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https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-10-16 17:13:33 +08:00
Attitude EKF: Remove param file
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@@ -40,7 +40,6 @@ px4_add_module(
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SRCS
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attitude_estimator_ekf_main.cpp
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attitude_estimator_ekf_params.c
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codegen/AttitudeEKF.c
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DEPENDS
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platforms__common
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@@ -108,6 +108,46 @@ usage(const char *reason)
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fprintf(stderr, "usage: attitude_estimator_ekf {start|stop|status} [-p <additional params>]\n\n");
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}
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int parameters_init(struct attitude_estimator_ekf_param_handles *h)
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{
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/* PID parameters */
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h->q0 = param_find("EKF_ATT_V3_Q0");
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h->q1 = param_find("EKF_ATT_V3_Q1");
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h->q2 = param_find("EKF_ATT_V3_Q2");
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h->q3 = param_find("EKF_ATT_V3_Q3");
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h->r0 = param_find("EKF_ATT_V4_R0");
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h->r1 = param_find("EKF_ATT_V4_R1");
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h->r2 = param_find("EKF_ATT_V4_R2");
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h->moment_inertia_J[0] = param_find("ATT_J11");
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h->moment_inertia_J[1] = param_find("ATT_J22");
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h->moment_inertia_J[2] = param_find("ATT_J33");
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h->use_moment_inertia = param_find("ATT_J_EN");
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return OK;
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}
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int parameters_update(const struct attitude_estimator_ekf_param_handles *h, struct attitude_estimator_ekf_params *p)
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{
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param_get(h->q0, &(p->q[0]));
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param_get(h->q1, &(p->q[1]));
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param_get(h->q2, &(p->q[2]));
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param_get(h->q3, &(p->q[3]));
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param_get(h->r0, &(p->r[0]));
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param_get(h->r1, &(p->r[1]));
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param_get(h->r2, &(p->r[2]));
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for (int i = 0; i < 3; i++) {
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param_get(h->moment_inertia_J[i], &(p->moment_inertia_J[3 * i + i]));
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}
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param_get(h->use_moment_inertia, &(p->use_moment_inertia));
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return OK;
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}
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/**
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* The attitude_estimator_ekf app only briefly exists to start
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* the background job. The stack size assigned in the
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@@ -129,43 +129,3 @@ PARAM_DEFINE_FLOAT(ATT_J33, 0.0037);
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* @max 1
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*/
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PARAM_DEFINE_INT32(ATT_J_EN, 0);
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int parameters_init(struct attitude_estimator_ekf_param_handles *h)
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{
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/* PID parameters */
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h->q0 = param_find("EKF_ATT_V3_Q0");
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h->q1 = param_find("EKF_ATT_V3_Q1");
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h->q2 = param_find("EKF_ATT_V3_Q2");
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h->q3 = param_find("EKF_ATT_V3_Q3");
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h->r0 = param_find("EKF_ATT_V4_R0");
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h->r1 = param_find("EKF_ATT_V4_R1");
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h->r2 = param_find("EKF_ATT_V4_R2");
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h->moment_inertia_J[0] = param_find("ATT_J11");
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h->moment_inertia_J[1] = param_find("ATT_J22");
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h->moment_inertia_J[2] = param_find("ATT_J33");
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h->use_moment_inertia = param_find("ATT_J_EN");
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return OK;
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}
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int parameters_update(const struct attitude_estimator_ekf_param_handles *h, struct attitude_estimator_ekf_params *p)
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{
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param_get(h->q0, &(p->q[0]));
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param_get(h->q1, &(p->q[1]));
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param_get(h->q2, &(p->q[2]));
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param_get(h->q3, &(p->q[3]));
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param_get(h->r0, &(p->r[0]));
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param_get(h->r1, &(p->r[1]));
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param_get(h->r2, &(p->r[2]));
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for (int i = 0; i < 3; i++) {
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param_get(h->moment_inertia_J[i], &(p->moment_inertia_J[3 * i + i]));
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}
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param_get(h->use_moment_inertia, &(p->use_moment_inertia));
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return OK;
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}
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