From 63fa17ef0dd4b0a184f6e3e298113bb143b2cb44 Mon Sep 17 00:00:00 2001 From: Thomas Gubler Date: Fri, 25 Jul 2014 15:23:26 +0200 Subject: att ekf: add param to enable/disable J --- .../attitude_estimator_ekf_main.cpp | 2 +- .../attitude_estimator_ekf_params.c | 19 +++++++++++++++---- .../attitude_estimator_ekf_params.h | 2 ++ 3 files changed, 18 insertions(+), 5 deletions(-) diff --git a/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_main.cpp b/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_main.cpp index e1bbf5bc7..667b74d1d 100755 --- a/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_main.cpp +++ b/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_main.cpp @@ -512,7 +512,7 @@ const unsigned int loop_interval_alarm = 6500; // loop interval in microseconds /* Call the estimator */ AttitudeEKF(false, // approx_prediction - false, // use_inertia_matrix + (unsigned char)ekf_params.use_moment_inertia, update_vect, dt, z_k, 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 5b57bfb4d..5c33bc2ac 100755 --- a/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_params.c +++ b/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_params.c @@ -79,7 +79,6 @@ PARAM_DEFINE_FLOAT(ATT_J11, 0.0018); */ PARAM_DEFINE_FLOAT(ATT_J22, 0.0018); - /* * Moment of inertia matrix diagonal entry (3, 3) * @@ -88,6 +87,16 @@ PARAM_DEFINE_FLOAT(ATT_J22, 0.0018); */ PARAM_DEFINE_FLOAT(ATT_J33, 0.0037); +/* + * Moment of inertia enabled in estimator + * + * If set to != 0 the moment of inertia will be used in the estimator + * + * @group attitude_ekf + * @min 0 + * @max 1 + */ +PARAM_DEFINE_INT32(ATT_J_EN, 0); int parameters_init(struct attitude_estimator_ekf_param_handles *h) { @@ -105,9 +114,10 @@ int parameters_init(struct attitude_estimator_ekf_param_handles *h) h->acc_comp = param_find("ATT_ACC_COMP"); - h->moment_inertia_J[0] = param_find("ATT_J11"); - h->moment_inertia_J[1] = param_find("ATT_J22"); - h->moment_inertia_J[2] = param_find("ATT_J33"); + h->moment_inertia_J[0] = param_find("ATT_J11"); + h->moment_inertia_J[1] = param_find("ATT_J22"); + h->moment_inertia_J[2] = param_find("ATT_J33"); + h->use_moment_inertia = param_find("ATT_J_EN"); return OK; } @@ -131,6 +141,7 @@ int parameters_update(const struct attitude_estimator_ekf_param_handles *h, stru for (int i = 0; i < 3; i++) { param_get(h->moment_inertia_J[i], &(p->moment_inertia_J[3 * i + i])); } + param_get(h->use_moment_inertia, &(p->use_moment_inertia)); return OK; } diff --git a/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_params.h b/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_params.h index fbb6a18ff..5d3b6b244 100755 --- a/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_params.h +++ b/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_params.h @@ -45,6 +45,7 @@ struct attitude_estimator_ekf_params { float r[3]; float q[4]; float moment_inertia_J[9]; + int32_t use_moment_inertia; float roll_off; float pitch_off; float yaw_off; @@ -56,6 +57,7 @@ struct attitude_estimator_ekf_param_handles { param_t r0, r1, r2; param_t q0, q1, q2, q3; param_t moment_inertia_J[3]; /**< diagonal entries of the matrix */ + param_t use_moment_inertia; param_t mag_decl; param_t acc_comp; }; -- cgit v1.2.3