- force initialize takeoff airspeed setpoint at start of takeoff modes
- force set airspeed constraints if slewed value is out of bounds
- always slew airspeed setpoints as long as inside constraints
- move target airspeed setpoint calculation into mode specific logic regions (hand vs runway)
when we're in a takeoff situation, we only want to adapt the airspeed to
avoid accelerated stall due to load factor changes. Disable othre logic
like minimum ground speed, wind based adaption and airspeed slew rating.
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
From looking at the history the BMM150 rotation was initially 0. Then,
this was changed to 6 when the intent was to only change it for Skynode.
A bit later, the rotation was changed back to 0, but only for Skynode.
This tells me that rotation 0 was correct for all 6X including Skynode
all along.
Signed-off-by: Julian Oes <julian@oes.ch>
- ekf2 heading first initializes to 0 degrees, then immediately resets to mag heading once a few samples are accumulated
- the yaw standard deviation check could be adjusted to exclude this brief (<1s) initial period
- on NuttX if the SD card was just cleared (quick format) it's possible for the newly created uninitialized dataman file to still have the previous compatibility key, which causes the initialization to be skipped
* added a new driver ASP5033 for measuring the differential pressure and airspeed
---------
Co-authored-by: nano <nanobotzhe@abv.bg>
Co-authored-by: Denislav Petrov <you@example.com>
When the yaw estimate is converging, the controller makes the drone yaw
in order to follow the current setpoint. This is unintuitive for the
pilot and it is preferable if the drone continues to fly towards the
same physical direction.
This estimate doesn't converge to the true yaw but can be used as a
more consistent but drifting heading source.
It can be used by a setpoint generator to adjust its heading setpoint
while the true yaw estimate is converging in order to keep a constant
course over ground.
This updates the gps/devices submodule which includes a fix that
requests the Unicore HEADINGA message in case the message is not enabled
by default.
Signed-off-by: Julian Oes <julian@oes.ch>
If the measured voltage is more than 65v we need to split the voltage
over multiple cells in order to avoid overflowing the uint16. This is
according to the MAVLink spec.
Signed-off-by: Julian Oes <julian@oes.ch>
The extension fields need to be 0 by default according to the MAVLink
spec. This is because extensions are 0 by default and need to be 0 when
unknown/unused for backwards compatibility.
The patch also simplifies the flow slightly in that it doesn't create a
temporary array but just fills in the cell voltages directly.
Signed-off-by: Julian Oes <julian@oes.ch>
Fixes the clang error:
/__w/PX4-Autopilot/PX4-Autopilot/src/drivers/drv_hrt.h:297:35: fatal error: identifier '_s' preceded by whitespace in a literal operator declaration is deprecated [-Wdeprecated-literal-operator]
297 | constexpr hrt_abstime operator "" _s(unsigned long long seconds)
