 0) {
retries++;
usleep(1000 * retries);
warn("failed to open temp file: %s", filename_tmp);
res = ERROR;
}
} while (fd < 0 && retries < 10);
if (res == OK) {
res = param_export(fd, false);
if (fd < 0) {
warn("opening '%s' for writing failed", param_get_default_file());
return fd;
}
do {
result = param_export(fd, false);
if (result != OK) {
retries++;
usleep(1000 * retries);
if (res != OK)
warnx("failed to write parameters to file: %s", filename_tmp);
}
} while (result != 0 && retries < 10);
close(fd);
if (result != OK) {
warn("error exporting parameters to '%s'", param_get_default_file());
(void)unlink(param_get_default_file());
return result;
close(fd);
}
return 0;
if (res == OK) {
/* delete parameters file */
res = unlink(filename);
if (res != OK && errno == ENOENT)
res = OK;
if (res != OK)
warn("failed to delete parameters file: %s", filename);
}
if (res == OK) {
/* rename temp file to parameters */
res = rename(filename_tmp, filename);
if (res != OK)
warn("failed to rename %s to %s", filename_tmp, filename);
}
free(filename_tmp);
return res;
}
/**

View File

@ -47,14 +47,12 @@
#include <mavlink/mavlink_log.h>
#include <uORB/topics/rc_channels.h>
int rc_calibration_check(void) {
int rc_calibration_check(int mavlink_fd) {
char nbuf[20];
param_t _parameter_handles_min, _parameter_handles_trim, _parameter_handles_max,
_parameter_handles_rev, _parameter_handles_dz;
int mavlink_fd = open(MAVLINK_LOG_DEVICE, 0);
float param_min, param_max, param_trim, param_rev, param_dz;
/* first check channel mappings */

View File

@ -47,6 +47,6 @@
* @return 0 / OK if RC calibration is ok, index + 1 of the first
* channel that failed else (so 1 == first channel failed)
*/
__EXPORT int rc_calibration_check(void);
__EXPORT int rc_calibration_check(int mavlink_fd);
__END_DECLS

View File

@ -140,7 +140,7 @@ int preflight_check_main(int argc, char *argv[])
/* ---- RC CALIBRATION ---- */
bool rc_ok = (OK == rc_calibration_check());
bool rc_ok = (OK == rc_calibration_check(mavlink_fd));
/* warn */
if (!rc_ok)
@ -227,4 +227,4 @@ static int led_off(int leds, int led)
static int led_on(int leds, int led)
{
return ioctl(leds, LED_ON, led);
}
}