The situation where this would be desired is unclear, plus it's basically
the same as setting ASPD_SC_P_NOISE to a very small value.
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
Do no longer use tas_innovation from wind estimator and test ratio, but calculate
the innovation based on wind estimate, TAS measurement (including currently applied scale)
and ground velocity. Use innovations directly to trigger failure.
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
As the purpose of this wind estimator is to (mainly) catch airspeed failures,
we don't value estimator stability as much as the reliability to catch
actual sensor issues, and thus do not reset the filter (as this may hide
a real issue with the sensor)
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
- run airspeed scale estimation always, not in dedicated mode
- add option to apply scale automatically, with extra feasibility check
- add airspeed scale for all 3 possible airspeed instances
- clean up parameters
- add check for data stuck (non-changing airspeed data)
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
Daniel Agar