96a0594078
rc_loss_alarm: formatting
2018-07-05 14:17:55 +02:00
0f2c710237
rc_loss_alarm: hiding all but default constructor
2018-07-05 14:17:55 +02:00
d2b9197587
rc_loss_alarm: sorting function definitions
2018-07-05 14:17:55 +02:00
c8ff5f09d4
rc_loss_alarm: Added some custom commands
2018-07-05 14:17:55 +02:00
c0db004294
rc_loss_alarm: Added basic functionality
2018-07-05 14:17:55 +02:00
278e4cef84
uORB fix ORB_COMMUNICATOR defined sections
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- keep portions of internal add/remove helpers
2018-07-05 07:03:27 +00:00
05fc506a56
[df_ms5607_wrapper] convert to mbar, fix error_count, device_id
2018-07-05 08:07:54 +02:00
5cb6753572
i2c.h: include board_config
2018-07-03 17:33:18 +02:00
84f937a098
airspeed sensor: use bus_option array from i2c.h instead of one in each driver
2018-07-03 17:33:18 +02:00
6cb17839ee
distance sensors: remove bus_option array and add it to i2c.h header
2018-07-03 17:33:18 +02:00
c13d69a610
distance sensor drivers: change all open and close to px4_open and px4_close
2018-07-03 17:33:18 +02:00
8f4e9228bf
mb12xx driver: add -b and -a flags to choose i2c busses and remove nuttx stuff such as exit functions
2018-07-03 17:33:18 +02:00
fed6c9ae34
srf02 driver: add -b and -a flags to choose i2c busses and remove nuttx stuff such as exit functions
2018-07-03 17:33:18 +02:00
5b259a008a
vl53lxx driver: add -b, -a and -R flags to choose i2c busses and sensor rotation and remove nuttx stuff such as exit functions
2018-07-03 17:33:18 +02:00
040662ff04
sf1xx driver: add -b and -a flags to choose i2c busses and remove nuttx stuff such as exit functions
2018-07-03 17:33:18 +02:00
7d281b2619
teraranger driver: add -b and -a flags to choose i2c busses and remove nuttx stuff such as exit functions
2018-07-03 17:33:18 +02:00
9d1fa8cee2
esc_calibration: adjust timeout when waiting for user to connect battery
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to 20 seconds
Signed-off-by: Roman <bapstroman@gmail.com >
2018-07-03 07:05:38 +00:00
5d87eed41c
esc_calibration: use hrt_elapsed_time instead of manually calculating the diff
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Signed-off-by: Roman <bapstroman@gmail.com >
2018-07-03 07:05:38 +00:00
73577df994
esc_calibration: use batter status connected flag instead of checking voltage
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Signed-off-by: Roman <bapstroman@gmail.com >
2018-07-03 07:05:38 +00:00
beb8c3e152
esc_calibration: use predefined literals
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Signed-off-by: Roman <bapstroman@gmail.com >
2018-07-03 07:05:38 +00:00
8b629454de
esc_calibration: increase safety and initialise all data
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- do not do calibration if not very sure that battery is not connected
- initialise all structs and variables
Signed-off-by: Roman <bapstroman@gmail.com >
2018-07-03 07:05:38 +00:00
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
Alessandro Simovic