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27 Commits

Author SHA1 Message Date
Eric Katzfey fbfb93ab26 Cleaned up the API and added SBUS support 2023-12-28 17:33:18 -08:00
Eric Katzfey 4b53be9444 Updated GPS driver to use the new platform independent UART driver 2023-12-27 15:39:33 -08:00
Eric Katzfey 4217b43728 Fixed various build issues with the new Serial implementation 2023-12-27 14:54:36 -08:00
Eric Katzfey baa857d56f Added a new device driver for a platform independent UART implementation 2023-12-27 13:08:26 -08:00
Silvan Fuhrer 6be8cbe439 Navigator: mission_block: reduce enforce eexit course margin to 105% (#22511)
With this margin it is made sure that if the loiter is not perfectly tracked,
(vehicle outside of path setpoint) a wp just at the border of the loiter
is still reachable.
It should though be as small as necessary, as otherwise, with good
loiter tracking,  waypoints that are close but not right on the loiter
radius are not enforcing the exit course neither.

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2023-12-21 16:58:22 +01:00
Silvan Fuhrer 7e22b47b85 Navigator/FlightTaskAuto yaw handling improvements/simplifications (#22532)
* PositionSetpoint: remove yaw_valid field

* Navigator: set yaw setpoint to NAN for Takeoff

Don't set a yaw setpoint for takeoff, as Navigator doesn't handle the yaw reset.
The yaw setpoint generation is handled by FlightTaskAuto.

* PositionSetpoint.msg: remove disable_weather_vane and instead only use the yaw field

Strictly follow the concept that if the position_setpoint.yaw is set, then
follow it the controller, and otherwise let the controller set it as it
thinks it's best.

* Navigator: remove logic that sets yaw to be accepted in TAKEOFF

No longer needed as during Takeoff we anyway don't set a yaw setpoint.

* PositionSetpoint.msg: remove yawspeed_valid

* PositionSetpoint.msg: remove yawspeed

* Navigator: set yaw setpoint to NAN instead of current

In set_takeoff and set_land_item, as well as for VTOL transition.
The flight tasks then set the yaw corresponding to the current yaw.

* Navigator: change get_yaw_acceptance into a bool

* PositionSetpoint.msg: improve comment for yaw

* MissionBlock: remove unnecessary code from set_vtol_transition_item

* Navigator: clean up calculate_breaking_stop(), set yaw to NAN

* Navigator: set yaw to NAN in variouls places where not specifc setpoint is desired

* Navigator: set yaw to NAN in reset_position_setpoint()

---------

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
Co-authored-by: Matthias Grob <maetugr@gmail.com>
2023-12-21 16:50:13 +01:00
Matthias Grob d872ef87da differential_drive_control: don't build by default
also add dependency on control allocation parameter CA_R_REV
2023-12-21 16:27:53 +01:00
Matthias Grob 3de5c609a4 Differential Rover: PR fixes 2023-12-21 16:27:53 +01:00
PerFrivik 056e41af8c Differential Rover: Ported R1 to GZ and introduced new GZ wheel interface 2023-12-21 16:27:53 +01:00
PerFrivik 1e7ce32480 Differential Rover: Added logging and dds topics 2023-12-21 16:27:53 +01:00
PerFrivik 3df71d1837 Differential Rover: Differential drive module & library 2023-12-21 16:27:53 +01:00
PerFrivik e3359ea884 Differential Rover: Update airframe architecture 2023-12-21 16:27:53 +01:00
Peter van der Perk 19d1941758 px4_fmuv6xrt: Switch to icm42686p on SPI1
icm42588p driver don't use a icm42688p when icm42686p is requested
2023-12-21 10:11:20 -05:00
bresch c1b139dea1 atune: reset param on start
This prevents a race condition where autotune cannot start because the param was already set to 1
2023-12-21 13:52:47 +01:00
MaEtUgR 74549e29a5 [AUTO COMMIT] update change indication 2023-12-21 11:42:08 +01:00
Matthias Grob bcb2b1ad40 matrix: fix slice to slice assignment to do deep copy
To fix usage of a.xy() = b.xy() which should copy
the first two elements over into a and not act on a copy of a.
2023-12-21 11:42:08 +01:00
Silvan Fuhrer 2afbd09c63 Commander: AirspeedCheck: increase timeout threshold to 2s
1s gives some false positives at boot up, as the airspeed selector only
starts publishing 2s after its startup.

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2023-12-21 11:34:28 +01:00
Silvan Fuhrer 9d00a3ae4d AirspeedSelector: remove option to disable airspeed sensor through ASPD_PRIMARY
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2023-12-21 11:34:28 +01:00
Silvan Fuhrer 29807a5e50 Replace CBRK_AIRSPD_CHK with SYS_HAS_NUM_ASPD
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2023-12-21 11:34:28 +01:00
Silvan Fuhrer 9e0c8fd75e FW controllers: change param FW_ARSP_MODE to FW_USE_AIRSPD
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2023-12-21 11:34:28 +01:00
Silvan Fuhrer 1f2a0bc657 Commander: remove check for FW_ARSP_MODE for airspeed missing reporting
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2023-12-21 11:34:28 +01:00
Silvan Fuhrer 5211c358aa FW Position Controller: change airspeed setpoint init
-remove dedicated vtol transition airspeed init logic
-init airspeed setpoint on first usage of tecs
-init to max of current airspeed and min airspeed

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2023-12-21 11:34:28 +01:00
Silvan Fuhrer 27957e1f2f FW Position Controller: set airspeed_valid flag to false if incoming data is not finite
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2023-12-21 11:34:28 +01:00
Silvan Fuhrer 123c06f2e6 NPFG: specify in comments that airspeed reference is for true airspeed
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2023-12-21 11:34:28 +01:00
Silvan Fuhrer 589f0f1fc7 FW Position Controller: rename _airspeed to _airspeed_eas
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2023-12-21 11:34:28 +01:00
bresch b8c81f6281 gps_blending: fallback to secondary if primary has no fix 2023-12-20 16:35:30 -05:00
bresch 094048ed04 gps_blending: fix selection rapid switching
Once a timeout of the primary instance is detected, a fallback is only
allowed until the primary receiver is regained.
2023-12-20 16:35:30 -05:00
121 changed files with 2009 additions and 725 deletions
@@ -66,7 +66,6 @@ param set-default SIM_GZ_SV_FUNC2 202
param set-default SIM_GZ_SV_FUNC3 203
param set-default COM_RC_IN_MODE 1
param set-default ASPD_PRIMARY 1
param set-default CA_SV_CS_COUNT 3
param set-default CA_SV_CS0_TYPE 1
-1
View File
@@ -153,7 +153,6 @@ fi
param set-default BAT1_N_CELLS 4
param set-default CBRK_AIRSPD_CHK 0
param set-default CBRK_SUPPLY_CHK 894281
# disable check, no CPU load reported on posix yet
@@ -28,13 +28,13 @@ param set-default BAT1_CAPACITY 23000
param set-default BAT1_N_CELLS 4
param set-default BAT1_R_INTERNAL 0.0025
param set-default CBRK_AIRSPD_CHK 162128
param set-default SYS_HAS_NUM_ASPD 0
param set-default CBRK_IO_SAFETY 22027
param set-default EKF2_GPS_POS_X -0.12
param set-default EKF2_IMU_POS_X -0.12
param set-default FW_ARSP_MODE 1
param set-default FW_USE_AIRSPD 0
param set-default NPFG_PERIOD 25
param set-default FW_PR_FF 0.7
param set-default FW_PR_I 0.18
@@ -54,3 +54,5 @@ param set-default MIS_TKO_LAND_REQ 2
# FW takeoff acceleration can easily exceed ublox GPS 2G default.
#
param set-default GPS_UBX_DYNMODEL 8
param set-default SYS_HAS_NUM_ASPD 1 # by default require an airspeed sensor
@@ -10,9 +10,6 @@ set VEHICLE_TYPE rover
# MAV_TYPE_GROUND_ROVER 10
param set-default MAV_TYPE 10
# Enable Airspeed check circuit breaker because Rovers will have no airspeed sensor
param set-default CBRK_AIRSPD_CHK 162128
param set-default MIS_TAKEOFF_ALT 0.01
param set-default NAV_ACC_RAD 2
@@ -5,7 +5,7 @@
ekf2 start &
# Start rover differential drive controller.
rover_control start
differential_drive_control start
# Start Land Detector.
land_detector start rover
@@ -9,6 +9,3 @@ set VEHICLE_TYPE uuv
# MAV_TYPE_SUBMARINE 12
param set-default MAV_TYPE 12
# UUV don't have an airspeed sensor, so disable checks around it
param set-default CBRK_AIRSPD_CHK 162128
@@ -42,4 +42,6 @@ param set-default MPC_MAN_Y_MAX 90
param set-default RTL_TYPE 1
param set-default SYS_HAS_NUM_ASPD 1 # by default require an airspeed sensor
param set-default WV_EN 1
-20
View File
@@ -1,20 +0,0 @@
{
"configurations": [
{
"browse": {
"databaseFilename": "${default}",
"limitSymbolsToIncludedHeaders": false
},
"includePath": [
"/opt/ros/humble/include/**",
"/usr/include/**"
],
"name": "ROS",
"intelliSenseMode": "gcc-x64",
"compilerPath": "/usr/bin/gcc",
"cStandard": "gnu11",
"cppStandard": "c++14"
}
],
"version": 4
}
-10
View File
@@ -1,10 +0,0 @@
{
"python.autoComplete.extraPaths": [
"/opt/ros/humble/lib/python3.10/site-packages",
"/opt/ros/humble/local/lib/python3.10/dist-packages"
],
"python.analysis.extraPaths": [
"/opt/ros/humble/lib/python3.10/site-packages",
"/opt/ros/humble/local/lib/python3.10/dist-packages"
]
}
@@ -39,7 +39,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
-1
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@@ -39,7 +39,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
-1
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@@ -36,7 +36,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
-1
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@@ -25,7 +25,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
-1
View File
@@ -43,7 +43,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
-1
View File
@@ -44,7 +44,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
@@ -39,7 +39,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
-1
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@@ -27,7 +27,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
@@ -37,7 +37,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
-1
View File
@@ -32,7 +32,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
# CONFIG_EKF2_AUXVEL is not set
# CONFIG_EKF2_BARO_COMPENSATION is not set
@@ -31,7 +31,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
# CONFIG_EKF2_AUXVEL is not set
# CONFIG_EKF2_BARO_COMPENSATION is not set
@@ -32,7 +32,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
# CONFIG_EKF2_AUXVEL is not set
# CONFIG_EKF2_BARO_COMPENSATION is not set
-1
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@@ -43,7 +43,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
-1
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@@ -41,7 +41,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
+1
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@@ -3,6 +3,7 @@ CONFIG_BOARD_LINUX_TARGET=y
CONFIG_BOARD_TOOLCHAIN="aarch64-linux-gnu"
CONFIG_BOARD_ROOTFSDIR="/data/px4"
CONFIG_DRIVERS_ACTUATORS_MODAL_IO=y
CONFIG_DRIVERS_GPS=y
CONFIG_DRIVERS_OSD_MSP_OSD=y
CONFIG_DRIVERS_QSHELL_POSIX=y
CONFIG_MODULES_COMMANDER=y
@@ -36,7 +36,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
@@ -37,7 +37,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
-1
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@@ -37,7 +37,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
@@ -35,7 +35,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
-1
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@@ -36,7 +36,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
-1
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@@ -35,7 +35,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
-1
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@@ -38,7 +38,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
-1
View File
@@ -39,7 +39,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
-1
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@@ -40,7 +40,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
-1
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@@ -41,7 +41,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
-1
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@@ -28,7 +28,6 @@ CONFIG_MODULES_ATTITUDE_ESTIMATOR_Q=y
CONFIG_MODULES_BATTERY_STATUS=y
CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
-1
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@@ -15,7 +15,6 @@ CONFIG_MODULES_AIRSPEED_SELECTOR=y
CONFIG_MODULES_ATTITUDE_ESTIMATOR_Q=y
CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
-1
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@@ -20,7 +20,6 @@ CONFIG_MODULES_ATTITUDE_ESTIMATOR_Q=y
CONFIG_MODULES_BATTERY_STATUS=y
CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
CONFIG_MODULES_FW_ATT_CONTROL=y
-1
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@@ -1,4 +1,3 @@
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_FLIGHT_MODE_MANAGER=n
CONFIG_MODULES_MC_ATT_CONTROL=n
CONFIG_MODULES_MC_POS_CONTROL=n
-1
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@@ -43,7 +43,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
-1
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@@ -44,7 +44,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
-1
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@@ -40,7 +40,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
-1
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@@ -48,7 +48,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
+1 -1
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@@ -53,7 +53,7 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_DIFFERENTIAL_DRIVE_CONTROL=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
-1
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@@ -37,7 +37,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
-1
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@@ -40,7 +40,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
-1
View File
@@ -37,7 +37,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_EVENTS=y
CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
+2 -2
View File
@@ -61,8 +61,8 @@ then
fi
fi
# Internal SPI bus ICM42688p (hard-mounted)
icm42688p -R 12 -b 1 -s start
# Internal SPI bus ICM42686p (hard-mounted)
icm42688p -6 -R 12 -b 1 -s start
# Internal on IMU SPI BMI088
bmi088 -A -R 4 -s start
+1 -1
View File
@@ -65,7 +65,7 @@
constexpr px4_spi_bus_t px4_spi_buses[SPI_BUS_MAX_BUS_ITEMS] = {
initSPIBus(SPI::Bus::LPSPI1, {
initSPIDevice(DRV_IMU_DEVTYPE_ICM42688P, SPI::CS{GPIO::Port2, GPIO::Pin11}, SPI::DRDY{GPIO::Port3, GPIO::Pin19}), /* GPIO_EMC_B2_01 GPIO2_IO11, GPIO_AD_20, GPIO3_IO19 */
initSPIDevice(DRV_IMU_DEVTYPE_ICM42686P, SPI::CS{GPIO::Port2, GPIO::Pin11}, SPI::DRDY{GPIO::Port3, GPIO::Pin19}), /* GPIO_EMC_B2_01 GPIO2_IO11, GPIO_AD_20, GPIO3_IO19 */
}, {GPIO::Port2, GPIO::Pin1}), // Power GPIO_EMC_B1_33 GPIO2_IO01
initSPIBus(SPI::Bus::LPSPI2, {
-1
View File
@@ -24,7 +24,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
+1 -1
View File
@@ -12,7 +12,7 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_DIFFERENTIAL_DRIVE_CONTROL=y
CONFIG_MODULES_EKF2=y
CONFIG_EKF2_AUX_GLOBAL_POSITION=y
CONFIG_MODULES_EVENTS=y
-1
View File
@@ -27,7 +27,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_EVENTS=y
CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
-1
View File
@@ -31,7 +31,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
-1
View File
@@ -37,7 +37,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
-1
View File
@@ -37,7 +37,6 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_ROVER_CONTROL=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
+1 -7
View File
@@ -22,11 +22,7 @@ float32 vz # local velocity setpoint in m/s in NED
float64 lat # latitude, in deg
float64 lon # longitude, in deg
float32 alt # altitude AMSL, in m
float32 yaw # yaw (only for multirotors), in rad [-PI..PI), NaN = hold current yaw
bool yaw_valid # true if yaw setpoint valid
float32 yawspeed # yawspeed (only for multirotors, in rad/s)
bool yawspeed_valid # true if yawspeed setpoint valid
float32 yaw # yaw (only in hover), in rad [-PI..PI), NaN = leave to flight task
float32 loiter_radius # loiter major axis radius in m
float32 loiter_minor_radius # loiter minor axis radius (used for non-circular loiter shapes) in m
@@ -39,5 +35,3 @@ float32 acceptance_radius # navigation acceptance_radius if we're doing waypoi
float32 cruising_speed # the generally desired cruising speed (not a hard constraint)
bool gliding_enabled # commands the vehicle to glide if the capability is available (fixed wing only)
float32 cruising_throttle # the generally desired cruising throttle (not a hard constraint), only has an effect for rover
bool disable_weather_vane # VTOL: disable (in auto mode) the weather vane feature that turns the nose into the wind
+1
View File
@@ -56,4 +56,5 @@ px4_add_module(
module.yaml
DEPENDS
git_gps_devices
drivers__device
)
+154 -175
View File
@@ -45,11 +45,11 @@
#include <poll.h>
#endif
#include <termios.h>
#include <cstring>
#include <drivers/drv_sensor.h>
#include <lib/drivers/device/Device.hpp>
#include <lib/drivers/device/Serial.hpp>
#include <lib/parameters/param.h>
#include <mathlib/mathlib.h>
#include <matrix/math.hpp>
@@ -81,6 +81,7 @@
#include <linux/spi/spidev.h>
#endif /* __PX4_LINUX */
using namespace device;
using namespace time_literals;
#define TIMEOUT_1HZ 1300 //!< Timeout time in mS, 1000 mS (1Hz) + 300 mS delta for error
@@ -169,7 +170,10 @@ public:
void reset_if_scheduled();
private:
int _serial_fd{-1}; ///< serial interface to GPS
#ifdef __PX4_LINUX
int _spi_fd {-1}; ///< SPI interface to GPS
#endif
Serial *_uart = nullptr;
unsigned _baudrate{0}; ///< current baudrate
const unsigned _configured_baudrate{0}; ///< configured baudrate (0=auto-detect)
char _port[20] {}; ///< device / serial port path
@@ -329,8 +333,10 @@ GPS::GPS(const char *path, gps_driver_mode_t mode, GPSHelper::Interface interfac
char c = _port[strlen(_port) - 1]; // last digit of path (eg /dev/ttyS2)
set_device_bus(c - 48); // sub 48 to convert char to integer
#ifdef __PX4_LINUX
} else if (_interface == GPSHelper::Interface::SPI) {
set_device_bus_type(device::Device::DeviceBusType::DeviceBusType_SPI);
#endif
}
if (_mode == gps_driver_mode_t::None) {
@@ -403,10 +409,22 @@ int GPS::callback(GPSCallbackType type, void *data1, int data2, void *user)
return num_read;
}
case GPSCallbackType::writeDeviceData:
gps->dumpGpsData((uint8_t *)data1, (size_t)data2, gps_dump_comm_mode_t::Full, true);
case GPSCallbackType::writeDeviceData: {
gps->dumpGpsData((uint8_t *)data1, (size_t)data2, gps_dump_comm_mode_t::Full, true);
return ::write(gps->_serial_fd, data1, (size_t)data2);
int ret = 0;
if (gps->_uart) {
ret = gps->_uart->write((void *) data1, (size_t) data2);
#ifdef __PX4_LINUX
} else if (gps->_spi_fd >= 0) {
ret = ::write(gps->_spi_fd, data1, (size_t)data2);
#endif
}
return ret;
}
case GPSCallbackType::setBaudrate:
return gps->setBaudrate(data2);
@@ -437,10 +455,11 @@ int GPS::callback(GPSCallbackType type, void *data1, int data2, void *user)
// as of 2021 setting the time on Nuttx temporarily pauses interrupts
// so only set the time if it is very wrong.
// TODO: clock slewing of the RTC for small time differences
#ifndef __PX4_QURT
px4_clock_settime(CLOCK_REALTIME, &rtc_gps_time);
#endif
}
break;
}
@@ -449,72 +468,64 @@ int GPS::callback(GPSCallbackType type, void *data1, int data2, void *user)
int GPS::pollOrRead(uint8_t *buf, size_t buf_length, int timeout)
{
int ret = 0;
const unsigned character_count = 32; // minimum bytes that we want to read
const int max_timeout = 50;
int timeout_adjusted = math::min(max_timeout, timeout);
handleInjectDataTopic();
#if !defined(__PX4_QURT)
if ((_interface == GPSHelper::Interface::UART) && (_uart)) {
ret = _uart->readAtLeast(buf, buf_length, character_count, timeout_adjusted);
/* For non QURT, use the usual polling. */
// SPI is only supported on Linux
#if defined(__PX4_LINUX)
//Poll only for the serial data. In the same thread we also need to handle orb messages,
//so ideally we would poll on both, the serial fd and orb subscription. Unfortunately the
//two pollings use different underlying mechanisms (at least under posix), which makes this
//impossible. Instead we limit the maximum polling interval and regularly check for new orb
//messages.
//FIXME: add a unified poll() API
const int max_timeout = 50;
} else if ((_interface == GPSHelper::Interface::SPI) && (_spi_fd >= 0)) {
pollfd fds[1];
fds[0].fd = _serial_fd;
fds[0].events = POLLIN;
//Poll only for the SPI data. In the same thread we also need to handle orb messages,
//so ideally we would poll on both, the SPI fd and orb subscription. Unfortunately the
//two pollings use different underlying mechanisms (at least under posix), which makes this
//impossible. Instead we limit the maximum polling interval and regularly check for new orb
//messages.
//FIXME: add a unified poll() API
int ret = poll(fds, sizeof(fds) / sizeof(fds[0]), math::min(max_timeout, timeout));
pollfd fds[1];
fds[0].fd = _spi_fd;
fds[0].events = POLLIN;
if (ret > 0) {
/* if we have new data from GPS, go handle it */
if (fds[0].revents & POLLIN) {
/*
* We are here because poll says there is some data, so this
* won't block even on a blocking device. But don't read immediately
* by 1-2 bytes, wait for some more data to save expensive read() calls.
* If we have all requested data available, read it without waiting.
* If more bytes are available, we'll go back to poll() again.
*/
const unsigned character_count = 32; // minimum bytes that we want to read
unsigned baudrate = _baudrate == 0 ? 115200 : _baudrate;
const unsigned sleeptime = character_count * 1000000 / (baudrate / 10);
ret = poll(fds, sizeof(fds) / sizeof(fds[0]), timeout_adjusted);
#ifdef __PX4_NUTTX
int err = 0;
int bytes_available = 0;
err = ::ioctl(_serial_fd, FIONREAD, (unsigned long)&bytes_available);
if (ret > 0) {
/* if we have new data from GPS, go handle it */
if (fds[0].revents & POLLIN) {
/*
* We are here because poll says there is some data, so this
* won't block even on a blocking device. But don't read immediately
* by 1-2 bytes, wait for some more data to save expensive read() calls.
* If we have all requested data available, read it without waiting.
* If more bytes are available, we'll go back to poll() again.
*/
unsigned baudrate = _baudrate == 0 ? 115200 : _baudrate;
const unsigned sleeptime = character_count * 1000000 / (baudrate / 10);
if (err != 0 || bytes_available < (int)character_count) {
px4_usleep(sleeptime);
ret = ::read(_spi_fd, buf, buf_length);
if (ret > 0) {
_num_bytes_read += ret;
}
} else {
ret = -1;
}
#else
px4_usleep(sleeptime);
#endif
ret = ::read(_serial_fd, buf, buf_length);
if (ret > 0) {
_num_bytes_read += ret;
}
} else {
ret = -1;
}
#endif
}
return ret;
#else
/* For QURT, just use read for now, since this doesn't block, we need to slow it down
* just a bit. */
px4_usleep(10000);
return ::read(_serial_fd, buf, buf_length);
#endif
}
void GPS::handleInjectDataTopic()
@@ -583,105 +594,38 @@ bool GPS::injectData(uint8_t *data, size_t len)
{
dumpGpsData(data, len, gps_dump_comm_mode_t::Full, true);
size_t written = ::write(_serial_fd, data, len);
::fsync(_serial_fd);
size_t written = 0;
if ((_interface == GPSHelper::Interface::UART) && (_uart)) {
written = _uart->write((const void *) data, len);
#ifdef __PX4_LINUX
} else if (_interface == GPSHelper::Interface::SPI) {
written = ::write(_spi_fd, data, len);
::fsync(_spi_fd);
#endif
}
return written == len;
}
int GPS::setBaudrate(unsigned baud)
{
/* process baud rate */
int speed;
if (_interface == GPSHelper::Interface::UART) {
if ((_uart) && (_uart->setBaudrate(baud))) {
return 0;
}
switch (baud) {
case 9600: speed = B9600; break;
#ifdef __PX4_LINUX
case 19200: speed = B19200; break;
case 38400: speed = B38400; break;
case 57600: speed = B57600; break;
case 115200: speed = B115200; break;
case 230400: speed = B230400; break;
#ifndef B460800
#define B460800 460800
} else if (_interface == GPSHelper::Interface::SPI) {
// Can't set the baudrate on a SPI port but just return a success
return 0;
#endif
case 460800: speed = B460800; break;
#ifndef B921600
#define B921600 921600
#endif
case 921600: speed = B921600; break;
default:
PX4_ERR("ERR: unknown baudrate: %d", baud);
return -EINVAL;
}
struct termios uart_config;
int termios_state;
/* fill the struct for the new configuration */
tcgetattr(_serial_fd, &uart_config);
/* properly configure the terminal (see also https://en.wikibooks.org/wiki/Serial_Programming/termios ) */
//
// Input flags - Turn off input processing
//
// convert break to null byte, no CR to NL translation,
// no NL to CR translation, don't mark parity errors or breaks
// no input parity check, don't strip high bit off,
// no XON/XOFF software flow control
//
uart_config.c_iflag &= ~(IGNBRK | BRKINT | ICRNL |
INLCR | PARMRK | INPCK | ISTRIP | IXON);
//
// Output flags - Turn off output processing
//
// no CR to NL translation, no NL to CR-NL translation,
// no NL to CR translation, no column 0 CR suppression,
// no Ctrl-D suppression, no fill characters, no case mapping,
// no local output processing
//
// config.c_oflag &= ~(OCRNL | ONLCR | ONLRET |
// ONOCR | ONOEOT| OFILL | OLCUC | OPOST);
uart_config.c_oflag = 0;
//
// No line processing
//
// echo off, echo newline off, canonical mode off,
// extended input processing off, signal chars off
//
uart_config.c_lflag &= ~(ECHO | ECHONL | ICANON | IEXTEN | ISIG);
/* no parity, one stop bit, disable flow control */
uart_config.c_cflag &= ~(CSTOPB | PARENB | CRTSCTS);
/* set baud rate */
if ((termios_state = cfsetispeed(&uart_config, speed)) < 0) {
GPS_ERR("ERR: %d (cfsetispeed)", termios_state);
return -1;
}
if ((termios_state = cfsetospeed(&uart_config, speed)) < 0) {
GPS_ERR("ERR: %d (cfsetospeed)", termios_state);
return -1;
}
if ((termios_state = tcsetattr(_serial_fd, TCSANOW, &uart_config)) < 0) {
GPS_ERR("ERR: %d (tcsetattr)", termios_state);
return -1;
}
return 0;
return -1;
}
void GPS::initializeCommunicationDump()
@@ -840,31 +784,58 @@ GPS::run()
_helper = nullptr;
}
if (_serial_fd < 0) {
/* open the serial port */
_serial_fd = ::open(_port, O_RDWR | O_NOCTTY);
if ((_interface == GPSHelper::Interface::UART) && (_uart == nullptr)) {
if (_serial_fd < 0) {
PX4_ERR("failed to open %s err: %d", _port, errno);
px4_sleep(1);
// Create the UART port instance
_uart = new Serial(_port);
if (_uart == nullptr) {
PX4_ERR("Error creating serial device %s", _port);
px4_usleep(100000);
continue;
}
}
if ((_interface == GPSHelper::Interface::UART) && (! _uart->isOpen())) {
// Configure the desired baudrate if one was specified by the user.
// Otherwise the default baudrate will be used.
if (_configured_baudrate) {
if (! _uart->setBaudrate(_configured_baudrate)) {
PX4_ERR("Error setting baudrate to %u on %s", _configured_baudrate, _port);
px4_usleep(100000);
continue;
}
}
// Open the UART. If this is successful then the UART is ready to use.
if (! _uart->open()) {
PX4_ERR("Error opening serial device %s", _port);
px4_usleep(100000);
continue;
}
#ifdef __PX4_LINUX
if (_interface == GPSHelper::Interface::SPI) {
int spi_speed = 1000000; // make sure the bus speed is not too high (required on RPi)
int status_value = ::ioctl(_serial_fd, SPI_IOC_WR_MAX_SPEED_HZ, &spi_speed);
} else if ((_interface == GPSHelper::Interface::SPI) && (_spi_fd < 0)) {
_spi_fd = ::open(_port, O_RDWR | O_NOCTTY);
if (status_value < 0) {
PX4_ERR("SPI_IOC_WR_MAX_SPEED_HZ failed for %s (%d)", _port, errno);
}
if (_spi_fd < 0) {
PX4_ERR("failed to open SPI port %s err: %d", _port, errno);
px4_sleep(1);
continue;
}
status_value = ::ioctl(_serial_fd, SPI_IOC_RD_MAX_SPEED_HZ, &spi_speed);
int spi_speed = 1000000; // make sure the bus speed is not too high (required on RPi)
int status_value = ::ioctl(_spi_fd, SPI_IOC_WR_MAX_SPEED_HZ, &spi_speed);
if (status_value < 0) {
PX4_ERR("SPI_IOC_RD_MAX_SPEED_HZ failed for %s (%d)", _port, errno);
}
if (status_value < 0) {
PX4_ERR("SPI_IOC_WR_MAX_SPEED_HZ failed for %s (%d)", _port, errno);
}
status_value = ::ioctl(_spi_fd, SPI_IOC_RD_MAX_SPEED_HZ, &spi_speed);
if (status_value < 0) {
PX4_ERR("SPI_IOC_RD_MAX_SPEED_HZ failed for %s (%d)", _port, errno);
}
#endif /* __PX4_LINUX */
@@ -1056,9 +1027,17 @@ GPS::run()
}
}
if (_serial_fd >= 0) {
::close(_serial_fd);
_serial_fd = -1;
if ((_interface == GPSHelper::Interface::UART) && (_uart)) {
(void) _uart->close();
delete _uart;
_uart = nullptr;
#ifdef __PX4_LINUX
} else if ((_interface == GPSHelper::Interface::SPI) && (_spi_fd >= 0)) {
::close(_spi_fd);
_spi_fd = -1;
#endif
}
if (_mode_auto) {
@@ -1477,12 +1456,12 @@ GPS *GPS::instantiate(int argc, char *argv[], Instance instance)
break;
case 'i':
if (!strcmp(myoptarg, "spi")) {
interface = GPSHelper::Interface::SPI;
} else if (!strcmp(myoptarg, "uart")) {
if (!strcmp(myoptarg, "uart")) {
interface = GPSHelper::Interface::UART;
#ifdef __PX4_LINUX
} else if (!strcmp(myoptarg, "spi")) {
interface = GPSHelper::Interface::SPI;
#endif
} else {
PX4_ERR("unknown interface: %s", myoptarg);
error_flag = true;
@@ -1490,12 +1469,12 @@ GPS *GPS::instantiate(int argc, char *argv[], Instance instance)
break;
case 'j':
if (!strcmp(myoptarg, "spi")) {
interface_secondary = GPSHelper::Interface::SPI;
} else if (!strcmp(myoptarg, "uart")) {
if (!strcmp(myoptarg, "uart")) {
interface_secondary = GPSHelper::Interface::UART;
#ifdef __PX4_LINUX
} else if (!strcmp(myoptarg, "spi")) {
interface_secondary = GPSHelper::Interface::SPI;
#endif
} else {
PX4_ERR("unknown interface for secondary: %s", myoptarg);
error_flag = true;
@@ -126,8 +126,9 @@ int ICM42688P::probe()
{
for (int i = 0; i < 3; i++) {
uint8_t whoami = RegisterRead(Register::BANK_0::WHO_AM_I);
uint8_t expected_whoami = isICM686 ? WHOAMI686 : WHOAMI;
if (whoami == WHOAMI || (isICM686 && whoami == WHOAMI686)) {
if (whoami == expected_whoami) {
return PX4_OK;
} else {
@@ -53,7 +53,6 @@
#define CBRK_BUZZER_KEY 782097
#define CBRK_SUPPLY_CHK_KEY 894281
#define CBRK_IO_SAFETY_KEY 22027
#define CBRK_AIRSPD_CHK_KEY 162128
#define CBRK_FLIGHTTERM_KEY 121212
#define CBRK_USB_CHK_KEY 197848
#define CBRK_VTOLARMING_KEY 159753
@@ -69,21 +69,6 @@ PARAM_DEFINE_INT32(CBRK_SUPPLY_CHK, 0);
*/
PARAM_DEFINE_INT32(CBRK_IO_SAFETY, 22027);
/**
* Circuit breaker for airspeed sensor
*
* Setting this parameter to 162128 will disable the check for an airspeed sensor.
* The sensor driver will not be started and it cannot be calibrated.
* WARNING: ENABLING THIS CIRCUIT BREAKER IS AT OWN RISK
*
* @reboot_required true
* @min 0
* @max 162128
* @category Developer
* @group Circuit Breaker
*/
PARAM_DEFINE_INT32(CBRK_AIRSPD_CHK, 0);
/**
* Circuit breaker for flight termination
*
+15 -4
View File
@@ -40,20 +40,31 @@ if (${PX4_PLATFORM} STREQUAL "nuttx")
if ("${CONFIG_SPI}" STREQUAL "y")
list(APPEND SRCS_PLATFORM nuttx/SPI.cpp)
endif()
list(APPEND SRCS_PLATFORM nuttx/SerialImpl.cpp)
elseif((${PX4_PLATFORM} MATCHES "qurt"))
list(APPEND SRCS_PLATFORM qurt/I2C.cpp)
list(APPEND SRCS_PLATFORM qurt/SPI.cpp)
list(APPEND SRCS_PLATFORM qurt/SerialImpl.cpp)
list(APPEND SRCS_PLATFORM qurt/uart.c)
elseif(UNIX AND NOT APPLE) #TODO: add linux PX4 platform type
# Linux I2Cdev and SPIdev
list(APPEND SRCS_PLATFORM
posix/I2C.cpp
posix/SPI.cpp
)
if ("${CONFIG_I2C}" STREQUAL "y")
list(APPEND SRCS_PLATFORM posix/I2C.cpp)
endif()
if ("${CONFIG_SPI}" STREQUAL "y")
list(APPEND SRCS_PLATFORM posix/SPI.cpp)
endif()
list(APPEND SRCS_PLATFORM posix/SerialImpl.cpp)
list(APPEND SRCS_PLATFORM posix/SerialSBUSImpl.cpp)
list(APPEND SRCS_PLATFORM posix/SerialStandardImpl.cpp)
endif()
px4_add_library(drivers__device
CDev.cpp
Serial.cpp
${SRCS_PLATFORM}
)
@@ -1,6 +1,6 @@
/****************************************************************************
*
* Copyright (c) 2023 PX4 Development Team. All rights reserved.
* Copyright (C) 2023 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
@@ -31,92 +31,73 @@
*
****************************************************************************/
#include "RoverControl.hpp"
#include "Serial.hpp"
using namespace time_literals;
using namespace matrix;
namespace rover_control
namespace device
{
RoverControl::RoverControl() :
ModuleParams(nullptr),
ScheduledWorkItem(MODULE_NAME, px4::wq_configurations::rate_ctrl),
_differential_drive_control(this)
Serial::Serial(const char *port, uint32_t baudrate) :
_impl(port, baudrate)
{
updateParams();
}
bool RoverControl::init()
Serial::~Serial()
{
ScheduleOnInterval(10_ms); // 100 Hz
return true;
}
void RoverControl::updateParams()
bool Serial::open()
{
ModuleParams::updateParams();
return _impl.open();
}
void RoverControl::Run()
bool Serial::isOpen() const
{
if (should_exit()) {
ScheduleClear();
exit_and_cleanup();
}
_differential_drive_control.Update();
return _impl.isOpen();
}
int RoverControl::task_spawn(int argc, char *argv[])
bool Serial::close()
{
RoverControl *instance = new RoverControl();
if (instance) {
_object.store(instance);
_task_id = task_id_is_work_queue;
if (instance->init()) {
return PX4_OK;
}
} else {
PX4_ERR("alloc failed");
}
delete instance;
_object.store(nullptr);
_task_id = -1;
return PX4_ERROR;
return _impl.close();
}
int RoverControl::custom_command(int argc, char *argv[])
ssize_t Serial::read(uint8_t *buffer, size_t buffer_size)
{
return print_usage("unknown command");
return _impl.read(buffer, buffer_size);
}
int RoverControl::print_usage(const char *reason)
ssize_t Serial::readAtLeast(uint8_t *buffer, size_t buffer_size, size_t character_count, uint32_t timeout_us)
{
if (reason) {
PX4_ERR("%s\n", reason);
}
PRINT_MODULE_DESCRIPTION(
R"DESCR_STR(
### Description
Rover state machine.
)DESCR_STR");
PRINT_MODULE_USAGE_NAME("rover_control", "controller");
PRINT_MODULE_USAGE_COMMAND("start");
PRINT_MODULE_USAGE_DEFAULT_COMMANDS();
return 0;
return _impl.readAtLeast(buffer, buffer_size, character_count, timeout_us);
}
extern "C" __EXPORT int rover_control_main(int argc, char *argv[])
ssize_t Serial::write(const void *buffer, size_t buffer_size)
{
return RoverControl::main(argc, argv);
return _impl.write(buffer, buffer_size);
}
} // namespace rover_control
uint32_t Serial::getBaudrate() const
{
return _impl.getBaudrate();
}
bool Serial::setBaudrate(uint32_t baudrate)
{
return _impl.setBaudrate(baudrate);
}
bool Serial::getSBUSMode() const
{
return _impl.getSBUSMode();
}
bool Serial::setSBUSMode(bool enable)
{
return _impl.setSBUSMode(enable);
}
const char *Serial::getPort() const
{
return _impl.getPort();
}
} // namespace device
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/****************************************************************************
*
* Copyright (C) 2023 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.
*
****************************************************************************/
#pragma once
// Bring in the correct platform implementation
#ifdef __PX4_NUTTX
#include "nuttx/SerialImpl.hpp"
#elif defined(__PX4_QURT)
#include "qurt/SerialImpl.hpp"
#else
#include "posix/SerialImpl.hpp"
#endif
namespace device __EXPORT
{
class Serial
{
public:
// Baud rate can be selected with constructor or by using setBaudrate
Serial(const char *port, uint32_t baudrate = 0);
virtual ~Serial();
// Open sets up the port and gets it configured. Unless an alternate mode
// is selected the port will be configured with parity disabled and 1 stop bit.
bool open();
bool isOpen() const;
bool close();
ssize_t read(uint8_t *buffer, size_t buffer_size);
ssize_t readAtLeast(uint8_t *buffer, size_t buffer_size, size_t character_count = 1, uint32_t timeout_us = 0);
ssize_t write(const void *buffer, size_t buffer_size);
uint32_t getBaudrate() const;
// If the port has already been opened it will be reconfigured with a change
// of baudrate.
bool setBaudrate(uint32_t baudrate);
// SBUS has special configuration considerations and methods so it
// is given a special mode. It has parity enabled and 2 stop bits
bool getSBUSMode() const;
bool setSBUSMode(bool enable);
const char *getPort() const;
private:
// Disable copy constructors
Serial(const Serial &);
Serial &operator=(const Serial &);
// platform implementation
SerialImpl _impl;
};
} // namespace device
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/****************************************************************************
*
* Copyright (C) 2023 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.
*
****************************************************************************/
#include "SerialImpl.hpp"
#include <string.h> // strncpy
#include <termios.h>
#include <px4_log.h>
#include <fcntl.h>
#include <errno.h>
#include <poll.h>
#include <drivers/drv_hrt.h>
#include <board_config.h>
namespace device
{
SerialImpl::SerialImpl(const char *port, uint32_t baudrate)
{
if (port) {
strncpy(_port, port, sizeof(_port) - 1);
_port[sizeof(_port) - 1] = '\0';
} else {
_port[0] = 0;
}
if (baudrate) {
_baudrate = baudrate;
} else {
// If baudrate is zero then choose a reasonable default
_baudrate = 9600;
}
}
SerialImpl::~SerialImpl()
{
if (isOpen()) {
close();
}
}
bool SerialImpl::configure()
{
struct termios uart_config;
if (_SBUSMode) {
if (_baudrate != DEFAULT_SBUS_BAUDRATE) {
PX4_WARN("Warning, SBUS baud rate being set to %lu", _baudrate);
}
/* even parity, two stop bits */
tcgetattr(_serial_fd, &uart_config);
cfsetspeed(&uart_config, _baudrate);
uart_config.c_cflag |= (CSTOPB | PARENB);
tcsetattr(_serial_fd, TCSANOW, &uart_config);
if (board_rc_singlewire(_port)) {
/* only defined in configs capable of IOCTL
* Note It is never turned off
*/
#ifdef TIOCSSINGLEWIRE
ioctl(_serial_fd, TIOCSSINGLEWIRE, SER_SINGLEWIRE_ENABLED);
#endif
}
} else {
/* process baud rate */
int speed;
switch (_baudrate) {
case 9600: speed = B9600; break;
case 19200: speed = B19200; break;
case 38400: speed = B38400; break;
case 57600: speed = B57600; break;
case 115200: speed = B115200; break;
case 230400: speed = B230400; break;
#ifndef B460800
#define B460800 460800
#endif
case 460800: speed = B460800; break;
#ifndef B921600
#define B921600 921600
#endif
case 921600: speed = B921600; break;
default:
PX4_ERR("ERR: unknown baudrate: %lu", _baudrate);
return false;
}
int termios_state;
/* fill the struct for the new configuration */
if ((termios_state = tcgetattr(_serial_fd, &uart_config)) < 0) {
PX4_ERR("ERR: %d (tcgetattr)", termios_state);
return false;
}
/* properly configure the terminal (see also https://en.wikibooks.org/wiki/Serial_Programming/termios ) */
//
// Input flags - Turn off input processing
//
// convert break to null byte, no CR to NL translation,
// no NL to CR translation, don't mark parity errors or breaks
// no input parity check, don't strip high bit off,
// no XON/XOFF software flow control
//
uart_config.c_iflag &= ~(IGNBRK | BRKINT | ICRNL |
INLCR | PARMRK | INPCK | ISTRIP | IXON);
//
// Output flags - Turn off output processing
//
// no CR to NL translation, no NL to CR-NL translation,
// no NL to CR translation, no column 0 CR suppression,
// no Ctrl-D suppression, no fill characters, no case mapping,
// no local output processing
//
// config.c_oflag &= ~(OCRNL | ONLCR | ONLRET |
// ONOCR | ONOEOT| OFILL | OLCUC | OPOST);
uart_config.c_oflag = 0;
//
// No line processing
//
// echo off, echo newline off, canonical mode off,
// extended input processing off, signal chars off
//
uart_config.c_lflag &= ~(ECHO | ECHONL | ICANON | IEXTEN | ISIG);
/* no parity, one stop bit, disable flow control */
uart_config.c_cflag &= ~(CSTOPB | PARENB | CRTSCTS);
/* set baud rate */
if ((termios_state = cfsetispeed(&uart_config, speed)) < 0) {
PX4_ERR("ERR: %d (cfsetispeed)", termios_state);
return false;
}
if ((termios_state = cfsetospeed(&uart_config, speed)) < 0) {
PX4_ERR("ERR: %d (cfsetospeed)", termios_state);
return false;
}
if ((termios_state = tcsetattr(_serial_fd, TCSANOW, &uart_config)) < 0) {
PX4_ERR("ERR: %d (tcsetattr)", termios_state);
return false;
}
}
return true;
}
bool SerialImpl::open()
{
if (isOpen()) {
return true;
}
// Open the serial port
int serial_fd = ::open(_port, O_RDWR | O_NOCTTY);
if (serial_fd < 0) {
PX4_ERR("failed to open %s err: %d", _port, errno);
return false;
}
_serial_fd = serial_fd;
// Configure the serial port
if (! configure()) {
PX4_ERR("failed to configure %s err: %d", _port, errno);
close();
return false;
}
_open = true;
return _open;
}
bool SerialImpl::isOpen() const
{
return _open;
}
bool SerialImpl::close()
{
if (_serial_fd >= 0) {
::close(_serial_fd);
}
_serial_fd = -1;
_open = false;
return true;
}
ssize_t SerialImpl::read(uint8_t *buffer, size_t buffer_size)
{
if (!_open) {
PX4_ERR("Cannot read from serial device until it has been opened");
return -1;
}
int ret = ::read(_serial_fd, buffer, buffer_size);
if (ret < 0) {
PX4_DEBUG("%s read error %d", _port, ret);
}
return ret;
}
ssize_t SerialImpl::readAtLeast(uint8_t *buffer, size_t buffer_size, size_t character_count, uint32_t timeout_us)
{
if (!_open) {
PX4_ERR("Cannot readAtLeast from serial device until it has been opened");
return -1;
}
if (buffer_size < character_count) {
PX4_ERR("%s: Buffer not big enough to hold desired amount of read data", __FUNCTION__);
return -1;
}
const hrt_abstime start_time_us = hrt_absolute_time();
int total_bytes_read = 0;
while ((total_bytes_read < (int) character_count) && (hrt_elapsed_time(&start_time_us) < timeout_us)) {
// Poll for incoming UART data.
pollfd fds[1];
fds[0].fd = _serial_fd;
fds[0].events = POLLIN;
hrt_abstime remaining_time = timeout_us - hrt_elapsed_time(&start_time_us);
if (remaining_time <= 0) { break; }
int ret = poll(fds, sizeof(fds) / sizeof(fds[0]), remaining_time);
if (ret > 0) {
if (fds[0].revents & POLLIN) {
ret = read(&buffer[total_bytes_read], buffer_size - total_bytes_read);
if (ret > 0) {
total_bytes_read += ret;
}
} else {
PX4_ERR("Got a poll error");
return -1;
}
}
}
return total_bytes_read;
}
ssize_t SerialImpl::write(const void *buffer, size_t buffer_size)
{
if (!_open) {
PX4_ERR("Cannot write to serial device until it has been opened");
return -1;
}
int written = ::write(_serial_fd, buffer, buffer_size);
::fsync(_serial_fd);
if (written < 0) {
PX4_ERR("%s write error %d", _port, written);
}
return written;
}
const char *SerialImpl::getPort() const
{
return _port;
}
uint32_t SerialImpl::getBaudrate() const
{
return _baudrate;
}
bool SerialImpl::setBaudrate(uint32_t baudrate)
{
// check if already configured
if (baudrate == _baudrate) {
return true;
}
_baudrate = baudrate;
// process baud rate change now if port is already open
if ((_open) && (configure() != 0)) {
// Configure failed! Close the port
close();
return false;
}
return true;
}
bool SerialImpl::getSBUSMode() const
{
return _SBUSMode;
}
bool SerialImpl::setSBUSMode(bool enable)
{
if (_open) {
PX4_ERR("Cannot configure SBUS mode after port has already been opened");
return false;
}
_SBUSMode = enable;
_baudrate = DEFAULT_SBUS_BAUDRATE;
return true;
}
} // namespace device
@@ -0,0 +1,83 @@
/****************************************************************************
*
* Copyright (C) 2023 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.
*
****************************************************************************/
#pragma once
#include <stdint.h>
namespace device
{
class SerialImpl
{
public:
SerialImpl(const char *port, uint32_t baudrate);
virtual ~SerialImpl();
bool open();
bool isOpen() const;
bool close();
ssize_t read(uint8_t *buffer, size_t buffer_size);
ssize_t readAtLeast(uint8_t *buffer, size_t buffer_size, size_t character_count = 1, uint32_t timeout_us = 0);
ssize_t write(const void *buffer, size_t buffer_size);
const char *getPort() const;
uint32_t getBaudrate() const;
bool setBaudrate(uint32_t baudrate);
bool getSBUSMode() const;
bool setSBUSMode(bool enable);
private:
int _serial_fd{-1};
bool _open{false};
char _port[32] {};
uint32_t _baudrate{0};
bool _SBUSMode{false};
static const uint32_t DEFAULT_SBUS_BAUDRATE{100000};
bool configure();
};
} // namespace device
+253
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/****************************************************************************
*
* Copyright (C) 2023 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.
*
****************************************************************************/
#include "SerialImpl.hpp"
#include <unistd.h>
#include <string.h> // strncpy
#include <px4_log.h>
#include <fcntl.h>
#include <errno.h>
#include <poll.h>
#include <drivers/drv_hrt.h>
namespace device
{
SerialImpl::SerialImpl(const char *port, uint32_t baudrate)
{
if (port) {
strncpy(_port, port, sizeof(_port) - 1);
_port[sizeof(_port) - 1] = '\0';
} else {
_port[0] = 0;
}
if (baudrate) {
_baudrate = baudrate;
} else {
// If baudrate is zero then choose a reasonable default
_baudrate = 9600;
}
}
SerialImpl::~SerialImpl()
{
if (isOpen()) {
close();
}
}
bool SerialImpl::configure()
{
if (_SBUSMode) {
return _sbus.configure(_serial_fd, _baudrate);
}
return _standard.configure(_serial_fd, _baudrate);
}
bool SerialImpl::open()
{
if (isOpen()) {
return true;
}
// Open the serial port
int serial_fd = ::open(_port, O_RDWR | O_NOCTTY);
if (serial_fd < 0) {
PX4_ERR("failed to open %s err: %d", _port, errno);
return false;
}
_serial_fd = serial_fd;
// Configure the serial port
if (! configure()) {
PX4_ERR("failed to configure %s err: %d", _port, errno);
close();
return false;
}
_open = true;
return _open;
}
bool SerialImpl::isOpen() const
{
return _open;
}
bool SerialImpl::close()
{
if (_serial_fd >= 0) {
::close(_serial_fd);
}
_serial_fd = -1;
_open = false;
return true;
}
ssize_t SerialImpl::read(uint8_t *buffer, size_t buffer_size)
{
if (!_open) {
PX4_ERR("Cannot read from serial device until it has been opened");
return -1;
}
int ret = ::read(_serial_fd, buffer, buffer_size);
if (ret < 0) {
PX4_DEBUG("%s read error %d", _port, ret);
}
return ret;
}
ssize_t SerialImpl::readAtLeast(uint8_t *buffer, size_t buffer_size, size_t character_count, uint32_t timeout_us)
{
if (!_open) {
PX4_ERR("Cannot readAtLeast from serial device until it has been opened");
return -1;
}
if (buffer_size < character_count) {
PX4_ERR("%s: Buffer not big enough to hold desired amount of read data", __FUNCTION__);
return -1;
}
const hrt_abstime start_time_us = hrt_absolute_time();
int total_bytes_read = 0;
while ((total_bytes_read < (int) character_count) && (hrt_elapsed_time(&start_time_us) < timeout_us)) {
// Poll for incoming UART data.
pollfd fds[1];
fds[0].fd = _serial_fd;
fds[0].events = POLLIN;
hrt_abstime remaining_time = timeout_us - hrt_elapsed_time(&start_time_us);
if (remaining_time <= 0) { break; }
int ret = poll(fds, sizeof(fds) / sizeof(fds[0]), remaining_time);
if (ret > 0) {
if (fds[0].revents & POLLIN) {
ret = read(&buffer[total_bytes_read], buffer_size - total_bytes_read);
if (ret > 0) {
total_bytes_read += ret;
}
} else {
PX4_ERR("Got a poll error");
return -1;
}
}
}
return total_bytes_read;
}
ssize_t SerialImpl::write(const void *buffer, size_t buffer_size)
{
if (!_open) {
PX4_ERR("Cannot write to serial device until it has been opened");
return -1;
}
int written = ::write(_serial_fd, buffer, buffer_size);
::fsync(_serial_fd);
if (written < 0) {
PX4_ERR("%s write error %d", _port, written);
}
return written;
}
const char *SerialImpl::getPort() const
{
return _port;
}
uint32_t SerialImpl::getBaudrate() const
{
return _baudrate;
}
bool SerialImpl::setBaudrate(uint32_t baudrate)
{
// check if already configured
if (baudrate == _baudrate) {
return true;
}
_baudrate = baudrate;
// process baud rate change now if port is already open
if ((_open) && (configure() != 0)) {
// Configure failed! Close the port
close();
return false;
}
return true;
}
bool SerialImpl::getSBUSMode() const
{
return _SBUSMode;
}
bool SerialImpl::setSBUSMode(bool enable)
{
if (_open) {
PX4_ERR("Cannot configure SBUS mode after port has already been opened");
return false;
}
_SBUSMode = enable;
_baudrate = SerialSBUSImpl::DEFAULT_BAUDRATE;
return true;
}
} // namespace device
@@ -0,0 +1,89 @@
/****************************************************************************
*
* Copyright (C) 2023 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.
*
****************************************************************************/
#pragma once
#include <stdint.h>
#include "SerialSBUSImpl.hpp"
#include "SerialStandardImpl.hpp"
namespace device
{
class SerialImpl
{
public:
SerialImpl(const char *port, uint32_t baudrate);
virtual ~SerialImpl();
bool open();
bool isOpen() const;
bool close();
ssize_t read(uint8_t *buffer, size_t buffer_size);
ssize_t readAtLeast(uint8_t *buffer, size_t buffer_size, size_t character_count = 1, uint32_t timeout_us = 0);
ssize_t write(const void *buffer, size_t buffer_size);
const char *getPort() const;
uint32_t getBaudrate() const;
bool setBaudrate(uint32_t baudrate);
bool getSBUSMode() const;
bool setSBUSMode(bool enable);
private:
int _serial_fd{-1};
bool _open{false};
char _port[32] {};
uint32_t _baudrate{0};
bool _SBUSMode{false};
// The configuration routines for SBUS versus other needed to be separated
// out because they use different methods with different, conflicting header files
SerialSBUSImpl _sbus;
SerialStandardImpl _standard;
bool configure();
};
} // namespace device
@@ -0,0 +1,80 @@
/****************************************************************************
*
* Copyright (C) 2023 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.
*
****************************************************************************/
#include "SerialSBUSImpl.hpp"
#include <sys/ioctl.h>
#include <asm-generic/termbits.h>
#include <px4_log.h>
namespace device
{
bool SerialSBUSImpl::configure(int fd, uint32_t baud)
{
struct termios2 tio = {};
if (ioctl(fd, TCGETS2, &tio)) {
return false;
}
if (baud != DEFAULT_BAUDRATE) {
PX4_WARN("Warning, SBUS baud rate being set to %u", baud);
}
/**
* Setting serial port,8E2, non-blocking.100Kbps
*/
tio.c_iflag &= ~(IGNBRK | BRKINT | PARMRK | ISTRIP | INLCR | IGNCR | ICRNL
| IXON);
tio.c_iflag |= (INPCK | IGNPAR);
tio.c_oflag &= ~OPOST;
tio.c_lflag &= ~(ECHO | ECHONL | ICANON | ISIG | IEXTEN);
tio.c_cflag &= ~(CSIZE | CRTSCTS | PARODD | CBAUD);
/**
* use BOTHER to specify speed directly in c_[io]speed member
*/
tio.c_cflag |= (CS8 | CSTOPB | CLOCAL | PARENB | BOTHER | CREAD);
tio.c_ispeed = baud;
tio.c_ospeed = baud;
tio.c_cc[VMIN] = 25;
tio.c_cc[VTIME] = 0;
if (ioctl(fd, TCSETS2, &tio)) {
return false;
}
return true;
}
} // namespace device
@@ -0,0 +1,53 @@
/****************************************************************************
*
* Copyright (C) 2023 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.
*
****************************************************************************/
#pragma once
#include <stdint.h>
namespace device
{
class SerialSBUSImpl
{
public:
SerialSBUSImpl() {};
virtual ~SerialSBUSImpl() {};
bool configure(int fd, uint32_t baud);
static const uint32_t DEFAULT_BAUDRATE{100000};
};
} // namespace device
@@ -0,0 +1,159 @@
/****************************************************************************
*
* Copyright (C) 2023 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.
*
****************************************************************************/
#include "SerialStandardImpl.hpp"
#include <sys/termios.h>
#include <px4_log.h>
namespace device
{
bool SerialStandardImpl::validateBaudrate(uint32_t baudrate)
{
return ((baudrate == 9600) ||
(baudrate == 19200) ||
(baudrate == 38400) ||
(baudrate == 57600) ||
(baudrate == 115200) ||
(baudrate == 230400) ||
(baudrate == 460800) ||
(baudrate == 921600));
}
bool SerialStandardImpl::configure(int fd, uint32_t baud)
{
/* process baud rate */
int speed;
if (! validateBaudrate(baud)) {
PX4_ERR("ERR: unknown baudrate: %u", baud);
return false;
}
switch (baud) {
case 9600: speed = B9600; break;
case 19200: speed = B19200; break;
case 38400: speed = B38400; break;
case 57600: speed = B57600; break;
case 115200: speed = B115200; break;
case 230400: speed = B230400; break;
#ifndef B460800
#define B460800 460800
#endif
case 460800: speed = B460800; break;
#ifndef B921600
#define B921600 921600
#endif
case 921600: speed = B921600; break;
default:
PX4_ERR("ERR: unknown baudrate: %d", baud);
return false;
}
struct termios uart_config;
int termios_state;
/* fill the struct for the new configuration */
if ((termios_state = tcgetattr(fd, &uart_config)) < 0) {
PX4_ERR("ERR: %d (tcgetattr)", termios_state);
return false;
}
/* properly configure the terminal (see also https://en.wikibooks.org/wiki/Serial_Programming/termios ) */
//
// Input flags - Turn off input processing
//
// convert break to null byte, no CR to NL translation,
// no NL to CR translation, don't mark parity errors or breaks
// no input parity check, don't strip high bit off,
// no XON/XOFF software flow control
//
uart_config.c_iflag &= ~(IGNBRK | BRKINT | ICRNL |
INLCR | PARMRK | INPCK | ISTRIP | IXON);
//
// Output flags - Turn off output processing
//
// no CR to NL translation, no NL to CR-NL translation,
// no NL to CR translation, no column 0 CR suppression,
// no Ctrl-D suppression, no fill characters, no case mapping,
// no local output processing
//
// config.c_oflag &= ~(OCRNL | ONLCR | ONLRET |
// ONOCR | ONOEOT| OFILL | OLCUC | OPOST);
uart_config.c_oflag = 0;
//
// No line processing
//
// echo off, echo newline off, canonical mode off,
// extended input processing off, signal chars off
//
uart_config.c_lflag &= ~(ECHO | ECHONL | ICANON | IEXTEN | ISIG);
/* no parity, one stop bit, disable flow control */
uart_config.c_cflag &= ~(CSTOPB | PARENB | CRTSCTS);
/* set baud rate */
if ((termios_state = cfsetispeed(&uart_config, speed)) < 0) {
PX4_ERR("ERR: %d (cfsetispeed)", termios_state);
return false;
}
if ((termios_state = cfsetospeed(&uart_config, speed)) < 0) {
PX4_ERR("ERR: %d (cfsetospeed)", termios_state);
return false;
}
if ((termios_state = tcsetattr(fd, TCSANOW, &uart_config)) < 0) {
PX4_ERR("ERR: %d (tcsetattr)", termios_state);
return false;
}
return true;
}
} // namespace device
@@ -0,0 +1,55 @@
/****************************************************************************
*
* Copyright (C) 2023 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.
*
****************************************************************************/
#pragma once
#include <stdint.h>
namespace device
{
class SerialStandardImpl
{
public:
SerialStandardImpl() {};
virtual ~SerialStandardImpl() {};
bool configure(int fd, uint32_t baud);
private:
bool validateBaudrate(uint32_t baudrate);
};
} // namespace device
+239
View File
@@ -0,0 +1,239 @@
/****************************************************************************
*
* Copyright (C) 2023 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.
*
****************************************************************************/
#include "SerialImpl.hpp"
#include <string.h> // strncpy
#include <px4_log.h>
#include <drivers/device/qurt/uart.h>
#include <drivers/drv_hrt.h>
namespace device
{
SerialImpl::SerialImpl(const char *port, uint32_t baudrate)
{
if (port) {
strncpy(_port, port, sizeof(_port) - 1);
_port[sizeof(_port) - 1] = '\0';
} else {
_port[0] = 0;
}
if (baudrate) {
_baudrate = baudrate;
} else {
// If baudrate is zero then choose a reasonable default.
// The default is the GPS UBX M10 default rate.
_baudrate = 115200;
}
}
SerialImpl::~SerialImpl()
{
if (isOpen()) {
close();
}
}
bool SerialImpl::open()
{
// There's no harm in calling open multiple times on the same port.
// In fact, that's the only way to change the baudrate
_open = false;
_serial_fd = -1;
// qurt_uart_open will check validity of port and baudrate
int serial_fd = qurt_uart_open(_port, _baudrate);
if (serial_fd < 0) {
PX4_ERR("failed to open %s at baudrate %u, fd: %d", _port, _baudrate, serial_fd);
close();
return false;
} else {
PX4_INFO("Successfully opened UART %s with baudrate %u", _port, _baudrate);
}
_serial_fd = serial_fd;
_open = true;
return _open;
}
bool SerialImpl::isOpen() const
{
return _open;
}
bool SerialImpl::close()
{
// No close defined for qurt uart yet
// if (_serial_fd >= 0) {
// qurt_uart_close(_serial_fd);
// }
_serial_fd = -1;
_open = false;
return true;
}
ssize_t SerialImpl::read(uint8_t *buffer, size_t buffer_size)
{
if (!_open) {
PX4_ERR("Cannot read from serial device until it has been opened");
return -1;
}
int ret_read = qurt_uart_read(_serial_fd, (char *) buffer, buffer_size, 500);
if (ret_read < 0) {
PX4_DEBUG("%s read error %d", _port, ret_read);
}
return ret_read;
}
ssize_t SerialImpl::readAtLeast(uint8_t *buffer, size_t buffer_size, size_t character_count, uint32_t timeout_us)
{
if (!_open) {
PX4_ERR("Cannot readAtLeast from serial device until it has been opened");
return -1;
}
if (buffer_size < character_count) {
PX4_ERR("%s: Buffer not big enough to hold desired amount of read data", __FUNCTION__);
return -1;
}
const hrt_abstime start_time_us = hrt_absolute_time();
int total_bytes_read = 0;
while (total_bytes_read < (int) character_count) {
if (timeout_us > 0) {
const uint64_t elapsed_us = hrt_elapsed_time(&start_time_us);
if (elapsed_us >= timeout_us) {
// If there was a partial read but not enough to satisfy the minimum then they will be lost
// but this really should never happen when everything is working normally.
// PX4_WARN("%s timeout %d bytes read (%llu us elapsed)", __FUNCTION__, total_bytes_read, elapsed_us);
// Or, instead of returning an error, should we return the number of bytes read (assuming it is greater than zero)?
return total_bytes_read;
}
}
int current_bytes_read = read(&buffer[total_bytes_read], buffer_size - total_bytes_read);
if (current_bytes_read < 0) {
// Again, if there was a partial read but not enough to satisfy the minimum then they will be lost
// but this really should never happen when everything is working normally.
PX4_ERR("%s failed to read uart", __FUNCTION__);
// Or, instead of returning an error, should we return the number of bytes read (assuming it is greater than zero)?
return -1;
}
// Current bytes read could be zero
total_bytes_read += current_bytes_read;
// If we have at least reached our desired minimum number of characters
// then we can return now
if (total_bytes_read >= (int) character_count) {
return total_bytes_read;
}
// Wait a set amount of time before trying again or the remaining time
// until the timeout if we are getting close
const uint64_t elapsed_us = hrt_elapsed_time(&start_time_us);
int64_t time_until_timeout = timeout_us - elapsed_us;
uint64_t time_to_sleep = 5000;
if ((time_until_timeout >= 0) &&
(time_until_timeout < (int64_t) time_to_sleep)) {
time_to_sleep = time_until_timeout;
}
px4_usleep(time_to_sleep);
}
return -1;
}
ssize_t SerialImpl::write(const void *buffer, size_t buffer_size)
{
if (!_open) {
PX4_ERR("Cannot write to serial device until it has been opened");
return -1;
}
int ret_write = qurt_uart_write(_serial_fd, (const char *) buffer, buffer_size);
if (ret_write < 0) {
PX4_ERR("%s write error %d", _port, ret_write);
}
return ret_write;
}
const char *SerialImpl::getPort() const
{
return _port;
}
uint32_t SerialImpl::getBaudrate() const
{
return _baudrate;
}
bool SerialImpl::setBaudrate(uint32_t baudrate)
{
// check if already configured
if (baudrate == _baudrate) {
return true;
}
_baudrate = baudrate;
// process baud rate change now if port is already open
if (_open) {
return open();
}
return true;
}
} // namespace device
@@ -0,0 +1,80 @@
/****************************************************************************
*
* Copyright (C) 2023 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.
*
****************************************************************************/
#pragma once
#include <stdint.h>
namespace device
{
class SerialImpl
{
public:
SerialImpl(const char *port, uint32_t baudrate);
virtual ~SerialImpl();
bool open();
bool isOpen() const;
bool close();
ssize_t read(uint8_t *buffer, size_t buffer_size);
ssize_t readAtLeast(uint8_t *buffer, size_t buffer_size, size_t character_count = 1, uint32_t timeout_us = 0);
ssize_t write(const void *buffer, size_t buffer_size);
const char *getPort() const;
uint32_t getBaudrate() const;
bool setBaudrate(uint32_t baudrate);
// Cannot configure Qurt UARTs for SBUS!
bool getSBUSMode() const { return false; }
bool setSBUSMode(bool enable) { return false; }
private:
int _serial_fd{-1};
bool _open{false};
char _port[32] {};
uint32_t _baudrate{0};
bool validateBaudrate(uint32_t baudrate);
};
} // namespace device
+8
View File
@@ -35,6 +35,8 @@ public:
assert(y0 + Q <= N);
}
Slice(const Slice<Type, P, Q, M, N> &other) = default;
const Type &operator()(size_t i, size_t j) const
{
assert(i < P);
@@ -52,6 +54,12 @@ public:
return (*_data)(_x0 + i, _y0 + j);
}
// Separate function needed otherwise the default copy constructor matches before the deep copy implementation
Slice<Type, P, Q, M, N> &operator=(const Slice<Type, P, Q, M, N> &other)
{
return this->operator=<M, N>(other);
}
template<size_t MM, size_t NN>
Slice<Type, P, Q, M, N> &operator=(const Slice<Type, P, Q, MM, NN> &other)
{
+9
View File
@@ -262,3 +262,12 @@ TEST(MatrixSliceTest, Slice)
float O_check_data_12 [4] = {2.5, 3, 4, 5};
EXPECT_EQ(res_12, (SquareMatrix<float, 2>(O_check_data_12)));
}
TEST(MatrixSliceTest, XYAssignmentTest)
{
Vector3f a(1, 2, 3);
Vector3f b(4, 5, 6);
// Assign first two elements from b to first two slot of a
a.xy() = b.xy();
EXPECT_EQ(a, Vector3f(4, 5, 3));
}
+19 -19
View File
@@ -85,7 +85,7 @@ public:
float canRun(const vehicle_local_position_s &local_pos, bool is_wind_valid) const;
/*
* Computes the lateral acceleration and airspeed references necessary to track
* Computes the lateral acceleration and true airspeed references necessary to track
* a path in wind (including excess wind conditions).
*
* @param[in] curr_pos_local Current horizontal vehicle position in local coordinates [m]
@@ -150,12 +150,12 @@ public:
void setMaxTrackKeepingMinGroundSpeed(float min_gsp) { min_gsp_track_keeping_max_ = math::max(min_gsp, 0.0f); }
/*
* Set the nominal airspeed reference [m/s].
* Set the nominal airspeed reference (true airspeed) [m/s].
*/
void setAirspeedNom(float airsp) { airspeed_nom_ = math::max(airsp, 0.1f); }
/*
* Set the maximum airspeed reference [m/s].
* Set the maximum airspeed reference (true airspeed) [m/s].
*/
void setAirspeedMax(float airsp) { airspeed_max_ = math::max(airsp, 0.1f); }
@@ -306,8 +306,8 @@ private:
// ^disabling this parameter disables all other excess wind handling options, using only the nominal airspeed for reference
// guidance settings
float airspeed_nom_{15.0f}; // nominal (desired) airspeed reference (generally equivalent to cruise optimized airspeed) [m/s]
float airspeed_max_{20.0f}; // maximum airspeed reference - the maximum achievable/allowed airspeed reference [m/s]
float airspeed_nom_{15.0f}; // nominal (desired) true airspeed reference (generally equivalent to cruise optimized airspeed) [m/s]
float airspeed_max_{20.0f}; // maximum true airspeed reference - the maximum achievable/allowed airspeed reference [m/s]
float roll_time_const_{0.0f}; // autopilot roll response time constant [s]
float min_gsp_desired_{0.0f}; // user defined miminum desired forward ground speed [m/s]
float min_gsp_track_keeping_max_{5.0f}; // maximum, minimum forward ground speed demand from track keeping logic [m/s]
@@ -341,8 +341,8 @@ private:
* guidance outputs
*/
float airspeed_ref_{15.0f}; // airspeed reference [m/s]
matrix::Vector2f air_vel_ref_{matrix::Vector2f{15.0f, 0.0f}}; // air velocity reference vector [m/s]
float airspeed_ref_{15.0f}; // true airspeed reference [m/s]
matrix::Vector2f air_vel_ref_{matrix::Vector2f{15.0f, 0.0f}}; // true air velocity reference vector [m/s]
float lateral_accel_{0.0f}; // lateral acceleration reference [m/s^2]
float lateral_accel_ff_{0.0f}; // lateral acceleration demand to maintain path curvature [m/s^2]
@@ -358,7 +358,7 @@ private:
* condition, path properties, and stability bounds.
*
* @param[in] ground_speed Vehicle ground speed [m/s]
* @param[in] airspeed Vehicle airspeed [m/s]
* @param[in] airspeed Vehicle true airspeed [m/s]
* @param[in] wind_speed Wind speed [m/s]
* @param[in] track_error Track error (magnitude) [m]
* @param[in] path_curvature Path curvature at closest point on track [m^-1]
@@ -384,7 +384,7 @@ private:
/*
* Cacluates an approximation of the wind factor (see [TODO: include citation]).
*
* @param[in] airspeed Vehicle airspeed [m/s]
* @param[in] airspeed Vehicle true airspeed [m/s]
* @param[in] wind_speed Wind speed [m/s]
* @return Non-dimensional wind factor approximation
*/
@@ -395,7 +395,7 @@ private:
* track keeping stability.
*
* @param[in] air_turn_rate The turn rate required to track the current path
* curvature at the current airspeed, in a no-wind condition [rad/s]
* curvature at the current true airspeed, in a no-wind condition [rad/s]
* @param[in] wind_factor Non-dimensional wind factor (see [TODO: include citation])
* @return Period upper bound [s]
*/
@@ -408,7 +408,7 @@ private:
* and a safety factor should be applied in addition to the returned value.
*
* @param[in] air_turn_rate The turn rate required to track the current path
* curvature at the current airspeed, in a no-wind condition [rad/s]
* curvature at the current true airspeed, in a no-wind condition [rad/s]
* @param[in] wind_factor Non-dimensional wind factor (see [TODO: include citation])
* @return Period lower bound [s]
*/
@@ -493,8 +493,8 @@ private:
/*
* Determines a reference air velocity *without curvature compensation, but
* including "optimal" airspeed reference compensation in excess wind conditions.
* Nominal and maximum airspeed member variables must be set before using this method.
* including "optimal" true airspeed reference compensation in excess wind conditions.
* Nominal and maximum true airspeed member variables must be set before using this method.
*
* @param[in] wind_vel Wind velocity vector [m/s]
* @param[in] bearing_vec Bearing vector
@@ -512,7 +512,7 @@ private:
* Projection of the air velocity vector onto the bearing line considering
* a connected wind triangle.
*
* @param[in] airspeed Vehicle airspeed [m/s]
* @param[in] airspeed Vehicle true airspeed [m/s]
* @param[in] wind_cross_bearing 2D cross product of wind velocity and bearing vector [m/s]
* @return Projection of air velocity vector on bearing vector [m/s]
*/
@@ -523,7 +523,7 @@ private:
*
* @param[in] wind_cross_bearing 2D cross product of wind velocity and bearing vector [m/s]
* @param[in] wind_dot_bearing 2D dot product of wind velocity and bearing vector [m/s]
* @param[in] airspeed Vehicle airspeed [m/s]
* @param[in] airspeed Vehicle true airspeed [m/s]
* @param[in] wind_speed Wind speed [m/s]
* @return Binary bearing feasibility: 1 if feasible, 0 if infeasible
*/
@@ -549,7 +549,7 @@ private:
* @param[in] wind_vel Wind velocity vector [m/s]
* @param[in] bearing_vec Bearing vector
* @param[in] wind_speed Wind speed [m/s]
* @param[in] airspeed Vehicle airspeed [m/s]
* @param[in] airspeed Vehicle true airspeed [m/s]
* @return Air velocity vector [m/s]
*/
matrix::Vector2f infeasibleAirVelRef(const matrix::Vector2f &wind_vel, const matrix::Vector2f &bearing_vec,
@@ -562,7 +562,7 @@ private:
*
* @param[in] wind_cross_bearing 2D cross product of wind velocity and bearing vector [m/s]
* @param[in] wind_dot_bearing 2D dot product of wind velocity and bearing vector [m/s]
* @param[in] airspeed Vehicle airspeed [m/s]
* @param[in] airspeed Vehicle true airspeed [m/s]
* @param[in] wind_speed Wind speed [m/s]
* @return bearing feasibility
*/
@@ -577,7 +577,7 @@ private:
* in direction of path
* @param[in] ground_vel Vehicle ground velocity vector [m/s]
* @param[in] wind_vel Wind velocity vector [m/s]
* @param[in] airspeed Vehicle airspeed [m/s]
* @param[in] airspeed Vehicle true airspeed [m/s]
* @param[in] wind_speed Wind speed [m/s]
* @param[in] signed_track_error Signed error to track at closest point (sign
* determined by path normal direction) [m]
@@ -594,7 +594,7 @@ private:
*
* @param[in] air_vel Vechile air velocity vector [m/s]
* @param[in] air_vel_ref Reference air velocity vector [m/s]
* @param[in] airspeed Vehicle airspeed [m/s]
* @param[in] airspeed Vehicle true airspeed [m/s]
* @return Lateral acceleration demand [m/s^2]
*/
float lateralAccel(const matrix::Vector2f &air_vel, const matrix::Vector2f &air_vel_ref,
+29
View File
@@ -42,7 +42,36 @@
bool param_modify_on_import(bson_node_t node)
{
// 2023-12-06: translate and invert FW_ARSP_MODE-> FW_USE_AIRSPD
{
if (strcmp("FW_ARSP_MODE", node->name) == 0) {
if (node->i32 == 0) {
node->i32 = 1;
} else {
node->i32 = 0;
}
strcpy(node->name, "FW_USE_AIRSPD");
PX4_INFO("copying and inverting %s -> %s", "FW_ARSP_MODE", "FW_USE_AIRSPD");
return true;
}
}
// 2023-12-06: translate CBRK_AIRSPD_CHK-> SYS_HAS_NUM_ASPD
{
if (strcmp("CBRK_AIRSPD_CHK", node->name) == 0) {
if (node->i32 == 162128) {
node->i32 = 0;
strcpy(node->name, "SYS_HAS_NUM_ASPD");
PX4_INFO("copying %s -> %s", "CBRK_AIRSPD_CHK", "SYS_HAS_NUM_ASPD");
}
return true;
}
}
return false;
}
+13
View File
@@ -216,6 +216,19 @@ PARAM_DEFINE_INT32(SYS_HAS_MAG, 1);
*/
PARAM_DEFINE_INT32(SYS_HAS_BARO, 1);
/**
* Control if the vehicle has an airspeed sensor
*
* Set this to 0 if the board has no airspeed sensor.
* If set to 0, the preflight checks will not check for the presence of an
* airspeed sensor.
*
* @group System
* @min 0
* @max 1
*/
PARAM_DEFINE_INT32(SYS_HAS_NUM_ASPD, 0);
/**
* Number of distance sensors to check being available
*
@@ -600,9 +600,8 @@ void AirspeedModule::select_airspeed_and_publish()
}
// check if airspeed based on ground-wind speed is valid and can be published
if (_param_airspeed_primary_index.get() > airspeed_index::DISABLED_INDEX &&
(_valid_airspeed_index < airspeed_index::FIRST_SENSOR_INDEX
|| _param_airspeed_primary_index.get() == airspeed_index::GROUND_MINUS_WIND_INDEX)) {
if (_valid_airspeed_index < airspeed_index::FIRST_SENSOR_INDEX
|| _param_airspeed_primary_index.get() == airspeed_index::GROUND_MINUS_WIND_INDEX) {
// _vehicle_local_position_valid determines if ground-wind estimate is valid
if (_vehicle_local_position_valid &&
@@ -132,7 +132,6 @@ PARAM_DEFINE_FLOAT(ASPD_SCALE_3, 1.0f);
/**
* Index or primary airspeed measurement source
*
* @value -1 Disabled
* @value 0 Groundspeed minus windspeed
* @value 1 First airspeed sensor
* @value 2 Second airspeed sensor
@@ -1,6 +1,6 @@
/****************************************************************************
*
* Copyright (c) 2019 PX4 Development Team. All rights reserved.
* Copyright (c) 2019-2023 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
@@ -37,24 +37,20 @@
using namespace time_literals;
AirspeedChecks::AirspeedChecks()
: _param_fw_arsp_mode_handle(param_find("FW_ARSP_MODE")), _param_fw_airspd_max_handle(param_find("FW_AIRSPD_MAX"))
: _param_fw_airspd_max_handle(param_find("FW_AIRSPD_MAX"))
{
}
void AirspeedChecks::checkAndReport(const Context &context, Report &reporter)
{
if (circuit_breaker_enabled_by_val(_param_cbrk_airspd_chk.get(), CBRK_AIRSPD_CHK_KEY) ||
if (_param_sys_has_num_aspd.get() <= 0 ||
(context.status().vehicle_type != vehicle_status_s::VEHICLE_TYPE_FIXED_WING && !context.status().is_vtol)) {
return;
}
int32_t airspeed_mode = 0;
param_get(_param_fw_arsp_mode_handle, &airspeed_mode);
const bool optional = (airspeed_mode == 1);
airspeed_validated_s airspeed_validated;
if (_airspeed_validated_sub.copy(&airspeed_validated) && hrt_elapsed_time(&airspeed_validated.timestamp) < 1_s) {
if (_airspeed_validated_sub.copy(&airspeed_validated) && hrt_elapsed_time(&airspeed_validated.timestamp) < 2_s) {
reporter.setIsPresent(health_component_t::differential_pressure);
@@ -100,13 +96,13 @@ void AirspeedChecks::checkAndReport(const Context &context, Report &reporter)
}
}
} else if (!optional) {
} else {
/* EVENT
* @description
* <profile name="dev">
* Most likely the airspeed selector module is not running.
* This check can be configured via <param>CBRK_AIRSPD_CHK</param> parameter.
* This check can be configured via <param>SYS_HAS_NUM_ASPD</param> parameter.
* </profile>
*/
reporter.healthFailure(NavModes::All, health_component_t::differential_pressure,
@@ -1,6 +1,6 @@
/****************************************************************************
*
* Copyright (c) 2022 PX4 Development Team. All rights reserved.
* Copyright (c) 2022-2023 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
@@ -49,10 +49,9 @@ public:
private:
uORB::Subscription _airspeed_validated_sub{ORB_ID(airspeed_validated)};
const param_t _param_fw_arsp_mode_handle;
const param_t _param_fw_airspd_max_handle;
DEFINE_PARAMETERS_CUSTOM_PARENT(HealthAndArmingCheckBase,
(ParamInt<px4::params::CBRK_AIRSPD_CHK>) _param_cbrk_airspd_chk
(ParamInt<px4::params::SYS_HAS_NUM_ASPD>) _param_sys_has_num_aspd
)
};
@@ -239,7 +239,7 @@ ControlAllocator::update_effectiveness_source()
break;
case EffectivenessSource::ROVER_DIFFERENTIAL:
// rover_control does allocation and publishes directly to actuator_motors topic
// differential_drive_control does allocation and publishes directly to actuator_motors topic
break;
case EffectivenessSource::FIXED_WING:
@@ -34,13 +34,11 @@
add_subdirectory(DifferentialDriveKinematics)
px4_add_module(
MODULE modules__rover_control
MAIN rover_control
MODULE modules__differential_drive_control
MAIN differential_drive_control
SRCS
DifferentialDriveControl.cpp
DifferentialDriveControl.hpp
RoverControl.cpp
RoverControl.hpp
DEPENDS
DifferentialDriveKinematics
px4_work_queue
@@ -38,8 +38,8 @@ using namespace matrix;
namespace differential_drive_control
{
DifferentialDriveControl::DifferentialDriveControl(ModuleParams *parent) :
ModuleParams(parent),
DifferentialDriveControl::DifferentialDriveControl() :
ModuleParams(nullptr),
ScheduledWorkItem(MODULE_NAME, px4::wq_configurations::rate_ctrl)
{
updateParams();
@@ -47,7 +47,7 @@ DifferentialDriveControl::DifferentialDriveControl(ModuleParams *parent) :
bool DifferentialDriveControl::init()
{
// ScheduleOnInterval(10_ms); // 100 Hz
ScheduleOnInterval(10_ms); // 100 Hz
return true;
}
@@ -128,33 +128,27 @@ void DifferentialDriveControl::Run()
_actuator_motors_pub.publish(actuator_motors);
}
void DifferentialDriveControl::Update()
{
Run();
}
int DifferentialDriveControl::task_spawn(int argc, char *argv[])
{
// DifferentialDriveControl *instance = new DifferentialDriveControl();
DifferentialDriveControl *instance = new DifferentialDriveControl();
// if (instance) {
// _object.store(instance);
// _task_id = task_id_is_work_queue;
if (instance) {
_object.store(instance);
_task_id = task_id_is_work_queue;
// if (instance->init()) {
// return PX4_OK;
// }
if (instance->init()) {
return PX4_OK;
}
// } else {
// PX4_ERR("alloc failed");
// }
} else {
PX4_ERR("alloc failed");
}
// delete instance;
// _object.store(nullptr);
// _task_id = -1;
delete instance;
_object.store(nullptr);
_task_id = -1;
// return PX4_ERROR;
return PX4_OK;
return PX4_ERROR;
}
int DifferentialDriveControl::custom_command(int argc, char *argv[])
@@ -66,7 +66,7 @@ class DifferentialDriveControl : public ModuleBase<DifferentialDriveControl>, pu
public px4::ScheduledWorkItem
{
public:
DifferentialDriveControl(ModuleParams *parent);
DifferentialDriveControl();
~DifferentialDriveControl() override = default;
/** @see ModuleBase */
@@ -80,8 +80,6 @@ public:
bool init();
void Update();
protected:
void updateParams() override;
@@ -65,3 +65,4 @@ matrix::Vector2f DifferentialDriveKinematics::computeInverseKinematics(float lin
return Vector2f(linear_velocity_x - rotational_velocity,
linear_velocity_x + rotational_velocity) / _max_speed;
}
@@ -1,5 +1,5 @@
menuconfig MODULES_ROVER_CONTROL
bool "ROVER_CONTROL"
menuconfig MODULES_DIFFERENTIAL_DRIVE_CONTROL
bool "differential_drive_control"
default n
depends on MODULES_CONTROL_ALLOCATOR
---help---
@@ -1,5 +1,5 @@
Timestamp,state[0],state[1],state[2],state[3],state[4],state[5],state[6],state[7],state[8],state[9],state[10],state[11],state[12],state[13],state[14],state[15],state[16],state[17],state[18],state[19],state[20],state[21],state[22],state[23],variance[0],variance[1],variance[2],variance[3],variance[4],variance[5],variance[6],variance[7],variance[8],variance[9],variance[10],variance[11],variance[12],variance[13],variance[14],variance[15],variance[16],variance[17],variance[18],variance[19],variance[20],variance[21],variance[22],variance[23]
10000,1,-0.0094,-0.01,-3.2e-06,0.00023,7.3e-05,-0.011,7.1e-06,2.2e-06,-0.00045,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0.01,0.01,0.00018,25,25,10,1e+02,1e+02,1e+02,0.01,0.01,0.01,0.04,0.04,0.04,0,0,0,0,0,0,0,0
10000,1,-0.0094,-0.01,-3.2e-06,0.00023,7.3e-05,-0.011,7.2e-06,2.2e-06,-0.00045,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0.01,0.01,0.00018,25,25,10,1e+02,1e+02,1e+02,0.01,0.01,0.01,0.04,0.04,0.04,0,0,0,0,0,0,0,0
90000,1,-0.0094,-0.011,6.9e-05,-0.00047,0.0026,-0.026,-1.6e-05,0.00011,-0.0023,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0.01,0.01,0.00046,25,25,10,1e+02,1e+02,1e+02,0.01,0.01,0.01,0.04,0.04,0.04,0,0,0,0,0,0,0,0
190000,1,-0.0094,-0.011,2.8e-05,6.9e-05,0.004,-0.041,-5.9e-06,0.00043,-0.0044,-3e-11,-2.7e-12,5.9e-13,0,0,-2e-09,0,0,0,0,0,0,0,0,0.011,0.011,0.00093,25,25,10,1e+02,1e+02,1,0.01,0.01,0.01,0.04,0.04,0.04,0,0,0,0,0,0,0,0
290000,1,-0.0094,-0.011,6.3e-05,0.001,0.0064,-0.053,3.8e-05,0.00036,-0.007,9.1e-10,1e-10,-2.8e-11,0,0,-4.8e-07,0,0,0,0,0,0,0,0,0.012,0.011,0.00077,25,25,9.6,0.37,0.37,0.41,0.01,0.01,0.0052,0.04,0.04,0.04,0,0,0,0,0,0,0,0
@@ -219,7 +219,7 @@ Timestamp,state[0],state[1],state[2],state[3],state[4],state[5],state[6],state[7
21690000,0.77,-0.012,-0.0018,-0.63,0.0057,0.021,0.017,0.0021,0.009,-3.7e+02,-0.0015,-0.0061,4.4e-05,-0.0002,0.0088,-0.13,-0.017,-0.0037,0.57,0,0,0,0,0,0.00039,0.00039,0.02,0.025,0.025,0.0084,0.058,0.058,0.038,1.4e-06,1.4e-06,6.3e-06,0.029,0.029,0.0005,0,0,0,0,0,0,0,0
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21990000,0.77,-0.012,-0.0017,-0.63,0.0031,0.023,0.016,-0.00047,0.013,-3.7e+02,-0.0015,-0.0061,4.4e-05,-0.00035,0.0085,-0.13,-0.017,-0.0037,0.57,0,0,0,0,0,0.00038,0.00038,0.02,0.021,0.021,0.0081,0.047,0.047,0.038,1.2e-06,1.2e-06,6.3e-06,0.029,0.029,0.0005,0,0,0,0,0,0,0,0
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22290000,0.77,-0.012,-0.0017,-0.63,0.005,0.021,0.015,0.00028,0.015,-3.7e+02,-0.0015,-0.0061,4.4e-05,-6.1e-05,0.0084,-0.13,-0.017,-0.0037,0.57,0,0,0,0,0,0.00038,0.00038,0.02,0.022,0.022,0.008,0.051,0.051,0.037,1.1e-06,1.1e-06,6.3e-06,0.029,0.029,0.0005,0,0,0,0,0,0,0,0
1 Timestamp,state[0],state[1],state[2],state[3],state[4],state[5],state[6],state[7],state[8],state[9],state[10],state[11],state[12],state[13],state[14],state[15],state[16],state[17],state[18],state[19],state[20],state[21],state[22],state[23],variance[0],variance[1],variance[2],variance[3],variance[4],variance[5],variance[6],variance[7],variance[8],variance[9],variance[10],variance[11],variance[12],variance[13],variance[14],variance[15],variance[16],variance[17],variance[18],variance[19],variance[20],variance[21],variance[22],variance[23]
2 10000,1,-0.0094,-0.01,-3.2e-06,0.00023,7.3e-05,-0.011,7.1e-06,2.2e-06,-0.00045,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0.01,0.01,0.00018,25,25,10,1e+02,1e+02,1e+02,0.01,0.01,0.01,0.04,0.04,0.04,0,0,0,0,0,0,0,0 10000,1,-0.0094,-0.01,-3.2e-06,0.00023,7.3e-05,-0.011,7.2e-06,2.2e-06,-0.00045,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0.01,0.01,0.00018,25,25,10,1e+02,1e+02,1e+02,0.01,0.01,0.01,0.04,0.04,0.04,0,0,0,0,0,0,0,0
3 90000,1,-0.0094,-0.011,6.9e-05,-0.00047,0.0026,-0.026,-1.6e-05,0.00011,-0.0023,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0.01,0.01,0.00046,25,25,10,1e+02,1e+02,1e+02,0.01,0.01,0.01,0.04,0.04,0.04,0,0,0,0,0,0,0,0
4 190000,1,-0.0094,-0.011,2.8e-05,6.9e-05,0.004,-0.041,-5.9e-06,0.00043,-0.0044,-3e-11,-2.7e-12,5.9e-13,0,0,-2e-09,0,0,0,0,0,0,0,0,0.011,0.011,0.00093,25,25,10,1e+02,1e+02,1,0.01,0.01,0.01,0.04,0.04,0.04,0,0,0,0,0,0,0,0
5 290000,1,-0.0094,-0.011,6.3e-05,0.001,0.0064,-0.053,3.8e-05,0.00036,-0.007,9.1e-10,1e-10,-2.8e-11,0,0,-4.8e-07,0,0,0,0,0,0,0,0,0.012,0.011,0.00077,25,25,9.6,0.37,0.37,0.41,0.01,0.01,0.0052,0.04,0.04,0.04,0,0,0,0,0,0,0,0
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223 22090000,0.77,-0.012,-0.0017,-0.63,0.0035,0.022,0.015,-0.00015,0.016,-3.7e+02,-0.0015,-0.0061,4.4e-05,-0.00036,0.0085,-0.13,-0.017,-0.0037,0.57,0,0,0,0,0,0.00038,0.00038,0.02,0.023,0.023,0.0081,0.053,0.053,0.038,1.2e-06,1.2e-06,6.3e-06,0.029,0.029,0.0005,0,0,0,0,0,0,0,0
224 22190000,0.77,-0.012,-0.0017,-0.63,0.0038,0.019,0.015,-0.00015,0.013,-3.7e+02,-0.0015,-0.0061,4.4e-05,-5.3e-05,0.0084,-0.13,-0.017,-0.0037,0.57,0,0,0,0,0,0.00038,0.00038,0.02,0.021,0.021,0.008,0.046,0.046,0.037,1.1e-06,1.1e-06,6.3e-06,0.029,0.029,0.0005,0,0,0,0,0,0,0,0
225 22290000,0.77,-0.012,-0.0017,-0.63,0.005,0.021,0.015,0.00028,0.015,-3.7e+02,-0.0015,-0.0061,4.4e-05,-6.1e-05,0.0084,-0.13,-0.017,-0.0037,0.57,0,0,0,0,0,0.00038,0.00038,0.02,0.022,0.022,0.008,0.051,0.051,0.037,1.1e-06,1.1e-06,6.3e-06,0.029,0.029,0.0005,0,0,0,0,0,0,0,0
@@ -1,5 +1,5 @@
Timestamp,state[0],state[1],state[2],state[3],state[4],state[5],state[6],state[7],state[8],state[9],state[10],state[11],state[12],state[13],state[14],state[15],state[16],state[17],state[18],state[19],state[20],state[21],state[22],state[23],variance[0],variance[1],variance[2],variance[3],variance[4],variance[5],variance[6],variance[7],variance[8],variance[9],variance[10],variance[11],variance[12],variance[13],variance[14],variance[15],variance[16],variance[17],variance[18],variance[19],variance[20],variance[21],variance[22],variance[23]
10000,1,-0.011,-0.01,0.00023,0.00033,-0.00013,-0.01,1e-05,-3.8e-06,-0.00042,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0.01,0.01,0.00018,25,25,10,1e+02,1e+02,1e+02,0.01,0.01,0.01,0.04,0.04,0.04,0,0,0,0,0,0,0,0
10000,1,-0.011,-0.01,0.00023,0.00033,-0.00013,-0.01,1e-05,-3.9e-06,-0.00042,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0.01,0.01,0.00018,25,25,10,1e+02,1e+02,1e+02,0.01,0.01,0.01,0.04,0.04,0.04,0,0,0,0,0,0,0,0
90000,1,-0.011,-0.01,0.00033,-0.001,-0.0031,-0.024,-3.8e-05,-0.00013,-0.0021,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0.01,0.01,0.00046,25,25,10,1e+02,1e+02,1e+02,0.01,0.01,0.01,0.04,0.04,0.04,0,0,0,0,0,0,0,0
190000,1,-0.012,-0.011,0.00044,-0.0023,-0.003,-0.037,-0.00017,-0.00043,-0.017,4.7e-10,-5e-10,-1.5e-11,0,0,-6.8e-08,0,0,0,0,0,0,0,0,0.011,0.011,0.00094,25,25,10,1e+02,1e+02,1,0.01,0.01,0.01,0.04,0.04,0.04,0,0,0,0,0,0,0,0
290000,1,-0.012,-0.011,0.00044,-0.0033,-0.0044,-0.046,-0.00024,-0.00025,-0.018,3.8e-09,-5.9e-09,-4.7e-10,0,0,-2.9e-06,0,0,0,0,0,0,0,0,0.011,0.012,0.00077,25,25,9.6,0.37,0.37,0.41,0.01,0.01,0.0052,0.04,0.04,0.04,0,0,0,0,0,0,0,0
1 Timestamp,state[0],state[1],state[2],state[3],state[4],state[5],state[6],state[7],state[8],state[9],state[10],state[11],state[12],state[13],state[14],state[15],state[16],state[17],state[18],state[19],state[20],state[21],state[22],state[23],variance[0],variance[1],variance[2],variance[3],variance[4],variance[5],variance[6],variance[7],variance[8],variance[9],variance[10],variance[11],variance[12],variance[13],variance[14],variance[15],variance[16],variance[17],variance[18],variance[19],variance[20],variance[21],variance[22],variance[23]
2 10000,1,-0.011,-0.01,0.00023,0.00033,-0.00013,-0.01,1e-05,-3.8e-06,-0.00042,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0.01,0.01,0.00018,25,25,10,1e+02,1e+02,1e+02,0.01,0.01,0.01,0.04,0.04,0.04,0,0,0,0,0,0,0,0 10000,1,-0.011,-0.01,0.00023,0.00033,-0.00013,-0.01,1e-05,-3.9e-06,-0.00042,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0.01,0.01,0.00018,25,25,10,1e+02,1e+02,1e+02,0.01,0.01,0.01,0.04,0.04,0.04,0,0,0,0,0,0,0,0
3 90000,1,-0.011,-0.01,0.00033,-0.001,-0.0031,-0.024,-3.8e-05,-0.00013,-0.0021,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0.01,0.01,0.00046,25,25,10,1e+02,1e+02,1e+02,0.01,0.01,0.01,0.04,0.04,0.04,0,0,0,0,0,0,0,0
4 190000,1,-0.012,-0.011,0.00044,-0.0023,-0.003,-0.037,-0.00017,-0.00043,-0.017,4.7e-10,-5e-10,-1.5e-11,0,0,-6.8e-08,0,0,0,0,0,0,0,0,0.011,0.011,0.00094,25,25,10,1e+02,1e+02,1,0.01,0.01,0.01,0.04,0.04,0.04,0,0,0,0,0,0,0,0
5 290000,1,-0.012,-0.011,0.00044,-0.0033,-0.0044,-0.046,-0.00024,-0.00025,-0.018,3.8e-09,-5.9e-09,-4.7e-10,0,0,-2.9e-06,0,0,0,0,0,0,0,0,0.011,0.012,0.00077,25,25,9.6,0.37,0.37,0.41,0.01,0.01,0.0052,0.04,0.04,0.04,0,0,0,0,0,0,0,0
@@ -466,7 +466,7 @@ bool FlightTaskAuto::_evaluateTriplets()
}
// activation/deactivation of weather vane is based on parameter WV_EN and setting of navigator (allow_weather_vane)
_weathervane.setNavigatorForceDisabled(_sub_triplet_setpoint.get().current.disable_weather_vane);
_weathervane.setNavigatorForceDisabled(PX4_ISFINITE(_sub_triplet_setpoint.get().current.yaw));
// Calculate the current vehicle state and check if it has updated.
State previous_state = _current_state;
@@ -481,7 +481,7 @@ bool FlightTaskAuto::_evaluateTriplets()
_obstacle_avoidance.updateAvoidanceDesiredWaypoints(_triplet_target, _yaw_setpoint, _yawspeed_setpoint,
_triplet_next_wp,
_sub_triplet_setpoint.get().next.yaw,
_sub_triplet_setpoint.get().next.yawspeed_valid ? _sub_triplet_setpoint.get().next.yawspeed : (float)NAN,
(float)NAN,
_weathervane.isActive(), _sub_triplet_setpoint.get().current.type);
_obstacle_avoidance.checkAvoidanceProgress(
_position, _triplet_prev_wp, _target_acceptance_radius, Vector2f(_closest_pt));
@@ -509,13 +509,7 @@ bool FlightTaskAuto::_evaluateTriplets()
_yaw_setpoint = NAN;
_yawspeed_setpoint = 0.f;
} else if ((_type != WaypointType::takeoff || _sub_triplet_setpoint.get().current.disable_weather_vane)
&& _sub_triplet_setpoint.get().current.yaw_valid) {
// Use the yaw computed in Navigator except during takeoff because
// Navigator is not handling the yaw reset properly.
// But: use if from Navigator during takeoff if disable_weather_vane is true,
// because we're then aligning to the transition waypoint.
// TODO: fix in navigator
} else if (PX4_ISFINITE(_sub_triplet_setpoint.get().current.yaw)) {
_yaw_setpoint = _sub_triplet_setpoint.get().current.yaw;
_yawspeed_setpoint = NAN;
@@ -150,7 +150,7 @@ float FixedwingAttitudeControl::get_airspeed_constrained()
// if no airspeed measurement is available out best guess is to use the trim airspeed
float airspeed = _param_fw_airspd_trim.get();
if ((_param_fw_arsp_mode.get() == 0) && airspeed_valid) {
if (_param_fw_use_airspd.get() && airspeed_valid) {
/* prevent numerical drama by requiring 0.5 m/s minimal speed */
airspeed = math::max(0.5f, _airspeed_validated_sub.get().calibrated_airspeed_m_s);
@@ -135,7 +135,7 @@ private:
(ParamFloat<px4::params::FW_AIRSPD_MIN>) _param_fw_airspd_min,
(ParamFloat<px4::params::FW_AIRSPD_STALL>) _param_fw_airspd_stall,
(ParamFloat<px4::params::FW_AIRSPD_TRIM>) _param_fw_airspd_trim,
(ParamInt<px4::params::FW_ARSP_MODE>) _param_fw_arsp_mode,
(ParamBool<px4::params::FW_USE_AIRSPD>) _param_fw_use_airspd,
(ParamFloat<px4::params::FW_MAN_P_MAX>) _param_fw_man_p_max,
(ParamFloat<px4::params::FW_MAN_R_MAX>) _param_fw_man_r_max,
@@ -75,6 +75,7 @@ bool FwAutotuneAttitudeControl::init()
void FwAutotuneAttitudeControl::reset()
{
_param_fw_at_start.reset();
}
void FwAutotuneAttitudeControl::Run()
@@ -59,9 +59,6 @@ FixedwingPositionControl::FixedwingPositionControl(bool vtol) :
, _figure_eight(_npfg, _wind_vel, _eas2tas)
#endif // CONFIG_FIGURE_OF_EIGHT
{
if (vtol) {
_param_handle_airspeed_trans = param_find("VT_ARSP_TRANS");
}
// limit to 50 Hz
_local_pos_sub.set_interval_ms(20);
@@ -80,7 +77,6 @@ FixedwingPositionControl::FixedwingPositionControl(bool vtol) :
/* fetch initial parameter values */
parameters_update();
_airspeed_slew_rate_controller.setForcedValue(_performance_model.getCalibratedTrimAirspeed());
_roll_slew_rate.setSlewRate(radians(_param_fw_pn_r_slew_max.get()));
_roll_slew_rate.setForcedValue(0.f);
@@ -111,11 +107,6 @@ FixedwingPositionControl::parameters_update()
_roll_slew_rate.setSlewRate(radians(_param_fw_pn_r_slew_max.get()));
// VTOL parameter VT_ARSP_TRANS
if (_param_handle_airspeed_trans != PARAM_INVALID) {
param_get(_param_handle_airspeed_trans, &_param_airspeed_trans);
}
// NPFG parameters
_npfg.setPeriod(_param_npfg_period.get());
_npfg.setDamping(_param_npfg_damping.get());
@@ -214,20 +205,23 @@ FixedwingPositionControl::airspeed_poll()
bool airspeed_valid = _airspeed_valid;
airspeed_validated_s airspeed_validated;
if ((_param_fw_arsp_mode.get() == 0) && _airspeed_validated_sub.update(&airspeed_validated)) {
if (_param_fw_use_airspd.get() && _airspeed_validated_sub.update(&airspeed_validated)) {
_eas2tas = 1.0f; //this is the default value, taken in case of invalid airspeed
if (PX4_ISFINITE(airspeed_validated.calibrated_airspeed_m_s)
&& PX4_ISFINITE(airspeed_validated.true_airspeed_m_s)
&& (airspeed_validated.calibrated_airspeed_m_s > 0.0f)) {
&& (airspeed_validated.calibrated_airspeed_m_s > FLT_EPSILON)) {
airspeed_valid = true;
_time_airspeed_last_valid = airspeed_validated.timestamp;
_airspeed = airspeed_validated.calibrated_airspeed_m_s;
_airspeed_eas = airspeed_validated.calibrated_airspeed_m_s;
_eas2tas = constrain(airspeed_validated.true_airspeed_m_s / airspeed_validated.calibrated_airspeed_m_s, 0.9f, 2.0f);
} else {
airspeed_valid = false;
}
} else {
@@ -391,8 +385,15 @@ FixedwingPositionControl::adapt_airspeed_setpoint(const float control_interval,
calibrated_airspeed_setpoint = constrain(calibrated_airspeed_setpoint, calibrated_min_airspeed,
_performance_model.getMaximumCalibratedAirspeed());
if (!PX4_ISFINITE(_airspeed_slew_rate_controller.getState())) {
_airspeed_slew_rate_controller.setForcedValue(calibrated_airspeed_setpoint);
// initialize the airspeed setpoint to the max(current airsped, min airspeed)
if (!PX4_ISFINITE(_airspeed_slew_rate_controller.getState())
|| !_tecs_is_running) {
_airspeed_slew_rate_controller.setForcedValue(math::max(calibrated_min_airspeed, _airspeed_eas));
}
// reset the airspeed setpoint to the min airspeed if the min airspeed changes while in operation
if (_airspeed_slew_rate_controller.getState() < calibrated_min_airspeed) {
_airspeed_slew_rate_controller.setForcedValue(calibrated_min_airspeed);
}
if (control_interval > FLT_EPSILON) {
@@ -400,10 +401,6 @@ FixedwingPositionControl::adapt_airspeed_setpoint(const float control_interval,
_airspeed_slew_rate_controller.update(calibrated_airspeed_setpoint, control_interval);
}
if (_airspeed_slew_rate_controller.getState() < calibrated_min_airspeed) {
_airspeed_slew_rate_controller.setForcedValue(calibrated_min_airspeed);
}
if (_airspeed_slew_rate_controller.getState() > _performance_model.getMaximumCalibratedAirspeed()) {
_airspeed_slew_rate_controller.setForcedValue(_performance_model.getMaximumCalibratedAirspeed());
}
@@ -648,7 +645,7 @@ void
FixedwingPositionControl::updateManualTakeoffStatus()
{
if (!_completed_manual_takeoff) {
const bool at_controllable_airspeed = _airspeed > _performance_model.getMinimumCalibratedAirspeed(getLoadFactor())
const bool at_controllable_airspeed = _airspeed_eas > _performance_model.getMinimumCalibratedAirspeed(getLoadFactor())
|| !_airspeed_valid;
const bool is_hovering = _vehicle_status.vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING
&& _control_mode.flag_armed;
@@ -1372,7 +1369,7 @@ FixedwingPositionControl::control_auto_takeoff(const hrt_abstime &now, const flo
_runway_takeoff.forceSetFlyState();
}
_runway_takeoff.update(now, takeoff_airspeed, _airspeed, _current_altitude - _takeoff_ground_alt,
_runway_takeoff.update(now, takeoff_airspeed, _airspeed_eas, _current_altitude - _takeoff_ground_alt,
clearance_altitude_amsl - _takeoff_ground_alt);
// yaw control is disabled once in "taking off" state
@@ -2516,48 +2513,14 @@ FixedwingPositionControl::tecs_update_pitch_throttle(const float control_interva
const float desired_max_sinkrate, const float desired_max_climbrate,
bool disable_underspeed_detection, float hgt_rate_sp)
{
_tecs_is_running = true;
// do not run TECS if vehicle is a VTOL and we are in rotary wing mode or in transition
// (it should also not run during VTOL blending because airspeed is too low still)
if (_vehicle_status.is_vtol) {
if (_vehicle_status.vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING || _vehicle_status.in_transition_mode) {
_tecs_is_running = false;
}
if (_vehicle_status.in_transition_mode) {
// we're in transition
_was_in_transition = true;
// set this to transition airspeed to init tecs correctly
if (_param_fw_arsp_mode.get() == 1 && PX4_ISFINITE(_param_airspeed_trans)) {
// some vtols fly without airspeed sensor
_airspeed_after_transition = _param_airspeed_trans;
} else {
_airspeed_after_transition = _airspeed;
}
_airspeed_after_transition = constrain(_airspeed_after_transition,
_performance_model.getMinimumCalibratedAirspeed(getLoadFactor()),
_performance_model.getMaximumCalibratedAirspeed());
} else if (_was_in_transition) {
// after transition we ramp up desired airspeed from the speed we had coming out of the transition
_airspeed_after_transition += control_interval * 2.0f; // increase 2m/s
if (_airspeed_after_transition < airspeed_sp && _airspeed < airspeed_sp) {
airspeed_sp = max(_airspeed_after_transition, _airspeed);
} else {
_was_in_transition = false;
_airspeed_after_transition = 0.0f;
}
}
}
if (!_tecs_is_running) {
if (_vehicle_status.is_vtol && (_vehicle_status.vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING
|| _vehicle_status.in_transition_mode)) {
_tecs_is_running = false;
return;
} else {
_tecs_is_running = true;
}
/* update TECS vehicle state estimates */
@@ -2575,7 +2538,7 @@ FixedwingPositionControl::tecs_update_pitch_throttle(const float control_interva
_current_altitude,
alt_sp,
airspeed_sp,
_airspeed,
_airspeed_eas,
_eas2tas,
throttle_min,
throttle_max,

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