* gnss: update supported baud rates
The Septentrio GNSS driver requires certain baud rates to test all the
supported baud rates of the receiver. Without these changes, certain
"non-standard" ones would print an error to the MAVLink console when the
driver was started through the console.
* platforms: add missing baudrate defines
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Co-authored-by: Thomas Frans <franske2000@gmail.com>
Co-authored-by: Julian Oes <julian@oes.ch>
- the module documentation parser can only resolve defines from the same file
- also it cannot deal with defines embeded in strings
- what board should it add for the general documentation anyways?
As a result of these issues I suggest to stay with the original hardcoded
/fs/microsd for the documentation. It's still the most common path as far as
I can see.
We've come accross a case where a ROS node would consistently take something
over 800 ms until the first arming check request subscription callback was
triggered.
After the first sample, the callback always triggered within the expected
timeframe.
Therefore this patch allows for more time right after registration until
timing out.
* Update Zenoh-pico from 0.7.0 to 1.0.0
* Update the zenoh-pico version to use PX4/dev/1.0.0-px4
* Remove the rostopic and rt/ prefix
* Unlike zenoh-bridge-dds we were using, zenoh-bridge-ros2dds is now adding the rt/ prefix automagically.
Avoid flying into terrain using the distance sensor.
Enable through the parameter NAV_MIN_GND_DIST.
Only active during commanded descents with vz>0 (to prevent climb-aways),
excluding landing and VTOL transitions.
It changes the altitude setpoint in the triplet to maintain the current altitude
and republish the triplet. We also change the mission item altitude used for
acceptance calculations to prevent getting stuck in a loop.
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
battery failures can occur upon arming when the load gets sgnificant.
In that case the safest thing to do is prevent a takeoff before anything
worse happens.
The wind variance can be reset to a value larger than the wind init
variance (e.g.: when the reset occurs when flying close to the N or E
axis). Constraining the variance after a covariance initialization would
artificially increase the correlation and could destabilize the filter.
