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| author | Don Gagne <don@thegagnes.com> | 2015-04-15 11:29:37 -0700 |
|---|---|---|
| committer | Don Gagne <don@thegagnes.com> | 2015-04-15 11:29:37 -0700 |
| commit | 05c351183f0425f1c4feba60bf68b28d73eee51f (patch) | |
| tree | cedf4dde1f5b5a41fd26e7c060a4ce7d74cb8cd1 /src/modules/attitude_estimator_ekf/attitude_estimator_ekf_params.c | |
| parent | d84ac41cd355f6c907e0a6e71a1ee12536bfb95e (diff) | |
| download | px4-firmware-05c351183f0425f1c4feba60bf68b28d73eee51f.tar.gz px4-firmware-05c351183f0425f1c4feba60bf68b28d73eee51f.tar.bz2 px4-firmware-05c351183f0425f1c4feba60bf68b28d73eee51f.zip | |
Parameter meta data fixes
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 | 22 |
1 files changed, 11 insertions, 11 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 e143f37b9..fe480e12b 100755 --- a/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_params.c +++ b/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_params.c @@ -48,49 +48,49 @@ /** * Body angular rate process noise * - * @group attitude_ekf + * @group Attitude EKF estimator */ PARAM_DEFINE_FLOAT(EKF_ATT_V3_Q0, 1e-4f); /** * Body angular acceleration process noise * - * @group attitude_ekf + * @group Attitude EKF estimator */ PARAM_DEFINE_FLOAT(EKF_ATT_V3_Q1, 0.08f); /** * Acceleration process noise * - * @group attitude_ekf + * @group Attitude EKF estimator */ PARAM_DEFINE_FLOAT(EKF_ATT_V3_Q2, 0.009f); /** * Magnet field vector process noise * - * @group attitude_ekf + * @group Attitude EKF estimator */ PARAM_DEFINE_FLOAT(EKF_ATT_V3_Q3, 0.005f); /** * Gyro measurement noise * - * @group attitude_ekf + * @group Attitude EKF estimator */ PARAM_DEFINE_FLOAT(EKF_ATT_V4_R0, 0.0008f); /** * Accel measurement noise * - * @group attitude_ekf + * @group Attitude EKF estimator */ PARAM_DEFINE_FLOAT(EKF_ATT_V4_R1, 10000.0f); /** * Mag measurement noise * - * @group attitude_ekf + * @group Attitude EKF estimator */ PARAM_DEFINE_FLOAT(EKF_ATT_V4_R2, 100.0f); @@ -102,7 +102,7 @@ PARAM_DEFINE_INT32(ATT_ACC_COMP, 2); /** * Moment of inertia matrix diagonal entry (1, 1) * - * @group attitude_ekf + * @group Attitude EKF estimator * @unit kg*m^2 */ PARAM_DEFINE_FLOAT(ATT_J11, 0.0018); @@ -110,7 +110,7 @@ PARAM_DEFINE_FLOAT(ATT_J11, 0.0018); /** * Moment of inertia matrix diagonal entry (2, 2) * - * @group attitude_ekf + * @group Attitude EKF estimator * @unit kg*m^2 */ PARAM_DEFINE_FLOAT(ATT_J22, 0.0018); @@ -118,7 +118,7 @@ PARAM_DEFINE_FLOAT(ATT_J22, 0.0018); /** * Moment of inertia matrix diagonal entry (3, 3) * - * @group attitude_ekf + * @group Attitude EKF estimator * @unit kg*m^2 */ PARAM_DEFINE_FLOAT(ATT_J33, 0.0037); @@ -128,7 +128,7 @@ PARAM_DEFINE_FLOAT(ATT_J33, 0.0037); * * If set to != 0 the moment of inertia will be used in the estimator * - * @group attitude_ekf + * @group Attitude EKF estimator * @min 0 * @max 1 */ |