Merge branch 'beta' into offboard2

This commit is contained in:
Anton Babushkin
2014-02-01 11:02:17 +01:00
50 changed files with 1452 additions and 1066 deletions
+26 -6
View File
@@ -10,16 +10,36 @@ then
#
# Default parameters for this platform
#
param set MC_ATT_P 5.0
param set MC_ATT_I 0.0
param set MC_ROLL_P 5.0
param set MC_ROLLRATE_P 0.17
param set MC_ROLLRATE_I 0.0
param set MC_ROLLRATE_D 0.006
param set MC_PITCH_P 5.0
param set MC_PITCHRATE_P 0.17
param set MC_PITCHRATE_I 0.0
param set MC_PITCHRATE_D 0.006
param set MC_YAW_P 0.5
param set MC_YAW_I 0.15
param set MC_ATTRATE_P 0.17
param set MC_ATTRATE_I 0.0
param set MC_ATTRATE_D 0.006
param set MC_YAWRATE_P 0.2
param set MC_YAWRATE_I 0.0
param set MC_YAWRATE_D 0.0
param set MPC_THR_MAX 1.0
param set MPC_THR_MIN 0.1
param set MPC_XY_P 1.0
param set MPC_XY_VEL_P 0.1
param set MPC_XY_VEL_I 0.02
param set MPC_XY_VEL_D 0.01
param set MPC_XY_VEL_MAX 5
param set MPC_XY_FF 0.5
param set MPC_Z_P 1.0
param set MPC_Z_VEL_P 0.1
param set MPC_Z_VEL_I 0.02
param set MPC_Z_VEL_D 0.0
param set MPC_Z_VEL_MAX 3
param set MPC_Z_FF 0.5
param set MPC_TILT_MAX 1.0
param set MPC_LAND_SPEED 1.0
param set MPC_LAND_TILT 0.3
fi
set VEHICLE_TYPE mc
+19 -13
View File
@@ -10,30 +10,36 @@ then
#
# Default parameters for this platform
#
param set MC_ATT_P 9.0
param set MC_ATT_I 0.0
param set MC_ROLL_P 9.0
param set MC_ROLLRATE_P 0.13
param set MC_ROLLRATE_I 0.0
param set MC_ROLLRATE_D 0.004
param set MC_PITCH_P 9.0
param set MC_PITCHRATE_P 0.13
param set MC_PITCHRATE_I 0.0
param set MC_PITCHRATE_D 0.004
param set MC_YAW_P 0.5
param set MC_YAW_I 0.15
param set MC_ATTRATE_P 0.13
param set MC_ATTRATE_I 0.0
param set MC_ATTRATE_D 0.004
param set MC_YAWRATE_P 0.2
param set MC_YAWRATE_I 0.0
param set MC_YAWRATE_D 0.0
param set MPC_TILT_MAX 1.0
param set MPC_THR_MAX 1.0
param set MPC_THR_MIN 0.1
param set MPC_XY_P 1.0
param set MPC_XY_VEL_D 0.01
param set MPC_XY_VEL_I 0.02
param set MPC_XY_VEL_MAX 5
param set MPC_XY_VEL_P 0.1
param set MPC_XY_VEL_I 0.02
param set MPC_XY_VEL_D 0.01
param set MPC_XY_VEL_MAX 5
param set MPC_XY_FF 0.5
param set MPC_Z_P 1.0
param set MPC_Z_VEL_D 0.0
param set MPC_Z_VEL_I 0.02
param set MPC_Z_VEL_MAX 3
param set MPC_Z_VEL_P 0.1
param set MPC_Z_VEL_I 0.02
param set MPC_Z_VEL_D 0.0
param set MPC_Z_VEL_MAX 3
param set MPC_Z_FF 0.5
param set MPC_TILT_MAX 1.0
param set MPC_LAND_SPEED 1.0
param set MPC_LAND_TILT 0.3
param set BAT_V_SCALING 0.00989
param set BAT_C_SCALING 0.0124
+1 -33
View File
@@ -5,38 +5,6 @@
# Maintainers: Anton Babushkin <anton.babushkin@me.com>
#
if [ $DO_AUTOCONFIG == yes ]
then
#
# Default parameters for this platform
#
param set MC_ATT_P 7.0
param set MC_ATT_I 0.0
param set MC_YAW_P 2.0
param set MC_YAW_I 0.0
param set MC_ATTRATE_P 0.12
param set MC_ATTRATE_I 0.0
param set MC_ATTRATE_D 0.004
param set MC_YAWRATE_P 0.3
param set MC_YAWRATE_I 0.2
param set MC_YAWRATE_D 0.005
param set MPC_TILT_MAX 1.0
param set MPC_THR_MAX 1.0
param set MPC_THR_MIN 0.1
param set MPC_XY_P 1.0
param set MPC_XY_VEL_D 0.01
param set MPC_XY_VEL_I 0.02
param set MPC_XY_VEL_MAX 5
param set MPC_XY_VEL_P 0.1
param set MPC_Z_P 1.0
param set MPC_Z_VEL_D 0.0
param set MPC_Z_VEL_I 0.02
param set MPC_Z_VEL_MAX 3
param set MPC_Z_VEL_P 0.1
fi
sh /etc/init.d/4001_quad_x
set HIL yes
set VEHICLE_TYPE mc
set MIXER FMU_quad_x
+10
View File
@@ -0,0 +1,10 @@
#!nsh
#
# Generic 10” Octo coaxial geometry
#
# Maintainers: Lorenz Meier <lm@inf.ethz.ch>, Anton Babushkin <anton.babushkin@me.com>
#
sh /etc/init.d/8001_octo_x
set MIXER FMU_octo_cox
@@ -1,37 +0,0 @@
#!nsh
#
# Generic 10” Octo coaxial geometry
#
# Maintainers: Lorenz Meier <lm@inf.ethz.ch>
#
if [ $DO_AUTOCONFIG == yes ]
then
#
# Default parameters for this platform
#
param set MC_ATT_P 7.0
param set MC_ATT_I 0.0
param set MC_ATT_D 0.0
param set MC_ATTRATE_P 0.12
param set MC_ATTRATE_I 0.0
param set MC_ATTRATE_D 0.004
param set MC_YAWPOS_P 2.0
param set MC_YAWPOS_I 0.0
param set MC_YAWPOS_D 0.0
param set MC_YAWRATE_P 0.3
param set MC_YAWRATE_I 0.2
param set MC_YAWRATE_D 0.005
# TODO add default MPC parameters
fi
set VEHICLE_TYPE mc
set MIXER FMU_octo_cox
set PWM_OUTPUTS 1234
set PWM_RATE 400
# DJI ESC range
set PWM_DISARMED 900
set PWM_MIN 1200
set PWM_MAX 1900
+52
View File
@@ -0,0 +1,52 @@
#!nsh
#
# Generic 10” Quad X geometry
#
# Maintainers: Lorenz Meier <lm@inf.ethz.ch>, Anton Babushkin <anton.babushkin@me.com>
#
if [ $DO_AUTOCONFIG == yes ]
then
#
# Default parameters for this platform
#
param set MC_ROLL_P 7.0
param set MC_ROLLRATE_P 0.12
param set MC_ROLLRATE_I 0.0
param set MC_ROLLRATE_D 0.004
param set MC_PITCH_P 7.0
param set MC_PITCHRATE_P 0.12
param set MC_PITCHRATE_I 0.0
param set MC_PITCHRATE_D 0.004
param set MC_YAW_P 2.0
param set MC_YAWRATE_P 0.3
param set MC_YAWRATE_I 0.2
param set MC_YAWRATE_D 0.005
param set MPC_THR_MAX 1.0
param set MPC_THR_MIN 0.1
param set MPC_XY_P 1.0
param set MPC_XY_VEL_P 0.1
param set MPC_XY_VEL_I 0.02
param set MPC_XY_VEL_D 0.01
param set MPC_XY_VEL_MAX 5
param set MPC_XY_FF 0.5
param set MPC_Z_P 1.0
param set MPC_Z_VEL_P 0.1
param set MPC_Z_VEL_I 0.02
param set MPC_Z_VEL_D 0.0
param set MPC_Z_VEL_MAX 3
param set MPC_Z_FF 0.5
param set MPC_TILT_MAX 1.0
param set MPC_LAND_SPEED 1.0
param set MPC_LAND_TILT 0.3
fi
set VEHICLE_TYPE mc
set MIXER FMU_quad_x
set PWM_OUTPUTS 1234
set PWM_RATE 400
set PWM_DISARMED 900
set PWM_MIN 1000
set PWM_MAX 2000
-57
View File
@@ -1,57 +0,0 @@
#!nsh
echo "[init] 08_ardrone: PX4FMU on PX4IOAR carrier board"
#
# Load default params for this platform
#
if param compare SYS_AUTOCONFIG 1
then
# Set all params here, then disable autoconfig
param set MC_ATTRATE_D 0
param set MC_ATTRATE_I 0
param set MC_ATTRATE_P 0.13
param set MC_ATT_D 0
param set MC_ATT_I 0.3
param set MC_ATT_P 5
param set MC_YAWPOS_D 0.1
param set MC_YAWPOS_I 0.15
param set MC_YAWPOS_P 1
param set MC_YAWRATE_D 0
param set MC_YAWRATE_I 0
param set MC_YAWRATE_P 0.15
param set SYS_AUTOCONFIG 0
param save
fi
#
# Force some key parameters to sane values
# MAV_TYPE 2 = quadrotor
#
param set MAV_TYPE 2
param set BAT_V_SCALING 0.008381
#
# Start MAVLink
#
mavlink start -d /dev/ttyS0 -b 57600
usleep 5000
#
# Configure PX4FMU for operation with PX4IOAR
#
fmu mode_gpio_serial
#
# Fire up the AR.Drone interface.
#
ardrone_interface start -d /dev/ttyS1
#
# Start common for all multirotors apps
#
sh /etc/init.d/rc.multirotor
# Exit, because /dev/ttyS0 is needed for MAVLink
exit
@@ -1,83 +0,0 @@
#!nsh
echo "[init] 09_ardrone_flow: PX4FMU on PX4IOAR carrier board with PX4FLOW"
#
# Load default params for this platform
#
if param compare SYS_AUTOCONFIG 1
then
# Set all params here, then disable autoconfig
param set MC_ATTRATE_D 0
param set MC_ATTRATE_I 0
param set MC_ATTRATE_P 0.13
param set MC_ATT_D 0
param set MC_ATT_I 0.3
param set MC_ATT_P 5
param set MC_YAWPOS_D 0.1
param set MC_YAWPOS_I 0.15
param set MC_YAWPOS_P 1
param set MC_YAWRATE_D 0
param set MC_YAWRATE_I 0
param set MC_YAWRATE_P 0.15
param set SYS_AUTOCONFIG 0
param save
fi
#
# Force some key parameters to sane values
# MAV_TYPE 2 = quadrotor
#
param set MAV_TYPE 2
param set BAT_V_SCALING 0.008381
#
# Start MAVLink and MAVLink Onboard (PX4FLOW Sensor)
#
mavlink start -d /dev/ttyS0 -b 57600
mavlink_onboard start -d /dev/ttyS3 -b 115200
usleep 5000
#
# Configure PX4FMU for operation with PX4IOAR
#
fmu mode_gpio_serial
#
# Fire up the AR.Drone interface.
#
ardrone_interface start -d /dev/ttyS1
#
# Start the sensors.
#
sh /etc/init.d/rc.sensors
#
# Start the attitude estimator
#
attitude_estimator_ekf start
#
# Start the position estimator
#
flow_position_estimator start
#
# Fire up the multi rotor attitude controller
#
mc_att_control_vector start
#
# Fire up the flow position controller
#
flow_position_control start
#
# Fire up the flow speed controller
#
flow_speed_control start
# Exit, because /dev/ttyS0 is needed for MAVLink
exit
+19 -13
View File
@@ -10,30 +10,36 @@ then
#
# Default parameters for this platform
#
param set MC_ATT_P 7.0
param set MC_ATT_I 0.0
param set MC_ROLL_P 7.0
param set MC_ROLLRATE_P 0.12
param set MC_ROLLRATE_I 0.0
param set MC_ROLLRATE_D 0.004
param set MC_PITCH_P 7.0
param set MC_PITCHRATE_P 0.12
param set MC_PITCHRATE_I 0.0
param set MC_PITCHRATE_D 0.004
param set MC_YAW_P 2.8
param set MC_YAW_I 0.0
param set MC_ATTRATE_P 0.12
param set MC_ATTRATE_I 0.0
param set MC_ATTRATE_D 0.004
param set MC_YAWRATE_P 0.2
param set MC_YAWRATE_I 0.05
param set MC_YAWRATE_D 0.0
param set MPC_TILT_MAX 1.0
param set MPC_THR_MAX 1.0
param set MPC_THR_MIN 0.1
param set MPC_XY_P 1.0
param set MPC_XY_VEL_D 0.01
param set MPC_XY_VEL_I 0.02
param set MPC_XY_VEL_MAX 5
param set MPC_XY_VEL_P 0.1
param set MPC_XY_VEL_I 0.02
param set MPC_XY_VEL_D 0.01
param set MPC_XY_VEL_MAX 5
param set MPC_XY_FF 0.5
param set MPC_Z_P 1.0
param set MPC_Z_VEL_D 0.0
param set MPC_Z_VEL_I 0.02
param set MPC_Z_VEL_MAX 3
param set MPC_Z_VEL_P 0.1
param set MPC_Z_VEL_I 0.02
param set MPC_Z_VEL_D 0.0
param set MPC_Z_VEL_MAX 3
param set MPC_Z_FF 0.5
param set MPC_TILT_MAX 1.0
param set MPC_LAND_SPEED 1.0
param set MPC_LAND_TILT 0.3
fi
set VEHICLE_TYPE mc
+25 -7
View File
@@ -10,18 +10,36 @@ then
#
# Default parameters for this platform
#
param set MC_ATT_P 7.0
param set MC_ATT_I 0.0
param set MC_ROLL_P 7.0
param set MC_ROLLRATE_P 0.12
param set MC_ROLLRATE_I 0.0
param set MC_ROLLRATE_D 0.004
param set MC_PITCH_P 7.0
param set MC_PITCHRATE_P 0.12
param set MC_PITCHRATE_I 0.0
param set MC_PITCHRATE_D 0.004
param set MC_YAW_P 2.0
param set MC_YAW_I 0.0
param set MC_ATTRATE_P 0.12
param set MC_ATTRATE_I 0.0
param set MC_ATTRATE_D 0.004
param set MC_YAWRATE_P 0.3
param set MC_YAWRATE_I 0.2
param set MC_YAWRATE_D 0.005
# TODO add default MPC parameters
param set MPC_THR_MAX 1.0
param set MPC_THR_MIN 0.1
param set MPC_XY_P 1.0
param set MPC_XY_VEL_P 0.1
param set MPC_XY_VEL_I 0.02
param set MPC_XY_VEL_D 0.01
param set MPC_XY_VEL_MAX 5
param set MPC_XY_FF 0.5
param set MPC_Z_P 1.0
param set MPC_Z_VEL_P 0.1
param set MPC_Z_VEL_I 0.02
param set MPC_Z_VEL_D 0.0
param set MPC_Z_VEL_MAX 3
param set MPC_Z_FF 0.5
param set MPC_TILT_MAX 1.0
param set MPC_LAND_SPEED 1.0
param set MPC_LAND_TILT 0.3
fi
set VEHICLE_TYPE mc
+28 -7
View File
@@ -10,18 +10,36 @@ then
#
# Default parameters for this platform
#
param set MC_ATT_P 5.5
param set MC_ATT_I 0
param set MC_ROLL_P 5.5
param set MC_ROLLRATE_P 0.14
param set MC_ROLLRATE_I 0
param set MC_ROLLRATE_D 0.006
param set MC_PITCH_P 5.5
param set MC_PITCHRATE_P 0.14
param set MC_PITCHRATE_I 0
param set MC_PITCHRATE_D 0.006
param set MC_YAW_P 0.6
param set MC_YAW_I 0
param set MC_ATTRATE_P 0.14
param set MC_ATTRATE_I 0
param set MC_ATTRATE_D 0.006
param set MC_YAWRATE_P 0.08
param set MC_YAWRATE_I 0
param set MC_YAWRATE_D 0
# TODO add default MPC parameters
param set MPC_THR_MAX 1.0
param set MPC_THR_MIN 0.1
param set MPC_XY_P 1.0
param set MPC_XY_VEL_P 0.1
param set MPC_XY_VEL_I 0.02
param set MPC_XY_VEL_D 0.01
param set MPC_XY_VEL_MAX 5
param set MPC_XY_FF 0.5
param set MPC_Z_P 1.0
param set MPC_Z_VEL_P 0.1
param set MPC_Z_VEL_I 0.02
param set MPC_Z_VEL_D 0.0
param set MPC_Z_VEL_MAX 3
param set MPC_Z_FF 0.5
param set MPC_TILT_MAX 1.0
param set MPC_LAND_SPEED 1.0
param set MPC_LAND_TILT 0.3
fi
set VEHICLE_TYPE mc
@@ -29,3 +47,6 @@ set MIXER FMU_quad_x
set PWM_OUTPUTS 1234
set PWM_RATE 400
set PWM_DISARMED 900
set PWM_MIN 1000
set PWM_MAX 2000
+10
View File
@@ -0,0 +1,10 @@
#!nsh
#
# Generic 10” Quad + geometry
#
# Maintainers: Lorenz Meier <lm@inf.ethz.ch>, Anton Babushkin <anton.babushkin@me.com>
#
sh /etc/init.d/4001_quad_x
set MIXER FMU_quad_+
@@ -1,37 +0,0 @@
#!nsh
#
# Generic 10” Quad + geometry
#
# Maintainers: Lorenz Meier <lm@inf.ethz.ch>
#
if [ $DO_AUTOCONFIG == yes ]
then
#
# Default parameters for this platform
#
param set MC_ATT_P 7.0
param set MC_ATT_I 0.0
param set MC_ATT_D 0.0
param set MC_ATTRATE_P 0.12
param set MC_ATTRATE_I 0.0
param set MC_ATTRATE_D 0.004
param set MC_YAWPOS_P 2.0
param set MC_YAWPOS_I 0.0
param set MC_YAWPOS_D 0.0
param set MC_YAWRATE_P 0.3
param set MC_YAWRATE_I 0.2
param set MC_YAWRATE_D 0.005
# TODO add default MPC parameters
fi
set VEHICLE_TYPE mc
set MIXER FMU_quad_+
set PWM_OUTPUTS 1234
set PWM_RATE 400
# DJI ESC range
set PWM_DISARMED 900
set PWM_MIN 1200
set PWM_MAX 1900
+12
View File
@@ -0,0 +1,12 @@
#!nsh
#
# Generic 10” Hexa X geometry
#
# Maintainers: Lorenz Meier <lm@inf.ethz.ch>, Anton Babushkin <anton.babushkin@me.com>
#
sh /etc/init.d/4001_quad_x
set MIXER FMU_hexa_x
set PWM_OUTPUTS 123456
@@ -1,37 +0,0 @@
#!nsh
#
# Generic 10” Hexa X geometry
#
# Maintainers: Lorenz Meier <lm@inf.ethz.ch>
#
if [ $DO_AUTOCONFIG == yes ]
then
#
# Default parameters for this platform
#
param set MC_ATT_P 7.0
param set MC_ATT_I 0.0
param set MC_ATT_D 0.0
param set MC_ATTRATE_P 0.12
param set MC_ATTRATE_I 0.0
param set MC_ATTRATE_D 0.004
param set MC_YAWPOS_P 2.0
param set MC_YAWPOS_I 0.0
param set MC_YAWPOS_D 0.0
param set MC_YAWRATE_P 0.3
param set MC_YAWRATE_I 0.2
param set MC_YAWRATE_D 0.005
# TODO add default MPC parameters
fi
set VEHICLE_TYPE mc
set MIXER FMU_hexa_x
set PWM_OUTPUTS 1234
set PWM_RATE 400
# DJI ESC range
set PWM_DISARMED 900
set PWM_MIN 1200
set PWM_MAX 1900
+10
View File
@@ -0,0 +1,10 @@
#!nsh
#
# Generic 10” Hexa + geometry
#
# Maintainers: Lorenz Meier <lm@inf.ethz.ch>, Anton Babushkin <anton.babushkin@me.com>
#
sh /etc/init.d/6001_hexa_x
set MIXER FMU_hexa_+
@@ -1,37 +0,0 @@
#!nsh
#
# Generic 10” Hexa + geometry
#
# Maintainers: Lorenz Meier <lm@inf.ethz.ch>
#
if [ $DO_AUTOCONFIG == yes ]
then
#
# Default parameters for this platform
#
param set MC_ATT_P 7.0
param set MC_ATT_I 0.0
param set MC_ATT_D 0.0
param set MC_ATTRATE_P 0.12
param set MC_ATTRATE_I 0.0
param set MC_ATTRATE_D 0.004
param set MC_YAWPOS_P 2.0
param set MC_YAWPOS_I 0.0
param set MC_YAWPOS_D 0.0
param set MC_YAWRATE_P 0.3
param set MC_YAWRATE_I 0.2
param set MC_YAWRATE_D 0.005
# TODO add default MPC parameters
fi
set VEHICLE_TYPE mc
set MIXER FMU_hexa_+
set PWM_OUTPUTS 1234
set PWM_RATE 400
# DJI ESC range
set PWM_DISARMED 900
set PWM_MIN 1200
set PWM_MAX 1900
+12
View File
@@ -0,0 +1,12 @@
#!nsh
#
# Generic 10” Octo X geometry
#
# Maintainers: Lorenz Meier <lm@inf.ethz.ch>, Anton Babushkin <anton.babushkin@me.com>
#
sh /etc/init.d/4001_quad_x
set MIXER FMU_octo_x
set PWM_OUTPUTS 12345678
@@ -1,37 +0,0 @@
#!nsh
#
# Generic 10” Octo X geometry
#
# Maintainers: Lorenz Meier <lm@inf.ethz.ch>
#
if [ $DO_AUTOCONFIG == yes ]
then
#
# Default parameters for this platform
#
param set MC_ATT_P 7.0
param set MC_ATT_I 0.0
param set MC_ATT_D 0.0
param set MC_ATTRATE_P 0.12
param set MC_ATTRATE_I 0.0
param set MC_ATTRATE_D 0.004
param set MC_YAWPOS_P 2.0
param set MC_YAWPOS_I 0.0
param set MC_YAWPOS_D 0.0
param set MC_YAWRATE_P 0.3
param set MC_YAWRATE_I 0.2
param set MC_YAWRATE_D 0.005
# TODO add default MPC parameters
fi
set VEHICLE_TYPE mc
set MIXER FMU_octo_x
set PWM_OUTPUTS 1234
set PWM_RATE 400
# DJI ESC range
set PWM_DISARMED 900
set PWM_MIN 1200
set PWM_MAX 1900
+10
View File
@@ -0,0 +1,10 @@
#!nsh
#
# Generic 10” Octo + geometry
#
# Maintainers: Lorenz Meier <lm@inf.ethz.ch>, Anton Babushkin <anton.babushkin@me.com>
#
sh /etc/init.d/8001_octo_x
set MIXER FMU_octo_+
@@ -1,37 +0,0 @@
#!nsh
#
# Generic 10” Octo + geometry
#
# Maintainers: Lorenz Meier <lm@inf.ethz.ch>
#
if [ $DO_AUTOCONFIG == yes ]
then
#
# Default parameters for this platform
#
param set MC_ATT_P 7.0
param set MC_ATT_I 0.0
param set MC_ATT_D 0.0
param set MC_ATTRATE_P 0.12
param set MC_ATTRATE_I 0.0
param set MC_ATTRATE_D 0.004
param set MC_YAWPOS_P 2.0
param set MC_YAWPOS_I 0.0
param set MC_YAWPOS_D 0.0
param set MC_YAWRATE_P 0.3
param set MC_YAWRATE_I 0.2
param set MC_YAWRATE_D 0.005
# TODO add default MPC parameters
fi
set VEHICLE_TYPE mc
set MIXER FMU_octo_+
set PWM_OUTPUTS 1234
set PWM_RATE 400
# DJI ESC range
set PWM_DISARMED 900
set PWM_MIN 1200
set PWM_MAX 1900
+8 -13
View File
@@ -101,14 +101,9 @@ fi
# Quad X
#
if param compare SYS_AUTOSTART 4008 8
if param compare SYS_AUTOSTART 4001
then
#sh /etc/init.d/4008_ardrone
fi
if param compare SYS_AUTOSTART 4009 9
then
#sh /etc/init.d/4009_ardrone_flow
sh /etc/init.d/4001_quad_x
fi
if param compare SYS_AUTOSTART 4010 10
@@ -132,7 +127,7 @@ fi
if param compare SYS_AUTOSTART 5001
then
sh /etc/init.d/5001_quad_+_pwm
sh /etc/init.d/5001_quad_+
fi
#
@@ -141,7 +136,7 @@ fi
if param compare SYS_AUTOSTART 6001
then
sh /etc/init.d/6001_hexa_x_pwm
sh /etc/init.d/6001_hexa_x
fi
#
@@ -150,7 +145,7 @@ fi
if param compare SYS_AUTOSTART 7001
then
sh /etc/init.d/7001_hexa_+_pwm
sh /etc/init.d/7001_hexa_+
fi
#
@@ -159,7 +154,7 @@ fi
if param compare SYS_AUTOSTART 8001
then
sh /etc/init.d/8001_octo_x_pwm
sh /etc/init.d/8001_octo_x
fi
#
@@ -168,7 +163,7 @@ fi
if param compare SYS_AUTOSTART 9001
then
sh /etc/init.d/9001_octo_+_pwm
sh /etc/init.d/9001_octo_+
fi
#
@@ -191,5 +186,5 @@ fi
if param compare SYS_AUTOSTART 12001
then
sh /etc/init.d/12001_octo_cox_pwm
sh /etc/init.d/12001_octo_cox
fi
+2 -1
View File
@@ -1,2 +1,3 @@
parameters.wiki
parameters.xml
parameters.xml
cookies.txt
+34 -9
View File
@@ -1,10 +1,24 @@
import output
from xml.sax.saxutils import escape
class DokuWikiOutput(output.Output):
def Generate(self, groups):
result = ""
pre_text = """<?xml version='1.0'?>
<methodCall>
<methodName>wiki.putPage</methodName>
<params>
<param>
<value>
<string>:firmware:parameters</string>
</value>
</param>
<param>
<value>
<string>"""
result = "====== Parameter Reference ======\nThis list is auto-generated every few minutes and contains the most recent parameter names and default values."
for group in groups:
result += "==== %s ====\n\n" % group.GetName()
result += "|< 100% 20% 20% 10% 10% 10% 30%>|\n"
result += "^ Name ^ Description ^ Min ^ Max ^ Default ^ Comment ^\n"
for param in group.GetParams():
code = param.GetFieldValue("code")
@@ -13,25 +27,36 @@ class DokuWikiOutput(output.Output):
result += "| %s | %s " % (code, name)
min_val = param.GetFieldValue("min")
if min_val is not None:
result += "| %s " % min_val
result += " | %s " % min_val
else:
result += "|"
result += " | "
max_val = param.GetFieldValue("max")
if max_val is not None:
result += "| %s " % max_val
result += " | %s " % max_val
else:
result += "|"
result += " | "
def_val = param.GetFieldValue("default")
if def_val is not None:
result += "| %s " % def_val
else:
result += "|"
result += " | "
long_desc = param.GetFieldValue("long_desc")
if long_desc is not None:
long_desc = long_desc.replace("\n", "")
result += "| %s " % long_desc
else:
result += "|"
result += "|\n"
result += " | "
result += " |\n"
result += "\n"
return result
post_text = """</string>
</value>
</param>
<param>
<value>
<name>sum</name>
<string>Updated parameters automagically from code.</string>
</value>
</param>
</params>
</methodCall>"""
return pre_text + escape(result) + post_text
+5
View File
@@ -0,0 +1,5 @@
python px_process_params.py
rm cookies.txt
curl --cookie cookies.txt --cookie-jar cookies.txt --user-agent Mozilla/4.0 --data "u=$XMLRPCUSER&p=$XMLRPCPASS" https://pixhawk.org/start?do=login
curl -k --cookie cookies.txt -H "Content-Type: application/xml" -X POST --data-binary @parameters.wiki "https://pixhawk.org/lib/exe/xmlrpc.php"
+7 -7
View File
@@ -246,14 +246,14 @@
*
* There are sensors on SPI1, and SPI3 is connected to the microSD slot.
*/
#define GPIO_SPI1_MISO GPIO_SPI1_MISO_1
#define GPIO_SPI1_MOSI GPIO_SPI1_MOSI_1
#define GPIO_SPI1_SCK GPIO_SPI1_SCK_1
#define GPIO_SPI1_MISO (GPIO_SPI1_MISO_1|GPIO_SPEED_50MHz)
#define GPIO_SPI1_MOSI (GPIO_SPI1_MOSI_1|GPIO_SPEED_50MHz)
#define GPIO_SPI1_SCK (GPIO_SPI1_SCK_1|GPIO_SPEED_50MHz)
#define GPIO_SPI3_MISO GPIO_SPI3_MISO_2
#define GPIO_SPI3_MOSI GPIO_SPI3_MOSI_1
#define GPIO_SPI3_SCK GPIO_SPI3_SCK_2
#define GPIO_SPI3_NSS GPIO_SPI3_NSS_2
#define GPIO_SPI3_MISO (GPIO_SPI3_MISO_2|GPIO_SPEED_50MHz)
#define GPIO_SPI3_MOSI (GPIO_SPI3_MOSI_1|GPIO_SPEED_50MHz)
#define GPIO_SPI3_SCK (GPIO_SPI3_SCK_2|GPIO_SPEED_50MHz)
#define GPIO_SPI3_NSS (GPIO_SPI3_NSS_2|GPIO_SPEED_50MHz)
/* SPI DMA configuration for SPI3 (microSD) */
#define DMACHAN_SPI3_RX DMAMAP_SPI3_RX_1
+6 -6
View File
@@ -260,13 +260,13 @@
*
* There are sensors on SPI1, and SPI2 is connected to the FRAM.
*/
#define GPIO_SPI1_MISO GPIO_SPI1_MISO_1
#define GPIO_SPI1_MOSI GPIO_SPI1_MOSI_1
#define GPIO_SPI1_SCK GPIO_SPI1_SCK_1
#define GPIO_SPI1_MISO (GPIO_SPI1_MISO_1|GPIO_SPEED_50MHz)
#define GPIO_SPI1_MOSI (GPIO_SPI1_MOSI_1|GPIO_SPEED_50MHz)
#define GPIO_SPI1_SCK (GPIO_SPI1_SCK_1|GPIO_SPEED_50MHz)
#define GPIO_SPI2_MISO GPIO_SPI2_MISO_1
#define GPIO_SPI2_MOSI GPIO_SPI2_MOSI_1
#define GPIO_SPI2_SCK GPIO_SPI2_SCK_2
#define GPIO_SPI2_MISO (GPIO_SPI2_MISO_1|GPIO_SPEED_50MHz)
#define GPIO_SPI2_MOSI (GPIO_SPI2_MOSI_1|GPIO_SPEED_50MHz)
#define GPIO_SPI2_SCK (GPIO_SPI2_SCK_2|GPIO_SPEED_50MHz)
/************************************************************************************
* Public Data
+14
View File
@@ -193,6 +193,20 @@ ORB_DECLARE(output_pwm);
* split between servos and GPIO */
#define PWM_SERVO_SET_COUNT _IOC(_PWM_SERVO_BASE, 20)
/** set the lockdown override flag to enable outputs in HIL */
#define PWM_SERVO_SET_DISABLE_LOCKDOWN _IOC(_PWM_SERVO_BASE, 21)
/** get the lockdown override flag to enable outputs in HIL */
#define PWM_SERVO_GET_DISABLE_LOCKDOWN _IOC(_PWM_SERVO_BASE, 22)
/*
*
*
* WARNING WARNING WARNING! DO NOT EXCEED 31 IN IOC INDICES HERE!
*
*
*/
/** set a single servo to a specific value */
#define PWM_SERVO_SET(_servo) _IOC(_PWM_SERVO_BASE, 0x20 + _servo)
+50 -4
View File
@@ -1,6 +1,6 @@
/****************************************************************************
*
* Copyright (c) 2012, 2013 PX4 Development Team. All rights reserved.
* Copyright (c) 2012-2014 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
@@ -62,6 +62,11 @@
*/
#define RC_INPUT_MAX_CHANNELS 18
/**
* Maximum RSSI value
*/
#define RC_INPUT_RSSI_MAX 255
/**
* Input signal type, value is a control position from zero to 100
* percent.
@@ -83,8 +88,11 @@ enum RC_INPUT_SOURCE {
* on the board involved.
*/
struct rc_input_values {
/** decoding time */
uint64_t timestamp;
/** publication time */
uint64_t timestamp_publication;
/** last valid reception time */
uint64_t timestamp_last_signal;
/** number of channels actually being seen */
uint32_t channel_count;
@@ -92,6 +100,40 @@ struct rc_input_values {
/** receive signal strength indicator (RSSI): < 0: Undefined, 0: no signal, 255: full reception */
int32_t rssi;
/**
* explicit failsafe flag: true on TX failure or TX out of range , false otherwise.
* Only the true state is reliable, as there are some (PPM) receivers on the market going
* into failsafe without telling us explicitly.
* */
bool rc_failsafe;
/**
* RC receiver connection status: True,if no frame has arrived in the expected time, false otherwise.
* True usally means that the receiver has been disconnected, but can also indicate a radio link loss on "stupid" systems.
* Will remain false, if a RX with failsafe option continues to transmit frames after a link loss.
* */
bool rc_lost;
/**
* Number of lost RC frames.
* Note: intended purpose: observe the radio link quality if RSSI is not available
* This value must not be used to trigger any failsafe-alike funtionality.
* */
uint16_t rc_lost_frame_count;
/**
* Number of total RC frames.
* Note: intended purpose: observe the radio link quality if RSSI is not available
* This value must not be used to trigger any failsafe-alike funtionality.
* */
uint16_t rc_total_frame_count;
/**
* Length of a single PPM frame.
* Zero for non-PPM systems
*/
uint16_t rc_ppm_frame_length;
/** Input source */
enum RC_INPUT_SOURCE input_source;
@@ -107,8 +149,12 @@ ORB_DECLARE(input_rc);
#define _RC_INPUT_BASE 0x2b00
/** Fetch R/C input values into (rc_input_values *)arg */
#define RC_INPUT_GET _IOC(_RC_INPUT_BASE, 0)
/** Enable RSSI input via ADC */
#define RC_INPUT_ENABLE_RSSI_ANALOG _IOC(_RC_INPUT_BASE, 1)
/** Enable RSSI input via PWM signal */
#define RC_INPUT_ENABLE_RSSI_PWM _IOC(_RC_INPUT_BASE, 2)
#endif /* _DRV_RC_INPUT_H */
+58
View File
@@ -0,0 +1,58 @@
/****************************************************************************
*
* Copyright (c) 2014 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 drv_sbus.h
*
* Futaba S.BUS / S.BUS 2 compatible interface.
*/
#ifndef _DRV_SBUS_H
#define _DRV_SBUS_H
#include <stdint.h>
#include <sys/ioctl.h>
#include "drv_orb_dev.h"
/**
* Path for the default S.BUS device
*/
#define SBUS_DEVICE_PATH "/dev/sbus"
#define _SBUS_BASE 0x2c00
/** Enable S.BUS version 1 / 2 output (0 to disable) */
#define SBUS_SET_PROTO_VERSION _IOC(_SBUS_BASE, 0)
#endif /* _DRV_SBUS_H */
+10 -2
View File
@@ -626,7 +626,7 @@ PX4FMU::task_main()
#ifdef HRT_PPM_CHANNEL
// see if we have new PPM input data
if (ppm_last_valid_decode != rc_in.timestamp) {
if (ppm_last_valid_decode != rc_in.timestamp_last_signal) {
// we have a new PPM frame. Publish it.
rc_in.channel_count = ppm_decoded_channels;
@@ -638,7 +638,15 @@ PX4FMU::task_main()
rc_in.values[i] = ppm_buffer[i];
}
rc_in.timestamp = ppm_last_valid_decode;
rc_in.timestamp_publication = ppm_last_valid_decode;
rc_in.timestamp_last_signal = ppm_last_valid_decode;
rc_in.rc_ppm_frame_length = ppm_frame_length;
rc_in.rssi = RC_INPUT_RSSI_MAX;
rc_in.rc_failsafe = false;
rc_in.rc_lost = false;
rc_in.rc_lost_frame_count = 0;
rc_in.rc_total_frame_count = 0;
/* lazily advertise on first publication */
if (to_input_rc == 0) {
+227 -32
View File
@@ -61,6 +61,7 @@
#include <drivers/device/device.h>
#include <drivers/drv_rc_input.h>
#include <drivers/drv_pwm_output.h>
#include <drivers/drv_sbus.h>
#include <drivers/drv_gpio.h>
#include <drivers/drv_hrt.h>
#include <drivers/drv_mixer.h>
@@ -238,6 +239,7 @@ private:
unsigned _update_interval; ///< Subscription interval limiting send rate
bool _rc_handling_disabled; ///< If set, IO does not evaluate, but only forward the RC values
unsigned _rc_chan_count; ///< Internal copy of the last seen number of RC channels
uint64_t _rc_last_valid; ///< last valid timestamp
volatile int _task; ///< worker task id
volatile bool _task_should_exit; ///< worker terminate flag
@@ -274,6 +276,7 @@ private:
servorail_status_s _servorail_status; ///< servorail status
bool _primary_pwm_device; ///< true if we are the default PWM output
bool _lockdown_override; ///< allow to override the safety lockdown
float _battery_amp_per_volt; ///< current sensor amps/volt
float _battery_amp_bias; ///< current sensor bias
@@ -444,7 +447,7 @@ private:
* @param vservo vservo register
* @param vrssi vrssi register
*/
void io_handle_vservo(uint16_t vbatt, uint16_t ibatt);
void io_handle_vservo(uint16_t vservo, uint16_t vrssi);
};
@@ -467,6 +470,7 @@ PX4IO::PX4IO(device::Device *interface) :
_update_interval(0),
_rc_handling_disabled(false),
_rc_chan_count(0),
_rc_last_valid(0),
_task(-1),
_task_should_exit(false),
_mavlink_fd(-1),
@@ -490,6 +494,7 @@ PX4IO::PX4IO(device::Device *interface) :
_to_servorail(0),
_to_safety(0),
_primary_pwm_device(false),
_lockdown_override(false),
_battery_amp_per_volt(90.0f / 5.0f), // this matches the 3DR current sensor
_battery_amp_bias(0),
_battery_mamphour_total(0),
@@ -1047,13 +1052,19 @@ PX4IO::io_set_arming_state()
uint16_t set = 0;
uint16_t clear = 0;
if (armed.armed && !armed.lockdown) {
if (armed.armed) {
set |= PX4IO_P_SETUP_ARMING_FMU_ARMED;
} else {
clear |= PX4IO_P_SETUP_ARMING_FMU_ARMED;
}
if (armed.lockdown && !_lockdown_override) {
set |= PX4IO_P_SETUP_ARMING_LOCKDOWN;
} else {
clear |= PX4IO_P_SETUP_ARMING_LOCKDOWN;
}
if (armed.ready_to_arm) {
set |= PX4IO_P_SETUP_ARMING_IO_ARM_OK;
@@ -1357,7 +1368,10 @@ PX4IO::io_get_status()
uint16_t regs[6];
int ret;
/* get STATUS_FLAGS, STATUS_ALARMS, STATUS_VBATT, STATUS_IBATT in that order */
/* get
* STATUS_FLAGS, STATUS_ALARMS, STATUS_VBATT, STATUS_IBATT,
* STATUS_VSERVO, STATUS_VRSSI, STATUS_PRSSI
* in that order */
ret = io_reg_get(PX4IO_PAGE_STATUS, PX4IO_P_STATUS_FLAGS, &regs[0], sizeof(regs) / sizeof(regs[0]));
if (ret != OK)
@@ -1394,7 +1408,8 @@ PX4IO::io_get_raw_rc_input(rc_input_values &input_rc)
*
* This should be the common case (9 channel R/C control being a reasonable upper bound).
*/
input_rc.timestamp = hrt_absolute_time();
input_rc.timestamp_publication = hrt_absolute_time();
ret = io_reg_get(PX4IO_PAGE_RAW_RC_INPUT, PX4IO_P_RAW_RC_COUNT, &regs[0], prolog + 9);
if (ret != OK)
@@ -1404,13 +1419,25 @@ PX4IO::io_get_raw_rc_input(rc_input_values &input_rc)
* Get the channel count any any extra channels. This is no more expensive than reading the
* channel count once.
*/
channel_count = regs[0];
channel_count = regs[PX4IO_P_RAW_RC_COUNT];
if (channel_count != _rc_chan_count)
perf_count(_perf_chan_count);
_rc_chan_count = channel_count;
input_rc.rc_ppm_frame_length = regs[PX4IO_P_RAW_RC_DATA];
input_rc.rssi = regs[PX4IO_P_RAW_RC_NRSSI];
input_rc.rc_failsafe = (regs[PX4IO_P_RAW_RC_FLAGS] & PX4IO_P_RAW_RC_FLAGS_FAILSAFE);
input_rc.rc_lost_frame_count = regs[PX4IO_P_RAW_LOST_FRAME_COUNT];
input_rc.rc_total_frame_count = regs[PX4IO_P_RAW_FRAME_COUNT];
/* rc_lost has to be set before the call to this function */
if (!input_rc.rc_lost && !input_rc.rc_failsafe)
_rc_last_valid = input_rc.timestamp_publication;
input_rc.timestamp_last_signal = _rc_last_valid;
if (channel_count > 9) {
ret = io_reg_get(PX4IO_PAGE_RAW_RC_INPUT, PX4IO_P_RAW_RC_BASE + 9, &regs[prolog + 9], channel_count - 9);
@@ -1427,13 +1454,12 @@ PX4IO::io_get_raw_rc_input(rc_input_values &input_rc)
int
PX4IO::io_publish_raw_rc()
{
/* if no raw RC, just don't publish */
if (!(_status & PX4IO_P_STATUS_FLAGS_RC_OK))
return OK;
/* fetch values from IO */
rc_input_values rc_val;
rc_val.timestamp = hrt_absolute_time();
/* set the RC status flag ORDER MATTERS! */
rc_val.rc_lost = !(_status & PX4IO_P_STATUS_FLAGS_RC_OK);
int ret = io_get_raw_rc_input(rc_val);
@@ -1452,13 +1478,11 @@ PX4IO::io_publish_raw_rc()
} else {
rc_val.input_source = RC_INPUT_SOURCE_UNKNOWN;
}
/* set RSSI */
if (rc_val.input_source != RC_INPUT_SOURCE_PX4IO_SBUS) {
// XXX the correct scaling needs to be validated here
rc_val.rssi = (_servorail_status.rssi_v / 3.3f) * UINT8_MAX;
/* we do not know the RC input, only publish if RC OK flag is set */
/* if no raw RC, just don't publish */
if (!(_status & PX4IO_P_STATUS_FLAGS_RC_OK))
return OK;
}
/* lazily advertise on first publication */
@@ -1767,15 +1791,14 @@ PX4IO::print_status()
printf("%u bytes free\n",
io_reg_get(PX4IO_PAGE_STATUS, PX4IO_P_STATUS_FREEMEM));
uint16_t flags = io_reg_get(PX4IO_PAGE_STATUS, PX4IO_P_STATUS_FLAGS);
printf("status 0x%04x%s%s%s%s%s%s%s%s%s%s%s%s%s\n",
uint16_t io_status_flags = flags;
printf("status 0x%04x%s%s%s%s%s%s%s%s%s%s%s%s\n",
flags,
((flags & PX4IO_P_STATUS_FLAGS_OUTPUTS_ARMED) ? " OUTPUTS_ARMED" : ""),
((flags & PX4IO_P_STATUS_FLAGS_SAFETY_OFF) ? " SAFETY_OFF" : " SAFETY_SAFE"),
((flags & PX4IO_P_STATUS_FLAGS_OVERRIDE) ? " OVERRIDE" : ""),
((flags & PX4IO_P_STATUS_FLAGS_RC_OK) ? " RC_OK" : " RC_FAIL"),
((flags & PX4IO_P_STATUS_FLAGS_RC_PPM) ? " PPM" : ""),
(((flags & PX4IO_P_STATUS_FLAGS_RC_DSM) && (!(flags & PX4IO_P_STATUS_FLAGS_RC_DSM11))) ? " DSM10" : ""),
(((flags & PX4IO_P_STATUS_FLAGS_RC_DSM) && (flags & PX4IO_P_STATUS_FLAGS_RC_DSM11)) ? " DSM11" : ""),
((flags & PX4IO_P_STATUS_FLAGS_RC_SBUS) ? " SBUS" : ""),
((flags & PX4IO_P_STATUS_FLAGS_FMU_OK) ? " FMU_OK" : " FMU_FAIL"),
((flags & PX4IO_P_STATUS_FLAGS_RAW_PWM) ? " RAW_PWM_PASSTHROUGH" : ""),
@@ -1834,8 +1857,17 @@ PX4IO::print_status()
printf("\n");
if ((flags & PX4IO_P_STATUS_FLAGS_RC_PPM)) {
int frame_len = io_reg_get(PX4IO_PAGE_STATUS, PX4IO_P_STATUS_RC_DATA);
flags = io_reg_get(PX4IO_PAGE_RAW_RC_INPUT, PX4IO_P_RAW_RC_FLAGS);
printf("R/C flags: 0x%04x%s%s%s%s%s\n", flags,
(((io_status_flags & PX4IO_P_STATUS_FLAGS_RC_DSM) && (!(flags & PX4IO_P_RAW_RC_FLAGS_RC_DSM11))) ? " DSM10" : ""),
(((io_status_flags & PX4IO_P_STATUS_FLAGS_RC_DSM) && (flags & PX4IO_P_RAW_RC_FLAGS_RC_DSM11)) ? " DSM11" : ""),
((flags & PX4IO_P_RAW_RC_FLAGS_FRAME_DROP) ? " FRAME_DROP" : ""),
((flags & PX4IO_P_RAW_RC_FLAGS_FAILSAFE) ? " FAILSAFE" : ""),
((flags & PX4IO_P_RAW_RC_FLAGS_MAPPING_OK) ? " MAPPING_OK" : "")
);
if ((io_status_flags & PX4IO_P_STATUS_FLAGS_RC_PPM)) {
int frame_len = io_reg_get(PX4IO_PAGE_RAW_RC_INPUT, PX4IO_P_RAW_RC_DATA);
printf("RC data (PPM frame len) %u us\n", frame_len);
if ((frame_len - raw_inputs * 2000 - 3000) < 0) {
@@ -1861,16 +1893,23 @@ PX4IO::print_status()
printf("\n");
/* setup and state */
printf("features 0x%04x\n", io_reg_get(PX4IO_PAGE_SETUP, PX4IO_P_SETUP_FEATURES));
uint16_t features = io_reg_get(PX4IO_PAGE_SETUP, PX4IO_P_SETUP_FEATURES);
printf("features 0x%04x%s%s%s%s\n", features,
((features & PX4IO_P_SETUP_FEATURES_SBUS1_OUT) ? " S.BUS1_OUT" : ""),
((features & PX4IO_P_SETUP_FEATURES_SBUS2_OUT) ? " S.BUS2_OUT" : ""),
((features & PX4IO_P_SETUP_FEATURES_PWM_RSSI) ? " RSSI_PWM" : ""),
((features & PX4IO_P_SETUP_FEATURES_ADC_RSSI) ? " RSSI_ADC" : "")
);
uint16_t arming = io_reg_get(PX4IO_PAGE_SETUP, PX4IO_P_SETUP_ARMING);
printf("arming 0x%04x%s%s%s%s%s%s\n",
printf("arming 0x%04x%s%s%s%s%s%s%s\n",
arming,
((arming & PX4IO_P_SETUP_ARMING_FMU_ARMED) ? " FMU_ARMED" : " FMU_DISARMED"),
((arming & PX4IO_P_SETUP_ARMING_IO_ARM_OK) ? " IO_ARM_OK" : " IO_ARM_DENIED"),
((arming & PX4IO_P_SETUP_ARMING_MANUAL_OVERRIDE_OK) ? " MANUAL_OVERRIDE_OK" : ""),
((arming & PX4IO_P_SETUP_ARMING_FAILSAFE_CUSTOM) ? " FAILSAFE_CUSTOM" : ""),
((arming & PX4IO_P_SETUP_ARMING_INAIR_RESTART_OK) ? " INAIR_RESTART_OK" : ""),
((arming & PX4IO_P_SETUP_ARMING_ALWAYS_PWM_ENABLE) ? " ALWAYS_PWM_ENABLE" : ""));
((arming & PX4IO_P_SETUP_ARMING_FMU_ARMED) ? " FMU_ARMED" : " FMU_DISARMED"),
((arming & PX4IO_P_SETUP_ARMING_IO_ARM_OK) ? " IO_ARM_OK" : " IO_ARM_DENIED"),
((arming & PX4IO_P_SETUP_ARMING_MANUAL_OVERRIDE_OK) ? " MANUAL_OVERRIDE_OK" : ""),
((arming & PX4IO_P_SETUP_ARMING_FAILSAFE_CUSTOM) ? " FAILSAFE_CUSTOM" : ""),
((arming & PX4IO_P_SETUP_ARMING_INAIR_RESTART_OK) ? " INAIR_RESTART_OK" : ""),
((arming & PX4IO_P_SETUP_ARMING_ALWAYS_PWM_ENABLE) ? " ALWAYS_PWM_ENABLE" : ""),
((arming & PX4IO_P_SETUP_ARMING_LOCKDOWN) ? " LOCKDOWN" : ""));
#ifdef CONFIG_ARCH_BOARD_PX4FMU_V1
printf("rates 0x%04x default %u alt %u relays 0x%04x\n",
io_reg_get(PX4IO_PAGE_SETUP, PX4IO_P_SETUP_PWM_RATES),
@@ -2067,6 +2106,14 @@ PX4IO::ioctl(file * /*filep*/, int cmd, unsigned long arg)
*(unsigned *)arg = _max_actuators;
break;
case PWM_SERVO_SET_DISABLE_LOCKDOWN:
_lockdown_override = arg;
break;
case PWM_SERVO_GET_DISABLE_LOCKDOWN:
*(unsigned *)arg = _lockdown_override;
break;
case DSM_BIND_START:
io_reg_set(PX4IO_PAGE_SETUP, PX4IO_P_SETUP_DSM, dsm_bind_power_down);
usleep(500000);
@@ -2283,6 +2330,38 @@ PX4IO::ioctl(file * /*filep*/, int cmd, unsigned long arg)
break;
case RC_INPUT_ENABLE_RSSI_ANALOG:
if (arg) {
ret = io_reg_modify(PX4IO_PAGE_SETUP, PX4IO_P_SETUP_FEATURES, 0, PX4IO_P_SETUP_FEATURES_ADC_RSSI);
} else {
ret = io_reg_modify(PX4IO_PAGE_SETUP, PX4IO_P_SETUP_FEATURES, PX4IO_P_SETUP_FEATURES_ADC_RSSI, 0);
}
break;
case RC_INPUT_ENABLE_RSSI_PWM:
if (arg) {
ret = io_reg_modify(PX4IO_PAGE_SETUP, PX4IO_P_SETUP_FEATURES, 0, PX4IO_P_SETUP_FEATURES_PWM_RSSI);
} else {
ret = io_reg_modify(PX4IO_PAGE_SETUP, PX4IO_P_SETUP_FEATURES, PX4IO_P_SETUP_FEATURES_PWM_RSSI, 0);
}
break;
case SBUS_SET_PROTO_VERSION:
if (arg == 1) {
ret = io_reg_modify(PX4IO_PAGE_SETUP, PX4IO_P_SETUP_FEATURES, 0, PX4IO_P_SETUP_FEATURES_SBUS1_OUT);
} else if (arg == 2) {
ret = io_reg_modify(PX4IO_PAGE_SETUP, PX4IO_P_SETUP_FEATURES, 0, PX4IO_P_SETUP_FEATURES_SBUS2_OUT);
} else {
ret = io_reg_modify(PX4IO_PAGE_SETUP, PX4IO_P_SETUP_FEATURES, (PX4IO_P_SETUP_FEATURES_SBUS1_OUT | PX4IO_P_SETUP_FEATURES_SBUS2_OUT), 0);
}
break;
default:
/* not a recognized value */
ret = -ENOTTY;
@@ -2656,7 +2735,7 @@ monitor(void)
/* clear screen */
printf("\033[2J");
unsigned cancels = 3;
unsigned cancels = 2;
for (;;) {
pollfd fds[1];
@@ -2692,13 +2771,72 @@ void
if_test(unsigned mode)
{
device::Device *interface = get_interface();
int result;
int result = interface->ioctl(1, mode); /* XXX magic numbers */
delete interface;
if (interface) {
result = interface->ioctl(1, mode); /* XXX magic numbers */
delete interface;
} else {
errx(1, "interface not loaded, exiting");
}
errx(0, "test returned %d", result);
}
void
lockdown(int argc, char *argv[])
{
if (g_dev != nullptr) {
if (argc > 2 && !strcmp(argv[2], "disable")) {
warnx("WARNING: ACTUATORS WILL BE LIVE IN HIL! PROCEED?");
warnx("Press 'y' to enable, any other key to abort.");
/* check if user wants to abort */
char c;
struct pollfd fds;
int ret;
hrt_abstime start = hrt_absolute_time();
const unsigned long timeout = 5000000;
while (hrt_elapsed_time(&start) < timeout) {
fds.fd = 0; /* stdin */
fds.events = POLLIN;
ret = poll(&fds, 1, 0);
if (ret > 0) {
read(0, &c, 1);
if (c != 'y') {
exit(0);
} else if (c == 'y') {
break;
}
}
usleep(10000);
}
if (hrt_elapsed_time(&start) > timeout)
errx(1, "TIMEOUT! ABORTED WITHOUT CHANGES.");
(void)g_dev->ioctl(0, PWM_SERVO_SET_DISABLE_LOCKDOWN, 1);
warnx("WARNING: ACTUATORS ARE NOW LIVE IN HIL!");
} else {
(void)g_dev->ioctl(0, PWM_SERVO_SET_DISABLE_LOCKDOWN, 0);
warnx("ACTUATORS ARE NOW SAFE IN HIL.");
}
} else {
errx(1, "driver not loaded, exiting");
}
exit(0);
}
} /* namespace */
int
@@ -2932,6 +3070,63 @@ px4io_main(int argc, char *argv[])
if (!strcmp(argv[1], "bind"))
bind(argc, argv);
if (!strcmp(argv[1], "lockdown"))
lockdown(argc, argv);
if (!strcmp(argv[1], "sbus1_out")) {
/* we can cheat and call the driver directly, as it
* doesn't reference filp in ioctl()
*/
int ret = g_dev->ioctl(nullptr, SBUS_SET_PROTO_VERSION, 1);
if (ret != 0) {
errx(ret, "S.BUS v1 failed");
}
exit(0);
}
if (!strcmp(argv[1], "sbus2_out")) {
/* we can cheat and call the driver directly, as it
* doesn't reference filp in ioctl()
*/
int ret = g_dev->ioctl(nullptr, SBUS_SET_PROTO_VERSION, 2);
if (ret != 0) {
errx(ret, "S.BUS v2 failed");
}
exit(0);
}
if (!strcmp(argv[1], "rssi_analog")) {
/* we can cheat and call the driver directly, as it
* doesn't reference filp in ioctl()
*/
int ret = g_dev->ioctl(nullptr, RC_INPUT_ENABLE_RSSI_ANALOG, 1);
if (ret != 0) {
errx(ret, "RSSI analog failed");
}
exit(0);
}
if (!strcmp(argv[1], "rssi_pwm")) {
/* we can cheat and call the driver directly, as it
* doesn't reference filp in ioctl()
*/
int ret = g_dev->ioctl(nullptr, RC_INPUT_ENABLE_RSSI_PWM, 1);
if (ret != 0) {
errx(ret, "RSSI PWM failed");
}
exit(0);
}
out:
errx(1, "need a command, try 'start', 'stop', 'status', 'test', 'monitor', 'debug',\n 'recovery', 'limit', 'current', 'bind', 'checkcrc', 'forceupdate' or 'update'");
errx(1, "need a command, try 'start', 'stop', 'status', 'test', 'monitor', 'debug <level>',\n"
"'recovery', 'limit <rate>', 'current', 'bind', 'checkcrc',\n"
"'forceupdate', 'update', 'sbus1_out', 'sbus2_out', 'rssi_analog' or 'rssi_pwm'");
}
@@ -68,7 +68,7 @@ PARAM_DEFINE_FLOAT(ATT_YAW_OFF3, 0.0f);
/* magnetic declination, in degrees */
PARAM_DEFINE_FLOAT(ATT_MAG_DECL, 0.0f);
PARAM_DEFINE_INT32(ATT_ACC_COMP, 0);
PARAM_DEFINE_INT32(ATT_ACC_COMP, 2);
int parameters_init(struct attitude_estimator_ekf_param_handles *h)
{
+44 -5
View File
@@ -154,6 +154,11 @@ static bool on_usb_power = false;
static float takeoff_alt = 5.0f;
static struct vehicle_status_s status;
static struct actuator_armed_s armed;
static struct safety_s safety;
static struct vehicle_control_mode_s control_mode;
/* tasks waiting for low prio thread */
typedef enum {
LOW_PRIO_TASK_NONE = 0,
@@ -212,6 +217,11 @@ void print_reject_arm(const char *msg);
void print_status();
int arm();
int disarm();
transition_result_t check_navigation_state_machine(struct vehicle_status_s *status, struct vehicle_control_mode_s *control_mode, struct vehicle_local_position_s *local_pos);
/**
* Loop that runs at a lower rate and priority for calibration and parameter tasks.
*/
@@ -277,6 +287,16 @@ int commander_main(int argc, char *argv[])
exit(0);
}
if (!strcmp(argv[1], "arm")) {
arm();
exit(0);
}
if (!strcmp(argv[1], "disarm")) {
disarm();
exit(0);
}
usage("unrecognized command");
exit(1);
}
@@ -343,6 +363,30 @@ void print_status()
static orb_advert_t status_pub;
int arm()
{
int arming_res = arming_state_transition(&status, &safety, ARMING_STATE_ARMED, &armed);
if (arming_res == TRANSITION_CHANGED) {
mavlink_log_info(mavlink_fd, "[cmd] ARMED by commandline");
return 0;
} else {
return 1;
}
}
int disarm()
{
int arming_res = arming_state_transition(&status, &safety, ARMING_STATE_STANDBY, &armed);
if (arming_res == TRANSITION_CHANGED) {
mavlink_log_info(mavlink_fd, "[cmd] ARMED by commandline");
return 0;
} else {
return 1;
}
}
bool handle_command(struct vehicle_status_s *status, const struct safety_s *safety, struct vehicle_command_s *cmd, struct actuator_armed_s *armed)
{
/* result of the command */
@@ -561,11 +605,6 @@ bool handle_command(struct vehicle_status_s *status, const struct safety_s *safe
}
static struct vehicle_status_s status;
static struct vehicle_control_mode_s control_mode;
static struct actuator_armed_s armed;
static struct safety_s safety;
int commander_thread_main(int argc, char *argv[])
{
/* not yet initialized */
+2 -2
View File
@@ -354,10 +354,10 @@ l_input_rc(const struct listener *l)
const unsigned port_width = 8;
for (unsigned i = 0; (i * port_width) < (rc_raw.channel_count + port_width); i++) {
for (unsigned i = 0; (i * port_width) < rc_raw.channel_count; i++) {
/* Channels are sent in MAVLink main loop at a fixed interval */
mavlink_msg_rc_channels_raw_send(chan,
rc_raw.timestamp / 1000,
rc_raw.timestamp_publication / 1000,
i,
(rc_raw.channel_count > (i * port_width) + 0) ? rc_raw.values[(i * port_width) + 0] : UINT16_MAX,
(rc_raw.channel_count > (i * port_width) + 1) ? rc_raw.values[(i * port_width) + 1] : UINT16_MAX,
File diff suppressed because it is too large Load Diff
@@ -41,13 +41,16 @@
#include <systemlib/param/param.h>
PARAM_DEFINE_FLOAT(MC_ATT_P, 6.0f);
PARAM_DEFINE_FLOAT(MC_ATT_I, 0.0f);
PARAM_DEFINE_FLOAT(MC_ROLL_P, 6.0f);
PARAM_DEFINE_FLOAT(MC_ROLLRATE_P, 0.1f);
PARAM_DEFINE_FLOAT(MC_ROLLRATE_I, 0.0f);
PARAM_DEFINE_FLOAT(MC_ROLLRATE_D, 0.002f);
PARAM_DEFINE_FLOAT(MC_PITCH_P, 6.0f);
PARAM_DEFINE_FLOAT(MC_PITCHRATE_P, 0.1f);
PARAM_DEFINE_FLOAT(MC_PITCHRATE_I, 0.0f);
PARAM_DEFINE_FLOAT(MC_PITCHRATE_D, 0.002f);
PARAM_DEFINE_FLOAT(MC_YAW_P, 2.0f);
PARAM_DEFINE_FLOAT(MC_YAW_I, 0.0f);
PARAM_DEFINE_FLOAT(MC_ATTRATE_P, 0.1f);
PARAM_DEFINE_FLOAT(MC_ATTRATE_I, 0.0f);
PARAM_DEFINE_FLOAT(MC_ATTRATE_D, 0.002f);
PARAM_DEFINE_FLOAT(MC_YAWRATE_P, 0.3f);
PARAM_DEFINE_FLOAT(MC_YAWRATE_I, 0.0f);
PARAM_DEFINE_FLOAT(MC_YAWRATE_D, 0.0f);
PARAM_DEFINE_FLOAT(MC_YAW_FF, 0.5f);
@@ -153,7 +153,6 @@ private:
param_t rc_scale_pitch;
param_t rc_scale_roll;
param_t rc_scale_yaw;
} _params_handles; /**< handles for interesting parameters */
struct {
@@ -165,7 +164,6 @@ private:
float rc_scale_pitch;
float rc_scale_roll;
float rc_scale_yaw;
math::Vector<3> pos_p;
math::Vector<3> vel_p;
@@ -312,7 +310,6 @@ MulticopterPositionControl::MulticopterPositionControl() :
_params_handles.land_tilt_max = param_find("MPC_LAND_TILT");
_params_handles.rc_scale_pitch = param_find("RC_SCALE_PITCH");
_params_handles.rc_scale_roll = param_find("RC_SCALE_ROLL");
_params_handles.rc_scale_yaw = param_find("RC_SCALE_YAW");
/* fetch initial parameter values */
parameters_update(true);
@@ -361,7 +358,6 @@ MulticopterPositionControl::parameters_update(bool force)
param_get(_params_handles.land_tilt_max, &_params.land_tilt_max);
param_get(_params_handles.rc_scale_pitch, &_params.rc_scale_pitch);
param_get(_params_handles.rc_scale_roll, &_params.rc_scale_roll);
param_get(_params_handles.rc_scale_yaw, &_params.rc_scale_yaw);
float v;
param_get(_params_handles.xy_p, &v);
@@ -649,7 +645,7 @@ MulticopterPositionControl::task_main()
if (pos_sp_offs_norm > 1.0f) {
pos_sp_offs /= pos_sp_offs_norm;
add_vector_to_global_position(_lat_sp, _lon_sp, pos_sp_offs(0) * _params.sp_offs_max(0), pos_sp_offs(1) * _params.sp_offs_max(1), &_lat_sp, &_lon_sp);
add_vector_to_global_position(_global_pos.lat, _global_pos.lon, pos_sp_offs(0) * _params.sp_offs_max(0), pos_sp_offs(1) * _params.sp_offs_max(1), &_lat_sp, &_lon_sp);
_alt_sp = alt - pos_sp_offs(2) * _params.sp_offs_max(2);
}
@@ -676,7 +672,7 @@ MulticopterPositionControl::task_main()
_pos_sp_triplet_pub = orb_advertise(ORB_ID(position_setpoint_triplet), &_pos_sp_triplet);
}
} else if (_control_mode.flag_control_auto_enabled) {
} else {
/* always use AMSL altitude for AUTO */
select_alt(true);
@@ -692,22 +688,24 @@ MulticopterPositionControl::task_main()
_reset_lat_lon_sp = true;
_reset_alt_sp = true;
/* update position setpoint */
_lat_sp = _pos_sp_triplet.current.lat;
_lon_sp = _pos_sp_triplet.current.lon;
_alt_sp = _pos_sp_triplet.current.alt;
/* update yaw setpoint if needed */
if (isfinite(_pos_sp_triplet.current.yaw)) {
_att_sp.yaw_body = _pos_sp_triplet.current.yaw;
}
} else {
/* no waypoint, loiter, reset position setpoint if needed */
reset_lat_lon_sp();
reset_alt_sp();
}
} else {
/* no control, reset setpoint */
reset_lat_lon_sp();
reset_alt_sp();
}
if (_control_mode.flag_control_auto_enabled && _pos_sp_triplet.current.valid && _pos_sp_triplet.current.type == SETPOINT_TYPE_IDLE) {
if (!_control_mode.flag_control_manual_enabled && _pos_sp_triplet.current.valid && _pos_sp_triplet.current.type == SETPOINT_TYPE_IDLE) {
/* idle state, don't run controller and set zero thrust */
R.identity();
memcpy(&_att_sp.R_body[0][0], R.data, sizeof(_att_sp.R_body));
@@ -715,7 +713,7 @@ MulticopterPositionControl::task_main()
_att_sp.roll_body = 0.0f;
_att_sp.pitch_body = 0.0f;
_att_sp.yaw_body = 0.0f;
_att_sp.yaw_body = _att.yaw;
_att_sp.thrust = 0.0f;
_att_sp.timestamp = hrt_absolute_time();
@@ -749,7 +747,7 @@ MulticopterPositionControl::task_main()
}
/* use constant descend rate when landing, ignore altitude setpoint */
if (_control_mode.flag_control_auto_enabled && _pos_sp_triplet.current.valid && _pos_sp_triplet.current.type == SETPOINT_TYPE_LAND) {
if (!_control_mode.flag_control_manual_enabled && _pos_sp_triplet.current.valid && _pos_sp_triplet.current.type == SETPOINT_TYPE_LAND) {
_vel_sp(2) = _params.land_speed;
}
@@ -843,30 +841,38 @@ MulticopterPositionControl::task_main()
thr_min = 0.0f;
}
float tilt_max = _params.tilt_max;
/* adjust limits for landing mode */
if (!_control_mode.flag_control_manual_enabled && _pos_sp_triplet.current.valid &&
_pos_sp_triplet.current.type == SETPOINT_TYPE_LAND) {
/* limit max tilt and min lift when landing */
tilt_max = _params.land_tilt_max;
if (thr_min < 0.0f)
thr_min = 0.0f;
}
/* limit min lift */
if (-thrust_sp(2) < thr_min) {
thrust_sp(2) = -thr_min;
saturation_z = true;
}
/* limit max tilt */
float tilt = atan2f(math::Vector<2>(thrust_sp(0), thrust_sp(1)).length(), -thrust_sp(2));
float tilt_max = _params.tilt_max;
if (!_control_mode.flag_control_manual_enabled) {
if (_pos_sp_triplet.current.valid && _pos_sp_triplet.current.type == SETPOINT_TYPE_LAND) {
/* limit max tilt and min lift when landing */
tilt_max = _params.land_tilt_max;
if (thr_min < 0.0f)
thr_min = 0.0f;
}
}
if (_control_mode.flag_control_velocity_enabled) {
if (tilt > tilt_max && thr_min >= 0.0f) {
/* crop horizontal component */
float k = tanf(tilt_max) / tanf(tilt);
thrust_sp(0) *= k;
thrust_sp(1) *= k;
saturation_xy = true;
/* limit max tilt */
if (thr_min >= 0.0f && tilt_max < M_PI / 2 - 0.05f) {
/* absolute horizontal thrust */
float thrust_sp_xy_len = math::Vector<2>(thrust_sp(0), thrust_sp(1)).length();
if (thrust_sp_xy_len > 0.01f) {
/* max horizontal thrust for given vertical thrust*/
float thrust_xy_max = -thrust_sp(2) * tanf(tilt_max);
if (thrust_sp_xy_len > thrust_xy_max) {
float k = thrust_xy_max / thrust_sp_xy_len;
thrust_sp(0) *= k;
thrust_sp(1) *= k;
saturation_xy = true;
}
}
}
} else {
/* thrust compensation for altitude only control mode */
+134 -89
View File
@@ -1,6 +1,6 @@
/****************************************************************************
*
* Copyright (C) 2012 PX4 Development Team. All rights reserved.
* Copyright (c) 2012-2014 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
@@ -59,6 +59,11 @@ static perf_counter_t c_gather_ppm;
void
controls_init(void)
{
/* no channels */
r_raw_rc_count = 0;
system_state.rc_channels_timestamp_received = 0;
system_state.rc_channels_timestamp_valid = 0;
/* DSM input (USART1) */
dsm_init("/dev/ttyS0");
@@ -97,35 +102,62 @@ controls_tick() {
/* receive signal strenght indicator (RSSI). 0 = no connection, 255: perfect connection */
uint16_t rssi = 0;
#ifdef ADC_RSSI
if (r_setup_features & PX4IO_P_SETUP_FEATURES_ADC_RSSI) {
unsigned counts = adc_measure(ADC_RSSI);
if (counts != 0xffff) {
/* use 1:1 scaling on 3.3V ADC input */
unsigned mV = counts * 3300 / 4096;
/* scale to 0..253 */
rssi = mV / 13;
}
}
#endif
perf_begin(c_gather_dsm);
uint16_t temp_count = r_raw_rc_count;
bool dsm_updated = dsm_input(r_raw_rc_values, &temp_count);
if (dsm_updated) {
r_status_flags |= PX4IO_P_STATUS_FLAGS_RC_DSM;
r_raw_rc_flags |= PX4IO_P_STATUS_FLAGS_RC_DSM;
r_raw_rc_count = temp_count & 0x7fff;
if (temp_count & 0x8000)
r_status_flags |= PX4IO_P_STATUS_FLAGS_RC_DSM11;
r_raw_rc_flags |= PX4IO_P_RAW_RC_FLAGS_RC_DSM11;
else
r_status_flags &= ~PX4IO_P_STATUS_FLAGS_RC_DSM11;
r_raw_rc_flags &= ~PX4IO_P_RAW_RC_FLAGS_RC_DSM11;
r_raw_rc_flags &= ~(PX4IO_P_RAW_RC_FLAGS_FRAME_DROP);
r_raw_rc_flags &= ~(PX4IO_P_RAW_RC_FLAGS_FAILSAFE);
rssi = 255;
}
perf_end(c_gather_dsm);
perf_begin(c_gather_sbus);
bool sbus_updated = sbus_input(r_raw_rc_values, &r_raw_rc_count, &rssi, PX4IO_RC_INPUT_CHANNELS);
bool sbus_status = (r_status_flags & PX4IO_P_STATUS_FLAGS_RC_SBUS);
bool sbus_failsafe, sbus_frame_drop;
bool sbus_updated = sbus_input(r_raw_rc_values, &r_raw_rc_count, &sbus_failsafe, &sbus_frame_drop, PX4IO_RC_INPUT_CHANNELS);
if (sbus_updated) {
r_status_flags |= PX4IO_P_STATUS_FLAGS_RC_SBUS;
}
/* switch S.Bus output pin as needed */
if (sbus_status != (r_status_flags & PX4IO_P_STATUS_FLAGS_RC_SBUS)) {
#ifdef ENABLE_SBUS_OUT
ENABLE_SBUS_OUT((r_status_flags & PX4IO_P_STATUS_FLAGS_RC_SBUS));
#endif
rssi = 255;
if (sbus_frame_drop) {
r_raw_rc_flags |= PX4IO_P_RAW_RC_FLAGS_FRAME_DROP;
rssi = 100;
} else {
r_raw_rc_flags &= ~(PX4IO_P_RAW_RC_FLAGS_FRAME_DROP);
}
if (sbus_failsafe) {
r_raw_rc_flags |= PX4IO_P_RAW_RC_FLAGS_FAILSAFE;
rssi = 0;
} else {
r_raw_rc_flags &= ~(PX4IO_P_RAW_RC_FLAGS_FAILSAFE);
}
}
perf_end(c_gather_sbus);
@@ -136,13 +168,12 @@ controls_tick() {
* disable the PPM decoder completely if we have S.bus signal.
*/
perf_begin(c_gather_ppm);
bool ppm_updated = ppm_input(r_raw_rc_values, &r_raw_rc_count, &r_page_status[PX4IO_P_STATUS_RC_DATA]);
bool ppm_updated = ppm_input(r_raw_rc_values, &r_raw_rc_count, &r_page_raw_rc_input[PX4IO_P_RAW_RC_DATA]);
if (ppm_updated) {
/* XXX sample RSSI properly here */
rssi = 255;
r_status_flags |= PX4IO_P_STATUS_FLAGS_RC_PPM;
r_raw_rc_flags &= ~(PX4IO_P_RAW_RC_FLAGS_FRAME_DROP);
r_raw_rc_flags &= ~(PX4IO_P_RAW_RC_FLAGS_FAILSAFE);
}
perf_end(c_gather_ppm);
@@ -150,6 +181,9 @@ controls_tick() {
if (r_raw_rc_count > PX4IO_RC_INPUT_CHANNELS)
r_raw_rc_count = PX4IO_RC_INPUT_CHANNELS;
/* store RSSI */
r_page_raw_rc_input[PX4IO_P_RAW_RC_NRSSI] = rssi;
/*
* In some cases we may have received a frame, but input has still
* been lost.
@@ -161,97 +195,100 @@ controls_tick() {
*/
if (dsm_updated || sbus_updated || ppm_updated) {
/* update RC-received timestamp */
system_state.rc_channels_timestamp = hrt_absolute_time();
/* record a bitmask of channels assigned */
unsigned assigned_channels = 0;
/* map raw inputs to mapped inputs */
/* XXX mapping should be atomic relative to protocol */
for (unsigned i = 0; i < r_raw_rc_count; i++) {
/* update RC-received timestamp */
system_state.rc_channels_timestamp_received = hrt_absolute_time();
/* map the input channel */
uint16_t *conf = &r_page_rc_input_config[i * PX4IO_P_RC_CONFIG_STRIDE];
/* do not command anything in failsafe, kick in the RC loss counter */
if (!(r_raw_rc_flags & PX4IO_P_RAW_RC_FLAGS_FAILSAFE)) {
if (conf[PX4IO_P_RC_CONFIG_OPTIONS] & PX4IO_P_RC_CONFIG_OPTIONS_ENABLED) {
/* update RC-received timestamp */
system_state.rc_channels_timestamp_valid = system_state.rc_channels_timestamp_received;
uint16_t raw = r_raw_rc_values[i];
/* map raw inputs to mapped inputs */
/* XXX mapping should be atomic relative to protocol */
for (unsigned i = 0; i < r_raw_rc_count; i++) {
int16_t scaled;
/* map the input channel */
uint16_t *conf = &r_page_rc_input_config[i * PX4IO_P_RC_CONFIG_STRIDE];
/*
* 1) Constrain to min/max values, as later processing depends on bounds.
*/
if (raw < conf[PX4IO_P_RC_CONFIG_MIN])
raw = conf[PX4IO_P_RC_CONFIG_MIN];
if (raw > conf[PX4IO_P_RC_CONFIG_MAX])
raw = conf[PX4IO_P_RC_CONFIG_MAX];
if (conf[PX4IO_P_RC_CONFIG_OPTIONS] & PX4IO_P_RC_CONFIG_OPTIONS_ENABLED) {
/*
* 2) Scale around the mid point differently for lower and upper range.
*
* This is necessary as they don't share the same endpoints and slope.
*
* First normalize to 0..1 range with correct sign (below or above center),
* then scale to 20000 range (if center is an actual center, -10000..10000,
* if parameters only support half range, scale to 10000 range, e.g. if
* center == min 0..10000, if center == max -10000..0).
*
* As the min and max bounds were enforced in step 1), division by zero
* cannot occur, as for the case of center == min or center == max the if
* statement is mutually exclusive with the arithmetic NaN case.
*
* DO NOT REMOVE OR ALTER STEP 1!
*/
if (raw > (conf[PX4IO_P_RC_CONFIG_CENTER] + conf[PX4IO_P_RC_CONFIG_DEADZONE])) {
scaled = 10000.0f * ((raw - conf[PX4IO_P_RC_CONFIG_CENTER] - conf[PX4IO_P_RC_CONFIG_DEADZONE]) / (float)(conf[PX4IO_P_RC_CONFIG_MAX] - conf[PX4IO_P_RC_CONFIG_CENTER] - conf[PX4IO_P_RC_CONFIG_DEADZONE]));
uint16_t raw = r_raw_rc_values[i];
} else if (raw < (conf[PX4IO_P_RC_CONFIG_CENTER] - conf[PX4IO_P_RC_CONFIG_DEADZONE])) {
scaled = 10000.0f * ((raw - conf[PX4IO_P_RC_CONFIG_CENTER] + conf[PX4IO_P_RC_CONFIG_DEADZONE]) / (float)(conf[PX4IO_P_RC_CONFIG_CENTER] - conf[PX4IO_P_RC_CONFIG_DEADZONE] - conf[PX4IO_P_RC_CONFIG_MIN]));
int16_t scaled;
} else {
/* in the configured dead zone, output zero */
scaled = 0;
}
/*
* 1) Constrain to min/max values, as later processing depends on bounds.
*/
if (raw < conf[PX4IO_P_RC_CONFIG_MIN])
raw = conf[PX4IO_P_RC_CONFIG_MIN];
if (raw > conf[PX4IO_P_RC_CONFIG_MAX])
raw = conf[PX4IO_P_RC_CONFIG_MAX];
/* invert channel if requested */
if (conf[PX4IO_P_RC_CONFIG_OPTIONS] & PX4IO_P_RC_CONFIG_OPTIONS_REVERSE)
scaled = -scaled;
/*
* 2) Scale around the mid point differently for lower and upper range.
*
* This is necessary as they don't share the same endpoints and slope.
*
* First normalize to 0..1 range with correct sign (below or above center),
* then scale to 20000 range (if center is an actual center, -10000..10000,
* if parameters only support half range, scale to 10000 range, e.g. if
* center == min 0..10000, if center == max -10000..0).
*
* As the min and max bounds were enforced in step 1), division by zero
* cannot occur, as for the case of center == min or center == max the if
* statement is mutually exclusive with the arithmetic NaN case.
*
* DO NOT REMOVE OR ALTER STEP 1!
*/
if (raw > (conf[PX4IO_P_RC_CONFIG_CENTER] + conf[PX4IO_P_RC_CONFIG_DEADZONE])) {
scaled = 10000.0f * ((raw - conf[PX4IO_P_RC_CONFIG_CENTER] - conf[PX4IO_P_RC_CONFIG_DEADZONE]) / (float)(conf[PX4IO_P_RC_CONFIG_MAX] - conf[PX4IO_P_RC_CONFIG_CENTER] - conf[PX4IO_P_RC_CONFIG_DEADZONE]));
/* and update the scaled/mapped version */
unsigned mapped = conf[PX4IO_P_RC_CONFIG_ASSIGNMENT];
if (mapped < PX4IO_CONTROL_CHANNELS) {
} else if (raw < (conf[PX4IO_P_RC_CONFIG_CENTER] - conf[PX4IO_P_RC_CONFIG_DEADZONE])) {
scaled = 10000.0f * ((raw - conf[PX4IO_P_RC_CONFIG_CENTER] + conf[PX4IO_P_RC_CONFIG_DEADZONE]) / (float)(conf[PX4IO_P_RC_CONFIG_CENTER] - conf[PX4IO_P_RC_CONFIG_DEADZONE] - conf[PX4IO_P_RC_CONFIG_MIN]));
/* invert channel if pitch - pulling the lever down means pitching up by convention */
if (mapped == 1) /* roll, pitch, yaw, throttle, override is the standard order */
} else {
/* in the configured dead zone, output zero */
scaled = 0;
}
/* invert channel if requested */
if (conf[PX4IO_P_RC_CONFIG_OPTIONS] & PX4IO_P_RC_CONFIG_OPTIONS_REVERSE)
scaled = -scaled;
r_rc_values[mapped] = SIGNED_TO_REG(scaled);
assigned_channels |= (1 << mapped);
/* and update the scaled/mapped version */
unsigned mapped = conf[PX4IO_P_RC_CONFIG_ASSIGNMENT];
if (mapped < PX4IO_CONTROL_CHANNELS) {
/* invert channel if pitch - pulling the lever down means pitching up by convention */
if (mapped == 1) /* roll, pitch, yaw, throttle, override is the standard order */
scaled = -scaled;
r_rc_values[mapped] = SIGNED_TO_REG(scaled);
assigned_channels |= (1 << mapped);
}
}
}
}
/* set un-assigned controls to zero */
for (unsigned i = 0; i < PX4IO_CONTROL_CHANNELS; i++) {
if (!(assigned_channels & (1 << i)))
r_rc_values[i] = 0;
}
/* set un-assigned controls to zero */
for (unsigned i = 0; i < PX4IO_CONTROL_CHANNELS; i++) {
if (!(assigned_channels & (1 << i)))
r_rc_values[i] = 0;
}
/*
* If we got an update with zero channels, treat it as
* a loss of input.
*
* This might happen if a protocol-based receiver returns an update
* that contains no channels that we have mapped.
*/
if (assigned_channels == 0 || rssi == 0) {
rc_input_lost = true;
} else {
/* set RC OK flag */
/* set RC OK flag, as we got an update */
r_status_flags |= PX4IO_P_STATUS_FLAGS_RC_OK;
/* if we have enough channels (5) to control the vehicle, the mapping is ok */
if (assigned_channels > 4) {
r_raw_rc_flags |= PX4IO_P_RAW_RC_FLAGS_MAPPING_OK;
} else {
r_raw_rc_flags &= ~(PX4IO_P_RAW_RC_FLAGS_MAPPING_OK);
}
}
/*
@@ -264,7 +301,7 @@ controls_tick() {
* If we haven't seen any new control data in 200ms, assume we
* have lost input.
*/
if (hrt_elapsed_time(&system_state.rc_channels_timestamp) > 200000) {
if (hrt_elapsed_time(&system_state.rc_channels_timestamp_received) > 200000) {
rc_input_lost = true;
/* clear the input-kind flags here */
@@ -272,24 +309,32 @@ controls_tick() {
PX4IO_P_STATUS_FLAGS_RC_PPM |
PX4IO_P_STATUS_FLAGS_RC_DSM |
PX4IO_P_STATUS_FLAGS_RC_SBUS);
}
/*
* Handle losing RC input
*/
if (rc_input_lost) {
/* this kicks in if the receiver is gone or the system went to failsafe */
if (rc_input_lost || (r_raw_rc_flags & PX4IO_P_RAW_RC_FLAGS_FAILSAFE)) {
/* Clear the RC input status flag, clear manual override flag */
r_status_flags &= ~(
PX4IO_P_STATUS_FLAGS_OVERRIDE |
PX4IO_P_STATUS_FLAGS_RC_OK);
/* Mark all channels as invalid, as we just lost the RX */
r_rc_valid = 0;
/* Set the RC_LOST alarm */
r_status_alarms |= PX4IO_P_STATUS_ALARMS_RC_LOST;
}
/* Mark the arrays as empty */
/* this kicks in if the receiver is completely gone */
if (rc_input_lost) {
/* Set channel count to zero */
r_raw_rc_count = 0;
r_rc_valid = 0;
}
/*
+13 -2
View File
@@ -223,14 +223,25 @@ mixer_tick(void)
}
}
if ((should_arm || should_always_enable_pwm) && !mixer_servos_armed) {
/* set arming */
bool needs_to_arm = (should_arm || should_always_enable_pwm);
/* check any conditions that prevent arming */
if (r_setup_arming & PX4IO_P_SETUP_ARMING_LOCKDOWN) {
needs_to_arm = false;
}
if (!should_arm && !should_always_enable_pwm) {
needs_to_arm = false;
}
if (needs_to_arm && !mixer_servos_armed) {
/* need to arm, but not armed */
up_pwm_servo_arm(true);
mixer_servos_armed = true;
r_status_flags |= PX4IO_P_STATUS_FLAGS_OUTPUTS_ARMED;
isr_debug(5, "> PWM enabled");
} else if ((!should_arm && !should_always_enable_pwm) && mixer_servos_armed) {
} else if (!needs_to_arm && mixer_servos_armed) {
/* armed but need to disarm */
up_pwm_servo_arm(false);
mixer_servos_armed = false;
+16 -4
View File
@@ -111,7 +111,6 @@
#define PX4IO_P_STATUS_FLAGS_INIT_OK (1 << 10) /* initialisation of the IO completed without error */
#define PX4IO_P_STATUS_FLAGS_FAILSAFE (1 << 11) /* failsafe is active */
#define PX4IO_P_STATUS_FLAGS_SAFETY_OFF (1 << 12) /* safety is off */
#define PX4IO_P_STATUS_FLAGS_RC_DSM11 (1 << 13) /* DSM input is 11 bit data */
#define PX4IO_P_STATUS_ALARMS 3 /* alarm flags - alarms latch, write 1 to a bit to clear it */
#define PX4IO_P_STATUS_ALARMS_VBATT_LOW (1 << 0) /* [1] VBatt is very close to regulator dropout */
@@ -128,8 +127,6 @@
#define PX4IO_P_STATUS_VSERVO 6 /* [2] servo rail voltage in mV */
#define PX4IO_P_STATUS_VRSSI 7 /* [2] RSSI voltage */
#define PX4IO_P_STATUS_PRSSI 8 /* [2] RSSI PWM value */
#define PX4IO_P_STATUS_NRSSI 9 /* [2] Normalized RSSI value, 0: no reception, 255: perfect reception */
#define PX4IO_P_STATUS_RC_DATA 10 /* [1] + [2] Details about the RC source (PPM frame length, Spektrum protocol type) */
/* array of post-mix actuator outputs, -10000..10000 */
#define PX4IO_PAGE_ACTUATORS 2 /* 0..CONFIG_ACTUATOR_COUNT-1 */
@@ -140,7 +137,17 @@
/* array of raw RC input values, microseconds */
#define PX4IO_PAGE_RAW_RC_INPUT 4
#define PX4IO_P_RAW_RC_COUNT 0 /* number of valid channels */
#define PX4IO_P_RAW_RC_BASE 1 /* CONFIG_RC_INPUT_COUNT channels from here */
#define PX4IO_P_RAW_RC_FLAGS 1 /* RC detail status flags */
#define PX4IO_P_RAW_RC_FLAGS_FRAME_DROP (1 << 0) /* single frame drop */
#define PX4IO_P_RAW_RC_FLAGS_FAILSAFE (1 << 1) /* receiver is in failsafe mode */
#define PX4IO_P_RAW_RC_FLAGS_RC_DSM11 (1 << 2) /* DSM decoding is 11 bit mode */
#define PX4IO_P_RAW_RC_FLAGS_MAPPING_OK (1 << 3) /* Channel mapping is ok */
#define PX4IO_P_RAW_RC_NRSSI 2 /* [2] Normalized RSSI value, 0: no reception, 255: perfect reception */
#define PX4IO_P_RAW_RC_DATA 3 /* [1] + [2] Details about the RC source (PPM frame length, Spektrum protocol type) */
#define PX4IO_P_RAW_FRAME_COUNT 4 /* Number of total received frames (wrapping counter) */
#define PX4IO_P_RAW_LOST_FRAME_COUNT 5 /* Number of total dropped frames (wrapping counter) */
#define PX4IO_P_RAW_RC_BASE 6 /* CONFIG_RC_INPUT_COUNT channels from here */
/* array of scaled RC input values, -10000..10000 */
#define PX4IO_PAGE_RC_INPUT 5
@@ -157,6 +164,10 @@
/* setup page */
#define PX4IO_PAGE_SETUP 50
#define PX4IO_P_SETUP_FEATURES 0
#define PX4IO_P_SETUP_FEATURES_SBUS1_OUT (1 << 0) /* enable S.Bus v1 output */
#define PX4IO_P_SETUP_FEATURES_SBUS2_OUT (1 << 1) /* enable S.Bus v2 output */
#define PX4IO_P_SETUP_FEATURES_PWM_RSSI (1 << 2) /* enable PWM RSSI parsing */
#define PX4IO_P_SETUP_FEATURES_ADC_RSSI (1 << 3) /* enable ADC RSSI parsing */
#define PX4IO_P_SETUP_ARMING 1 /* arming controls */
#define PX4IO_P_SETUP_ARMING_IO_ARM_OK (1 << 0) /* OK to arm the IO side */
@@ -166,6 +177,7 @@
#define PX4IO_P_SETUP_ARMING_INAIR_RESTART_OK (1 << 4) /* OK to try in-air restart */
#define PX4IO_P_SETUP_ARMING_ALWAYS_PWM_ENABLE (1 << 5) /* Output of PWM right after startup enabled to help ESCs initialize and prevent them from beeping */
#define PX4IO_P_SETUP_ARMING_RC_HANDLING_DISABLED (1 << 6) /* Disable the IO-internal evaluation of the RC */
#define PX4IO_P_SETUP_ARMING_LOCKDOWN (1 << 7) /* If set, the system operates normally, but won't actuate any servos */
#define PX4IO_P_SETUP_PWM_RATES 2 /* bitmask, 0 = low rate, 1 = high rate */
#define PX4IO_P_SETUP_PWM_DEFAULTRATE 3 /* 'low' PWM frame output rate in Hz */
+6 -4
View File
@@ -1,6 +1,6 @@
/****************************************************************************
*
* Copyright (C) 2012 PX4 Development Team. All rights reserved.
* Copyright (c) 2012-2014 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
@@ -96,8 +96,9 @@ extern uint16_t r_page_servo_disarmed[]; /* PX4IO_PAGE_DISARMED_PWM */
#define r_raw_rc_count r_page_raw_rc_input[PX4IO_P_RAW_RC_COUNT]
#define r_raw_rc_values (&r_page_raw_rc_input[PX4IO_P_RAW_RC_BASE])
#define r_raw_rc_flags r_page_raw_rc_input[PX4IO_P_RAW_RC_FLAGS]
#define r_rc_valid r_page_rc_input[PX4IO_P_RC_VALID]
#define r_rc_values (&r_page_rc_input[PX4IO_P_RAW_RC_BASE])
#define r_rc_values (&r_page_rc_input[PX4IO_P_RC_BASE])
#define r_setup_features r_page_setup[PX4IO_P_SETUP_FEATURES]
#define r_setup_arming r_page_setup[PX4IO_P_SETUP_ARMING]
@@ -115,7 +116,8 @@ extern uint16_t r_page_servo_disarmed[]; /* PX4IO_PAGE_DISARMED_PWM */
*/
struct sys_state_s {
volatile uint64_t rc_channels_timestamp;
volatile uint64_t rc_channels_timestamp_received;
volatile uint64_t rc_channels_timestamp_valid;
/**
* Last FMU receive time, in microseconds since system boot
@@ -215,7 +217,7 @@ extern int dsm_init(const char *device);
extern bool dsm_input(uint16_t *values, uint16_t *num_values);
extern void dsm_bind(uint16_t cmd, int pulses);
extern int sbus_init(const char *device);
extern bool sbus_input(uint16_t *values, uint16_t *num_values, uint16_t *rssi, uint16_t max_channels);
extern bool sbus_input(uint16_t *values, uint16_t *num_values, bool *sbus_failsafe, bool *sbus_frame_drop, uint16_t max_channels);
/** global debug level for isr_debug() */
extern volatile uint8_t debug_level;
+49 -11
View File
@@ -90,8 +90,6 @@ uint16_t r_page_status[] = {
[PX4IO_P_STATUS_VSERVO] = 0,
[PX4IO_P_STATUS_VRSSI] = 0,
[PX4IO_P_STATUS_PRSSI] = 0,
[PX4IO_P_STATUS_NRSSI] = 0,
[PX4IO_P_STATUS_RC_DATA] = 0
};
/**
@@ -116,6 +114,12 @@ uint16_t r_page_servos[PX4IO_SERVO_COUNT];
uint16_t r_page_raw_rc_input[] =
{
[PX4IO_P_RAW_RC_COUNT] = 0,
[PX4IO_P_RAW_RC_FLAGS] = 0,
[PX4IO_P_RAW_RC_NRSSI] = 0,
[PX4IO_P_RAW_RC_DATA] = 0,
[PX4IO_P_RAW_FRAME_COUNT] = 0,
[PX4IO_P_RAW_LOST_FRAME_COUNT] = 0,
[PX4IO_P_RAW_RC_DATA] = 0,
[PX4IO_P_RAW_RC_BASE ... (PX4IO_P_RAW_RC_BASE + PX4IO_RC_INPUT_CHANNELS)] = 0
};
@@ -144,7 +148,12 @@ uint16_t r_page_scratch[32];
*/
volatile uint16_t r_page_setup[] =
{
#ifdef CONFIG_ARCH_BOARD_PX4IO_V2
/* default to RSSI ADC functionality */
[PX4IO_P_SETUP_FEATURES] = PX4IO_P_SETUP_FEATURES_ADC_RSSI,
#else
[PX4IO_P_SETUP_FEATURES] = 0,
#endif
[PX4IO_P_SETUP_ARMING] = 0,
[PX4IO_P_SETUP_PWM_RATES] = 0,
[PX4IO_P_SETUP_PWM_DEFAULTRATE] = 50,
@@ -162,14 +171,22 @@ volatile uint16_t r_page_setup[] =
[PX4IO_P_SETUP_CRC ... (PX4IO_P_SETUP_CRC+1)] = 0,
};
#define PX4IO_P_SETUP_FEATURES_VALID (0)
#ifdef CONFIG_ARCH_BOARD_PX4IO_V2
#define PX4IO_P_SETUP_FEATURES_VALID (PX4IO_P_SETUP_FEATURES_SBUS1_OUT | \
PX4IO_P_SETUP_FEATURES_SBUS2_OUT | \
PX4IO_P_SETUP_FEATURES_ADC_RSSI | \
PX4IO_P_SETUP_FEATURES_PWM_RSSI)
#else
#define PX4IO_P_SETUP_FEATURES_VALID 0
#endif
#define PX4IO_P_SETUP_ARMING_VALID (PX4IO_P_SETUP_ARMING_FMU_ARMED | \
PX4IO_P_SETUP_ARMING_MANUAL_OVERRIDE_OK | \
PX4IO_P_SETUP_ARMING_INAIR_RESTART_OK | \
PX4IO_P_SETUP_ARMING_IO_ARM_OK | \
PX4IO_P_SETUP_ARMING_FAILSAFE_CUSTOM | \
PX4IO_P_SETUP_ARMING_ALWAYS_PWM_ENABLE | \
PX4IO_P_SETUP_ARMING_RC_HANDLING_DISABLED)
PX4IO_P_SETUP_ARMING_RC_HANDLING_DISABLED | \
PX4IO_P_SETUP_ARMING_LOCKDOWN)
#define PX4IO_P_SETUP_RATES_VALID ((1 << PX4IO_SERVO_COUNT) - 1)
#define PX4IO_P_SETUP_RELAYS_VALID ((1 << PX4IO_RELAY_CHANNELS) - 1)
@@ -438,9 +455,35 @@ registers_set_one(uint8_t page, uint8_t offset, uint16_t value)
case PX4IO_P_SETUP_FEATURES:
value &= PX4IO_P_SETUP_FEATURES_VALID;
r_setup_features = value;
/* no implemented feature selection at this point */
/* some of the options conflict - give S.BUS out precedence, then ADC RSSI, then PWM RSSI */
/* switch S.Bus output pin as needed */
#ifdef ENABLE_SBUS_OUT
ENABLE_SBUS_OUT(value & (PX4IO_P_SETUP_FEATURES_SBUS1_OUT | PX4IO_P_SETUP_FEATURES_SBUS2_OUT));
/* disable the conflicting options */
if (value & (PX4IO_P_SETUP_FEATURES_SBUS1_OUT | PX4IO_P_SETUP_FEATURES_SBUS2_OUT)) {
value &= ~(PX4IO_P_SETUP_FEATURES_PWM_RSSI | PX4IO_P_SETUP_FEATURES_ADC_RSSI);
}
#endif
/* disable the conflicting options with ADC RSSI */
if (value & (PX4IO_P_SETUP_FEATURES_ADC_RSSI)) {
value &= ~(PX4IO_P_SETUP_FEATURES_PWM_RSSI |
PX4IO_P_SETUP_FEATURES_SBUS1_OUT |
PX4IO_P_SETUP_FEATURES_SBUS2_OUT);
}
/* disable the conflicting options with PWM RSSI (without effect here, but for completeness) */
if (value & (PX4IO_P_SETUP_FEATURES_PWM_RSSI)) {
value &= ~(PX4IO_P_SETUP_FEATURES_ADC_RSSI |
PX4IO_P_SETUP_FEATURES_SBUS1_OUT |
PX4IO_P_SETUP_FEATURES_SBUS2_OUT);
}
/* apply changes */
r_setup_features = value;
break;
@@ -456,11 +499,6 @@ registers_set_one(uint8_t page, uint8_t offset, uint16_t value)
* lockup of the IO arming state.
*/
// XXX do not reset IO's safety state by FMU for now
// if ((r_setup_arming & PX4IO_P_SETUP_ARMING_FMU_ARMED) && !(value & PX4IO_P_SETUP_ARMING_FMU_ARMED)) {
// r_status_flags &= ~PX4IO_P_STATUS_FLAGS_ARMED;
// }
if (value & PX4IO_P_SETUP_ARMING_RC_HANDLING_DISABLED) {
r_status_flags |= PX4IO_P_STATUS_FLAGS_INIT_OK;
}
+12 -10
View File
@@ -87,7 +87,7 @@ static unsigned partial_frame_count;
unsigned sbus_frame_drops;
static bool sbus_decode(hrt_abstime frame_time, uint16_t *values, uint16_t *num_values, uint16_t *rssi, uint16_t max_channels);
static bool sbus_decode(hrt_abstime frame_time, uint16_t *values, uint16_t *num_values, bool *sbus_failsafe, bool *sbus_frame_drop, uint16_t max_channels);
int
sbus_init(const char *device)
@@ -118,7 +118,7 @@ sbus_init(const char *device)
}
bool
sbus_input(uint16_t *values, uint16_t *num_values, uint16_t *rssi, uint16_t max_channels)
sbus_input(uint16_t *values, uint16_t *num_values, bool *sbus_failsafe, bool *sbus_frame_drop, uint16_t max_channels)
{
ssize_t ret;
hrt_abstime now;
@@ -175,7 +175,7 @@ sbus_input(uint16_t *values, uint16_t *num_values, uint16_t *rssi, uint16_t max_
* decode it.
*/
partial_frame_count = 0;
return sbus_decode(now, values, num_values, rssi, max_channels);
return sbus_decode(now, values, num_values, sbus_failsafe, sbus_frame_drop, max_channels);
}
/*
@@ -215,7 +215,7 @@ static const struct sbus_bit_pick sbus_decoder[SBUS_INPUT_CHANNELS][3] = {
};
static bool
sbus_decode(hrt_abstime frame_time, uint16_t *values, uint16_t *num_values, uint16_t *rssi, uint16_t max_values)
sbus_decode(hrt_abstime frame_time, uint16_t *values, uint16_t *num_values, bool *sbus_failsafe, bool *sbus_frame_drop, uint16_t max_values)
{
/* check frame boundary markers to avoid out-of-sync cases */
if ((frame[0] != 0x0f)) {
@@ -289,20 +289,22 @@ sbus_decode(hrt_abstime frame_time, uint16_t *values, uint16_t *num_values, uint
/* decode and handle failsafe and frame-lost flags */
if (frame[SBUS_FLAGS_BYTE] & (1 << SBUS_FAILSAFE_BIT)) { /* failsafe */
/* report that we failed to read anything valid off the receiver */
*rssi = 0;
return false;
*sbus_failsafe = true;
*sbus_frame_drop = true;
}
else if (frame[SBUS_FLAGS_BYTE] & (1 << SBUS_FRAMELOST_BIT)) { /* a frame was lost */
/* set a special warning flag or try to calculate some kind of RSSI information - to be implemented
/* set a special warning flag
*
* Attention! This flag indicates a skipped frame only, not a total link loss! Handling this
* condition as fail-safe greatly reduces the reliability and range of the radio link,
* e.g. by prematurely issueing return-to-launch!!! */
*rssi = 100; // XXX magic number indicating bad signal, but not a signal loss (yet)
*sbus_failsafe = false;
*sbus_frame_drop = true;
} else {
*sbus_failsafe = false;
*sbus_frame_drop = false;
}
*rssi = 255;
return true;
}
+6 -3
View File
@@ -1270,6 +1270,9 @@ Sensors::rc_poll()
orb_copy(ORB_ID(input_rc), _rc_sub, &rc_input);
if (rc_input.rc_lost)
return;
struct manual_control_setpoint_s manual_control;
struct actuator_controls_s actuator_group_3;
@@ -1314,7 +1317,7 @@ Sensors::rc_poll()
channel_limit = _rc_max_chan_count;
/* we are accepting this message */
_rc_last_valid = rc_input.timestamp;
_rc_last_valid = rc_input.timestamp_last_signal;
/* Read out values from raw message */
for (unsigned int i = 0; i < channel_limit; i++) {
@@ -1363,9 +1366,9 @@ Sensors::rc_poll()
}
_rc.chan_count = rc_input.channel_count;
_rc.timestamp = rc_input.timestamp;
_rc.timestamp = rc_input.timestamp_last_signal;
manual_control.timestamp = rc_input.timestamp;
manual_control.timestamp = rc_input.timestamp_last_signal;
/* roll input - rolling right is stick-wise and rotation-wise positive */
manual_control.roll = limit_minus_one_to_one(_rc.chan[_rc.function[ROLL]].scaled);
+1 -2
View File
@@ -93,8 +93,7 @@ void cpuload_initialize_once()
#endif /* CONFIG_SCHED_WORKQUEUE */
// perform static initialization of "system" threads
for (system_load.total_count = 0; system_load.total_count < static_tasks_count; system_load.total_count++)
{
for (system_load.total_count = 0; system_load.total_count < static_tasks_count; system_load.total_count++) {
system_load.tasks[system_load.total_count].start_time = now;
system_load.tasks[system_load.total_count].total_runtime = 0;
system_load.tasks[system_load.total_count].curr_start_time = 0;
+6 -6
View File
@@ -40,15 +40,15 @@ __BEGIN_DECLS
#include <nuttx/sched.h>
struct system_load_taskinfo_s {
uint64_t total_runtime; ///< Runtime since start (start_time - total_runtime)/(start_time - current_time) = load
uint64_t curr_start_time; ///< Start time of the current scheduling slot
uint64_t start_time; ///< FIRST start time of task
FAR struct tcb_s *tcb; ///<
bool valid; ///< Task is currently active / valid
uint64_t total_runtime; ///< Runtime since start (start_time - total_runtime)/(start_time - current_time) = load
uint64_t curr_start_time; ///< Start time of the current scheduling slot
uint64_t start_time; ///< FIRST start time of task
FAR struct tcb_s *tcb; ///<
bool valid; ///< Task is currently active / valid
};
struct system_load_s {
uint64_t start_time; ///< Global start time of measurements
uint64_t start_time; ///< Global start time of measurements
struct system_load_taskinfo_s tasks[CONFIG_MAX_TASKS];
uint8_t initialized;
int total_count;
+1 -1
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@@ -320,7 +320,7 @@ do_set(const char* name, const char* val)
char* end;
f = strtod(val,&end);
param_set(param, &f);
printf(" -> new: %f\n", f);
printf(" -> new: %4.4f\n", (double)f);
}
+11 -11
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@@ -65,20 +65,20 @@ static int mixer_callback(uintptr_t handle,
const unsigned output_max = 8;
static float actuator_controls[output_max];
static bool should_arm = false;
uint16_t r_page_servo_disarmed[output_max];
uint16_t r_page_servo_control_min[output_max];
uint16_t r_page_servo_control_max[output_max];
uint16_t r_page_servos[output_max];
uint16_t servo_predicted[output_max];
/*
* PWM limit structure
*/
pwm_limit_t pwm_limit;
int test_mixer(int argc, char *argv[])
{
/*
* PWM limit structure
*/
pwm_limit_t pwm_limit;
static bool should_arm = false;
uint16_t r_page_servo_disarmed[output_max];
uint16_t r_page_servo_control_min[output_max];
uint16_t r_page_servo_control_max[output_max];
uint16_t r_page_servos[output_max];
uint16_t servo_predicted[output_max];
warnx("testing mixer");
char *filename = "/etc/mixers/IO_pass.mix";
+1 -1
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@@ -121,7 +121,7 @@ int test_rc(int argc, char *argv[])
return ERROR;
}
if (hrt_absolute_time() - rc_input.timestamp > 100000) {
if (hrt_absolute_time() - rc_input.timestamp_last_signal > 100000) {
warnx("TIMEOUT, less than 10 Hz updates");
(void)close(_rc_sub);
return ERROR;