|
|
|
@ -95,19 +95,6 @@ PARAM_DEFINE_FLOAT(EKF_ATT_V4_R1, 10000.0f);
@@ -95,19 +95,6 @@ PARAM_DEFINE_FLOAT(EKF_ATT_V4_R1, 10000.0f);
|
|
|
|
|
*/ |
|
|
|
|
PARAM_DEFINE_FLOAT(EKF_ATT_V4_R2, 100.0f); |
|
|
|
|
|
|
|
|
|
/**
|
|
|
|
|
* EKF attitude estimator enabled |
|
|
|
|
* |
|
|
|
|
* If enabled, it uses the older EKF filter. |
|
|
|
|
* However users can enable the new quaternion |
|
|
|
|
* based complimentary filter by setting EKF_ATT_ENABLED = 0. |
|
|
|
|
* |
|
|
|
|
* @min 0 |
|
|
|
|
* @max 1 |
|
|
|
|
* @group Attitude EKF estimator |
|
|
|
|
*/ |
|
|
|
|
PARAM_DEFINE_INT32(EKF_ATT_ENABLED, 1); |
|
|
|
|
|
|
|
|
|
/**
|
|
|
|
|
* Moment of inertia matrix diagonal entry (1, 1) |
|
|
|
|
* |
|
|
|
|