c8ce120c92
PX4 Flow: modernize output and replace warnx() with PX4_INFO/WARN
2018-07-02 21:44:29 +00:00
7402d8223b
Fix up references to pixhawk.org
2018-07-02 13:11:15 +02:00
fb3e3b1cad
uORB::DeviceNode initialize _publisher
2018-07-01 16:30:31 -04:00
8599495082
uORB add ORB_COMMUNICATOR define to enable remote uORB
2018-07-01 16:03:03 +00:00
6579b7254a
Change TECS max sink rate minimum value, because very fragile aircraft might not be able to sustain higher max sink rates
2018-07-01 10:42:27 -04:00
a76c4c55d4
Decrease default flare altitude. The previous value was way too high for any small aircraft. It was also unsafe because after the flar, pitch is currently controlled open-loop, which means that stall can potentially happen during the flare
2018-07-01 10:42:27 -04:00
8f09a20478
Update TECS integrator gain parameter description to represent the changes in https://github.com/PX4/ecl/commit/ccfba4997147658d8340f7efa351c19299120704
2018-07-01 10:42:27 -04:00
9ce83f2208
fix all sign-compare warnings
2018-07-01 09:36:55 +00:00
cf74166801
double promotion warning fix or ignore per module
2018-07-01 09:36:55 +00:00
11d348ec4f
microbench split into hrt, math, matrix, uorb
2018-07-01 09:25:22 +00:00
ea0a80d4d1
microbench add uorb and matrix test
2018-07-01 09:25:22 +00:00
3ba97297d5
tests simple timing microbenchmark
2018-07-01 09:25:22 +00:00
02d4405a62
c++11 default destructors
2018-06-30 19:55:08 -04:00
c39ac93ca8
device integrator cleanup initialization
2018-06-30 19:55:08 -04:00
16d67ed179
frsky_telemetry improved com port init ( fix #9783 ), minor refactor ( #9798 )
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* frsky_telemetry added support for hw flow control com port and minor improvements
* DTYPE tested OK. Return 0 for unix compatibility, whitespace removed. Full test start - status- stop - start -status OK
2018-06-29 21:41:53 +00:00
17df184953
Fix sending first High Latency message
2018-06-29 16:49:30 +00:00
ca1f7a4a19
Reenable the MissionManager for the Iridium mavlink instance
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The MissionManager handles the MAVLINK_MSG_ID_MISSION_SET_CURRENT command which should also be supported for SatCom.
2018-06-29 16:49:30 +00:00
8825bbed29
Increase the stack size for the IridiumSBD driver
2018-06-29 16:49:30 +00:00
a04468ba9f
ekf2: Fix EKF preflight check fail false positives
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Uses a relaxed yaw innovation check threshold for fixed wing vehicle that can recover from larger yaw errors after takeoff.
Replaces the peak hold with decay filtering applied to the magnetic yaw innovations with a conventional lowpass filter. This prevents mag heading innovation transients caused by preflight handling from failing the check, but catches persistent errors. Sign swapping of innovations due to angle wrapping is not a problem due to the way that innovations are calculated inside the EKF, so a simple LPF sufficient.
2018-06-29 16:36:38 +00:00
6ff9fd2209
calibration: remove warning message
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The calibration warning was only used in the ESC calibration and in all
cases it actually meant that the calibration failed. In order to keep
the API as small as possible, I've deprecated the warning string and
converted the warning messages to failed messages.
2018-06-29 16:07:32 +00:00
02116c0a80
mavlink: Indicate if the instance did not start correctly ( #9744 )
2018-06-29 10:11:27 -04:00
8551d2eb9d
mission feasibility: add small tolerance to fw landing slope alt
2018-06-29 12:10:53 +00:00
d3c169b1e0
Fix whitespaces in PreflightCheck.cpp, tilt_quad.aux.mix, and tilt_quad.main.mix
2018-06-28 20:20:32 -04:00
96f47d4772
EKF2 add perf counters ( #9795 )
2018-06-28 17:28:03 -04:00
6a06417096
rpi_rc_in: replace chinese comments with english ones
2018-06-28 15:33:24 +02:00
bb8e653469
mc_att_control: keep integral enabled based on land detector
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Previously the rate controller disabled updating the integral below 20%
throttle. This is not ideal for several reasons:
- some racers already hover with 20% throttle.
- for acro it is important to always keep the integral enabled, it has a
noticeable effect on flight performance.
2018-06-27 09:11:23 +00:00
bf1c11a33c
commander: move comment to the right place
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It's now the same way as in the ARM logic further down.
2018-06-27 10:41:21 +02:00
02fc68a53e
commander arming: disable stick (dis-)arming when arming switch/button is used
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A reason for using switch arming in the first place is that you cannot
accidentally disarm in-air with the sticks during acrobatic flights.
It also adds a low-throttle arming requirement for switch arming.
2018-06-27 10:41:21 +02:00
db2b010630
commander arming: add a grace period of 5 seconds to allow re-arming w/o preflight checks
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This changes the arming logic such that the preflight checks don't need
to be satisfied if arming happens < 5 seconds after the last disarming.
This allows to recover from accidental in-air disarming.
2018-06-27 10:41:21 +02:00
8c3cf0167c
commander arming_state_transition: respect fRunPreArmChecks properly
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if fRunPreArmChecks was set to false, there were still cases where the
preflight checks could be called. This fixes that.
arming_state_transition() with fRunPreArmChecks=false is only called
when entering & leaving preflight calibration mode.
All other places use fRunPreArmChecks=true, which means there is no change
for these.
2018-06-27 10:41:21 +02:00
469b5f98e2
commander Preflight::preflightCheck: transition condition_system_sensors_initialized only to true
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- this matches the logic in arming_state_transition()
- if Commander::preflight_check was run in armed state and the checks
failed, disarming was not possible anymore
(because disarming checks for condition_system_sensors_initialized).
That is currently not the case, but the existing logic is way too fragile.
Alternative solution: check if armed in Preflight::preflightCheck, and
only transition to false if disarmed (but also respect the re-arming
grace period).
2018-06-27 10:41:21 +02:00
9eae8e7c5b
Update submodule libuavcan to latest Wed Jun 27 01:27:03 UTC 2018 ( #9779 )
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- libuavcan in PX4/Firmware (fab974fde713b9de0ece1b85239d9dc52622052e): https://github.com/UAVCAN/libuavcan/commit/231b221b64265db4e98f86e53721316f9e17e143
- libuavcan current upstream: https://github.com/UAVCAN/libuavcan/commit/dfcdf22eda16ff06847976fd6c7f40671fc92eb5
- Changes: https://github.com/UAVCAN/libuavcan/compare/231b221b64265db4e98f86e53721316f9e17e143...dfcdf22eda16ff06847976fd6c7f40671fc92eb5
dfcdf22#142 from thirtytwobits/feature/issue141
529a376#141 Add Vagrantfile to automate dev environment
2018-06-27 00:09:19 -04:00
0ac1ef12c7
gpssim: unadvertise gps topics
2018-06-26 15:51:17 +02:00
ddde968a6f
mavlink: allow resetting streams to their default via 'mavlink stream' command
2018-06-25 12:19:56 +02:00
ec15fc333b
mavlink: add 'mavlink status streams' command
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Displays all enabled streams and their configured rates.
Example output:
instance #1 :
Name Rate Config (current) [Hz] Message Size (if active) [B]
HEARTBEAT 1.00 (1.000) 21
STATUSTEXT 20.00 (6.320)
COMMAND_LONG unlimited
ALTITUDE 1.00 (0.316)
ATTITUDE 25.00 (7.900) 40
ATTITUDE_TARGET 10.00 (3.160) 49
ESTIMATOR_STATUS 1.00 (0.316) 44
EXTENDED_SYS_STATE 1.00 (0.316) 14
GLOBAL_POSITION_INT 10.00 (3.160) 40
GPS_RAW_INT 1.00 (0.316) 62
HOME_POSITION 0.50 (0.158)
RC_CHANNELS 5.00 (1.580)
SERVO_OUTPUT_RAW_0 1.00 (0.316) 49
SYS_STATUS 5.00 (1.580) 43
SYSTEM_TIME 1.00 (0.316) 24
VFR_HUD 25.00 (7.900) 32
WIND_COV 2.00 (0.632)
2018-06-25 12:19:56 +02:00
84841236cb
mavlink: allow resetting mavlink streams to default via MAV_CMD_SET_MESSAGE_INTERVAL
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This implementation does not need more resources.
It's not super efficient in terms of runtime, but it's also not something
that is called often.
2018-06-25 12:19:56 +02:00
333fd9cf45
mavlink: improve status output
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- add datarate
- add UDP remote port
- add partner IP
2018-06-25 12:19:56 +02:00
f59412ba65
mavlink: only enable HIL_ACTUATOR_CONTROLS in hil if link has enough bandwidth
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Plus correct return value.
Iridium links are below that.
2018-06-25 12:19:56 +02:00
4553992760
mavlink: refactor get_client_source_address() to return a reference instead of a pointer
2018-06-25 12:19:56 +02:00
aa270fcd89
Mission feasibility: remove 2/3rds distance warnings that don't reject a mission ( #9743 )
2018-06-23 10:39:23 -04:00
d21cf7123e
version library add ECL
2018-06-22 08:46:30 +02:00
325fe16178
airspeed drivers: add PX4_I2C_BUS_ONBOARD as possible bus
2018-06-21 07:37:53 +02:00
035f240e76
ets_airspeed: add -a flag to scan all i2c busses during start
2018-06-21 07:37:53 +02:00
670c3cbf4e
sdp3x_airspeed: add -a flag to scan all i2c busses during start
2018-06-21 07:37:53 +02:00
fd675084cc
ms5525_airspeed: add -a flag to scan all i2c busses during start
2018-06-21 07:37:53 +02:00
cf816fe556
ms4525_airspeed: remove i2c_bus parameter from start function (it tries all busses)
2018-06-21 07:37:53 +02:00
5f3ea2f7ba
ms4525_airspeed: change start_bus from bool to int
2018-06-21 07:37:53 +02:00
c231b6834d
ms4525_airspeed: remove PX4_I2C_ALL
2018-06-21 07:37:53 +02:00
fa35731e02
ms4525_airspeed: add -a flag to scan all i2c busses during start
2018-06-21 07:37:53 +02:00
7a82c777b2
LandDetector FW: Fix param min/max values and descriptions as well as some variable names which were wrong/outdated ( #9708 )
2018-06-20 16:13:33 -04:00
Lorenz Meier