forked from Archive/PX4-Autopilot
EKF2: increase default of EKF2_WIND_NSD and EKF2_TAS_GATE
Increasing the wind process noise results in a more dynamic wind estimation, which is capable of catching fast-varying winds. As wind is used in the lateral guidance it's important that we don't filter it too much. Furher the gate of the airspeed fusion is increased, to reduce the likelihood of airspeed fusion stopping due to dynamic wind conditions. The airspeed is validated in the airspeed validator (EKF consumes the validated one). Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
This commit is contained in:
parent
ec20f92558
commit
0a271b1982
|
@ -342,7 +342,7 @@ PARAM_DEFINE_FLOAT(EKF2_MAG_E_NOISE, 1.0e-3f);
|
|||
* @unit m/s^2/sqrt(Hz)
|
||||
* @decimal 3
|
||||
*/
|
||||
PARAM_DEFINE_FLOAT(EKF2_WIND_NSD, 1.0e-2f);
|
||||
PARAM_DEFINE_FLOAT(EKF2_WIND_NSD, 5.0e-2f);
|
||||
|
||||
/**
|
||||
* Measurement noise for gps horizontal velocity.
|
||||
|
@ -601,7 +601,7 @@ PARAM_DEFINE_FLOAT(EKF2_GPS_V_GATE, 5.0f);
|
|||
* @unit SD
|
||||
* @decimal 1
|
||||
*/
|
||||
PARAM_DEFINE_FLOAT(EKF2_TAS_GATE, 3.0f);
|
||||
PARAM_DEFINE_FLOAT(EKF2_TAS_GATE, 5.0f);
|
||||
|
||||
/**
|
||||
* Will be removed after v1.14 release
|
||||
|
|
Loading…
Reference in New Issue