Lines Matching defs:accel
47 //int accuracy_accel; /**< Accel Accuracy */
81 long accel[3];
82 inv_get_accel_set(accel, accuracy, timestamp);
83 values[0] = accel[0] * ACCEL_CONVERSION;
84 values[1] = accel[1] * ACCEL_CONVERSION;
85 values[2] = accel[2] * ACCEL_CONVERSION;
90 MPL_LOGV("accel values:%f %f %f -%d -%lld", values[0], values[1],
97 * accel biases while at rest.
106 long gravity[3], accel[3];
109 inv_get_accel_set(accel, accuracy, timestamp);
111 accel[0] -= gravity[0] >> 14;
112 accel[1] -= gravity[1] >> 14;
113 accel[2] -= gravity[2] >> 14;
114 values[0] = accel[0] * ACCEL_CONVERSION;
115 values[1] = accel[1] * ACCEL_CONVERSION;
116 values[2] = accel[2] * ACCEL_CONVERSION;
257 long accel[3], quat_6_axis[4];
258 inv_get_accel_set(accel, accuracy, timestamp);
506 long accel[3];
507 inv_get_accel_set(accel, accuracy, timestamp);
544 hal_out.accel_status = sensor_cal->accel.status;
555 if ((sensor_cal->accel.status & INV_SENSOR_ON) && (sr > sensor_cal->accel.sample_rate_ms)) {
556 sr = sensor_cal->accel.sample_rate_ms;
571 if ((sensor_cal->accel.status & sensor_cal->compass.status & INV_SENSOR_ON) == 0) {
575 if ((sensor_cal->gyro.status & sensor_cal->accel.status & sensor_cal->compass.status & INV_SENSOR_ON) == 0) {
588 hal_out.nine_axis_status = (sensor_cal->accel.status & INV_NEW_DATA) ? 1 : 0;
589 hal_out.nav_timestamp = sensor_cal->accel.timestamp;
