- this is to prevent vtol_att_control running at absurdly high rates (kilohertz) from every single actuator controls publication from both the multicopter and fixed wing controllers
- I don't really like this solution, but it works for now until there are larger VTOL architectural changes in place
- this lowers the load immediately at boot while still allowing each VehicleIMU instance to properly measure the actual accel/gyro data rates
- for lockstep builds this is ignored and VehicleIMU initially runs with every new sensor_accel/sensor_gyro publication
I changed the input constraint in #15349 but screwed up the usage
because I was convinced it's püass by reference. I'll double check
for sure next time.
- matrix in PX4/Firmware (20d5e7acd6d7be141de802ad155592e7be4c9f77): 9a30828a0a
- matrix current upstream: 0fd99c59f1
- Changes: 9a30828a0a...0fd99c59f1
0fd99c5 2020-07-14 Matthias Grob - Switch operator() to return a const reference
8a59b46 2020-07-17 kamilritz - Quaternion: Use template type instead of single hardcoded type
- vehicle_air_data won't necessary have an update every iteration and these adjusted throttle values aren't stored
- this only would have worked in the past because the vast majority of systems were using the ms5611 barometer with a publication rate that's faster than the controller
This fixes the takeoff and land CI test where we do a takeoff and land
without RC connected.
In my opinion it does not make sense to go into RC lost failsafe if
a datalink is still available.
Of course, this can be dangerous if someone has a companion computer
connected which gets detected as "data link" but actually has no
connection to the ground station.
During takeoff, Navigator is sending a constant yaw value.
However, there is always a reset at 1.5m of the yaw estimate in EKF2
that is not handled by Navigator that produces a glitch in the rate
controller. Given that in FlightTask, the yaw
is already computed and properly corrected in case of an estimator reset
event, we just ignore the yaw value sent by navigator during takeoff.
- increase rate
- cpu load calculation grab timestamp atomically
- only check one task per cycle (but cycle at a higher rate)
- decrease available FD threshold
- minor cleanup
