I could not extract the open_drone_id helpers to a separate lib because
it would require the mavlink headers while the mavlink library would
also depend on it, so it ended up being a circular dependency.
Instead, I'm now just using the headers from within the mavlink module
as well as from the uavcan driver.
This extracts the function mapping from MAV_TYPE to MAV_ODID_UA_TYPE to
the library, so that it can be re-used later by the remote ID
implementation over DroneCAN.
Signed-off-by: Julian Oes <julian@oes.ch>
- default to v0.0.0 if tag isn't available
- src/lib/px_update_git_header.py use same PX4_GIT_TAG as cmake
- update lingering master branch references to main
* lib: add FilteredDerivative class
* AirspeedValidator: add first principle check
- filters throttle, pitch and airspeed rate, and triggers
if the airspeed rate is negative even though the vehicle
is pitching down and giving high throttle.
Check has to fail for duration defined by ASPD_FP_T_WINDOW
to trigger an airspeed failure.
* AirspeedValidator: define constants for first principle check
* FilteredDerivative: set initialised to false if sample interval is invalid
* airspeed_selector: improved comment
* increase IAS derivative filter time constant from 4 to 5
* use legacy parameter handling for FW_PSP_OFF
* handle FW_THR_MAX as well
* ROMFS/airframes: exclude some airframes for v6x and v4pro to save flash on them
---------
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
Signed-off-by: RomanBapst <bapstroman@gmail.com>
Co-authored-by: Silvan Fuhrer <silvan@auterion.com>
Pulls cell count, min voltage and max voltage from log file but still allows for over-rides. Also added debug info to tell user what what it found in the log and what it is using
Co-authored-by: chfriedrich98 <125505139+chfriedrich98@users.noreply.github.com>
- MPC_VEL_LP: new velocity first order low pass filter (off by default)
- MPC_VEL_NF_FRQ/MPC_VEL_NF_BW: new velocity notch filter (off by default)
- MPC_VELD_LP: existing velocity derivative low pass filter, but I've dropped the remaining controllib usage
The case where the airframe maintainer wants to enforce a reset to airframe is
not covered anymore with the `param set-default` mechanism. For products based
on PX4 this is still required to ensure proper functionality after a major update.
VTOLs consume a lot more power in hover copared to fixed-wing fligt.
The remaining flight time thus should reset if one switches from MC to FW,
as otherwise it takes several minutes until the estimate goes down.
- upate to NOAA grid API to build WMM table in one pass
- refactor declination/inclination/totalintensity table printing to
shared method
- compute scaling factor to maximize resolution
