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| author | Darryl Taylor <darryl.c.taylor@gmail.com> | 2014-06-18 20:49:48 +0800 |
|---|---|---|
| committer | Darryl Taylor <darryl.c.taylor@gmail.com> | 2014-06-18 20:49:48 +0800 |
| commit | 95003c6e1061b61dce6ed86e6c68d662e39a222d (patch) | |
| tree | 2864c1fe98cb25a431dec69568bb766800a53571 /src/modules/attitude_estimator_ekf/attitude_estimator_ekf_params.c | |
| parent | 90a89ff2cdbb5268f4b8bee64b8da24db508f5a7 (diff) | |
| download | px4-firmware-95003c6e1061b61dce6ed86e6c68d662e39a222d.tar.gz px4-firmware-95003c6e1061b61dce6ed86e6c68d662e39a222d.tar.bz2 px4-firmware-95003c6e1061b61dce6ed86e6c68d662e39a222d.zip | |
Removed unused ATT_XXX_OFF3 paramters. Offset tuning now accomplished via the sensors app using new SENS_BOARD_XXX_OFF parameters.
Diffstat (limited to 'src/modules/attitude_estimator_ekf/attitude_estimator_ekf_params.c')
| -rwxr-xr-x | src/modules/attitude_estimator_ekf/attitude_estimator_ekf_params.c | 13 |
1 files changed, 0 insertions, 13 deletions
diff --git a/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_params.c b/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_params.c index 3ff3d9922..49a892609 100755 --- a/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_params.c +++ b/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_params.c @@ -61,11 +61,6 @@ PARAM_DEFINE_FLOAT(EKF_ATT_V4_R2, 100.0f); /* offset estimation - UNUSED */ PARAM_DEFINE_FLOAT(EKF_ATT_V4_R3, 0.0f); -/* offsets in roll, pitch and yaw of sensor plane and body */ -PARAM_DEFINE_FLOAT(ATT_ROLL_OFF3, 0.0f); -PARAM_DEFINE_FLOAT(ATT_PITCH_OFF3, 0.0f); -PARAM_DEFINE_FLOAT(ATT_YAW_OFF3, 0.0f); - /* magnetic declination, in degrees */ PARAM_DEFINE_FLOAT(ATT_MAG_DECL, 0.0f); @@ -85,10 +80,6 @@ int parameters_init(struct attitude_estimator_ekf_param_handles *h) h->r2 = param_find("EKF_ATT_V4_R2"); h->r3 = param_find("EKF_ATT_V4_R3"); - h->roll_off = param_find("ATT_ROLL_OFF3"); - h->pitch_off = param_find("ATT_PITCH_OFF3"); - h->yaw_off = param_find("ATT_YAW_OFF3"); - h->mag_decl = param_find("ATT_MAG_DECL"); h->acc_comp = param_find("ATT_ACC_COMP"); @@ -109,10 +100,6 @@ int parameters_update(const struct attitude_estimator_ekf_param_handles *h, stru param_get(h->r2, &(p->r[2])); param_get(h->r3, &(p->r[3])); - param_get(h->roll_off, &(p->roll_off)); - param_get(h->pitch_off, &(p->pitch_off)); - param_get(h->yaw_off, &(p->yaw_off)); - param_get(h->mag_decl, &(p->mag_decl)); p->mag_decl *= M_PI / 180.0f; |