24596 Commits

Author SHA1 Message Date
Daniel Agar
aa2566970e FW landing abort remove message comma (read as a pause) 2017-10-06 20:11:19 +02:00
Beat Küng
efb170d91d tap_esc: some cleanup
- use select_responder from tap_esc_common namespace (same definition)
- switch pwm output to uint16, that's what's used in send_esc_output()
- use SCHED_PRIORITY_ACTUATOR_OUTPUTS instead of SCHED_PRIORITY_MAX
2017-10-06 19:32:53 +02:00
Daniel Agar
38f45d1a9d airspeed sensor startup improvements (#7903) 2017-10-05 14:29:44 -07:00
Daniel Agar
123a0b584a cmake fix posix upload targets 2017-10-05 11:28:10 -10:00
Daniel Agar
87a1b15509 NuttX build restore old .px4 file naming (drop nuttx_ prefix) 2017-10-05 11:28:10 -10:00
Daniel Agar
8d07c647f7 NuttX improve apps builtins dependencies 2017-10-05 11:28:10 -10:00
davidaroyer
ed9e798f86 docker_run.sh: add ocpoc target 2017-10-05 09:34:14 -07:00
davidaroyer
89f8956ae3 boards: update ocpoc board_config defines 2017-10-05 09:34:14 -07:00
Paul Riseborough
0def4ace5f commander: check magnetometers for inconsistency preflight 2017-10-05 09:30:26 -07:00
Paul Riseborough
60a68d30c7 sensors: Calculate and publish magnetometer inconsistency 2017-10-05 09:30:26 -07:00
Paul Riseborough
c7097085fa msg: publish magnetometer inconsistency level 2017-10-05 09:30:26 -07:00
Beat Küng
20e987faa9 estimator_status: add missing descriptions for control_mode_flags 2017-10-05 10:04:02 +02:00
ChristophTobler
8541555e13 gpssim: add possibility to change parameters
fix_type, satellites_used and a noise parameter can now be set manually for testing purposes
2017-10-05 07:18:20 +02:00
ChristophTobler
b41c471090 accelsim/gyrosim: fix seg fault if not enough arguments
happens with 'accelsim/gyrosim -R'
2017-10-05 07:18:20 +02:00
ChristophTobler
6843155357 gpssim: fix seg fault if not enough arguments
happens with e.g. 'gpssim -f'
2017-10-05 07:18:20 +02:00
ChristophTobler
2436a27848 gpssim: use px4_getopt 2017-10-05 07:18:20 +02:00
David Sidrane
bed4714cfe kinetis:adc fix typo vailid->valid (#8054)
Fix typo on master
2017-10-04 08:05:18 -10:00
David Sidrane
86389930be drv_sensor:Part number changed to fxos8701cq 2017-10-04 04:49:35 -10:00
David Sidrane
b363b794b1 fxos8700cq:Part number change fxos8701cq 2017-10-04 04:49:35 -10:00
David Sidrane
390f93724c nxphlite-v3:Fixed USB PRODUCTSTR. CONFIG_CDCACM_PRODUCTID Still needs update 2017-10-04 04:49:35 -10:00
David Sidrane
e1496a6d57 kinetis:io_timer Added SYC on CCR setting
Fixes error in fmu test "servo 0 readback error, got 900
                          expected 1002"
2017-10-04 04:49:35 -10:00
David Sidrane
10f418a272 nxphlite-v3:rcS move mavlink to UART4 connector P10 2017-10-04 04:49:35 -10:00
David Sidrane
b6c15d7223 nxphlite-v3:Manage Spektrum power & bind 2017-10-04 04:49:35 -10:00
David Sidrane
e11b08aa68 nxphlite-v3:ADC 12 use bit 2017-10-04 04:49:35 -10:00
David Sidrane
3e863dff5d nxphlite-v3:ADC digital USB connected 2017-10-04 04:49:35 -10:00
David Sidrane
7a0254d9f3 nxphlite-v3:Use BOARD_HAS_CONTROL_STATUS_LEDS 2017-10-04 04:49:35 -10:00
David Sidrane
1615d5642e kinetis:drv_io_timer ensure the Mod register is updated 2017-10-04 04:49:35 -10:00
David Sidrane
ccc83dde33 nxphlite-v3:Build rgbled_pwm driver 2017-10-04 04:49:35 -10:00
David Sidrane
99dc1b17e2 nxphlite-v3:Add PWM RGB LEDs 2017-10-04 04:49:35 -10:00
David Sidrane
36d4619045 nxphlite-v3:Define RGB LED timer assignments 2017-10-04 04:49:35 -10:00
David Sidrane
9c7fd0ab9c nxphlite-v3:Use LED D9 and D10, remove RGB LEDs (going to PWM) 2017-10-04 04:49:35 -10:00
David Sidrane
f68da76701 kinetis:PWM LED driver 2017-10-04 04:49:35 -10:00
David Sidrane
e11af2bc27 fmu:Add PWM6 mode for nxphlite v3.5 2017-10-04 04:49:35 -10:00
David Sidrane
2eaf0c8c0a fxos8700cq:Drop SCLK to 1 Mhz 2017-10-04 04:49:35 -10:00
David Sidrane
b9c13b86cb nxphlite-v3:Refreshed Config 2017-10-04 04:49:35 -10:00
David Sidrane
812128d565 nxphlite-v3:V3.5 HW changes 2017-10-04 04:49:35 -10:00
David Sidrane
9ce3fc6700 nxphlite-v3 cmake:Bring inline with master 2017-10-04 04:49:35 -10:00
Julien Lecoeur
5d01eac5de Fix check_stack target (#8050) 2017-10-04 10:02:23 -04:00
Jonas Vautherin
93c1ad3103 sitl: add possibility to not run gazebo when running make 2017-10-04 15:38:37 +02:00
Beat Küng
dd98ed565e protocol_splitter: fix type comparison 2017-10-04 14:13:14 +02:00
ChristophTobler
ec61ae0003 ekf2: add some comments 2017-10-04 13:11:11 +02:00
Beat Küng
8016d69ba4 mavlink_log_handler: set current_log_filep to NULL after closing the file
It probably did not cause further issues, except that fclose() was called
on an invalid file handle later on.
2017-10-04 07:33:47 +02:00
José Roberto de Souza
c47e541d02 AeroFC: Disable UART8 (#8046)
* AeroFC: Update defconfig

defconfig generated using: make aerofc-v1_default oldconfig

* AeroFC: Disable UART8

It is not used but it share the same pinout in the FC connector with
other pin used as I2C2, so it needs to stay in high-z.
2017-10-03 18:14:50 -10:00
Beat Küng
2dd34d639d commander: ignore internal commands during calibration
if vmount was enabled in mavlink mode, it was continuously sending mavlink
commmands, which lead to 'command denied during calibration: 205' messages
during calibration.
2017-10-03 07:50:27 +02:00
Beat Küng
29e85edac8 Revert "param MPC_MAN_TILT_MAX: decrease maximum from 90 to 85 degrees"
This reverts commit d6df692b7a69460642f1efaad967538f8b6ef1c2.

The changes to attitude controller improve this a lot.
2017-10-01 15:36:21 +02:00
Beat Küng
98893c9f4f mc_att_control params: increase max roll/pitch/yaw rates to 1800
If you want to go to the limit of what the vehicle can do, you need to be
able to set it so large that it is guaranteed that it's never limited by
software.

Tests showed that it's not a problem to increase it to very high numbers.
2017-10-01 15:36:21 +02:00
Beat Küng
f5d9155ab2 mc_att_control params: reduce default max acro rates from 360 to 120 deg/s
360 is too fast if you just want to hover. Next step is to add expo(),
so that we still have fine-grained control at the center and high rates
at the edges.
2017-10-01 15:36:21 +02:00
Beat Küng
55da07d3c4 mc_att_control: fix computation of yaw weight for attitude control
Previously, the yaw weight was based on the tilt angle of the attitude
setpoint (R_sp(2, 2) == cos(tilt angle)). This makes no sense, it means
the weight is low for high tilt angles even if there is no roll-pitch error
at all.

This patch changes the weight computation to be based on the tilt angle
error: the yaw weight is 1 if there is no roll-pitch error (independent
from current tilt angle), and is reduced for higher tilt angle errors.

The weight was added in 05e9a30573f50dd271f10, without any explanation or
derivation of how and why the weight is chosen that way.

However this patch works much better in practice. The yaw control is
improved, though it can be a bit slow to converge if you do continuous &
fast roll-pitch motions (which is expected).
2017-10-01 15:36:21 +02:00
Beat Küng
2f1ca409b7 mc_att_control: add more comments to the code, better explaining what it does
No semantic changes.
2017-10-01 15:36:21 +02:00
Beat Küng
69b1bfca6c mc_att_control: fix yaw feedforwarding
The feedforwarding was applied in the wrong frame: the term is given in
global coordinates, but was directly applied to body coordinates. This
patch adds the missing transformation from global to body frame.

In addition, it moves the feedforwarding before the rate limitation, so
that we cannot exceed the configured rates.
2017-10-01 15:36:21 +02:00