Probe and configure the sensor when present; log and continue boot if init fails so boards without BMA456 still run normally. Co-authored-by: Cursor <cursoragent@cursor.com>
163 lines
5.8 KiB
C
163 lines
5.8 KiB
C
/**\
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* Copyright (c) 2022 Bosch Sensortec GmbH. All rights reserved.
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*
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* SPDX-License-Identifier: BSD-3-Clause
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**/
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#include <stdio.h>
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#include "bma456h.h"
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#include "common.h"
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/******************************************************************************/
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/*! Macro definition */
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/*! Earth's gravity in m/s^2 */
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#define GRAVITY_EARTH (9.80665f)
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/*! Macro that holds the total number of accel x,y and z axes sample counts to be printed */
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#define ACCEL_SAMPLE_COUNT UINT8_C(100)
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/******************************************************************************/
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/*! Static Function Declaration */
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/*! @brief This internal API converts raw sensor values(LSB) to meters per seconds square.
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*
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* @param[in] val : Raw sensor value.
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* @param[in] g_range : Accel Range selected (2G, 4G, 8G, 16G).
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* @param[in] bit_width : Resolution of the sensor.
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*
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* @return Accel values in meters per second square.
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*
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*/
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static float lsb_to_ms2(int16_t val, float g_range, uint8_t bit_width);
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/******************************************************************************/
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/*! Functions */
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/* This function starts the execution of program. */
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int main(void)
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{
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/* Variable to store the status of API */
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int8_t rslt;
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/* Sensor initialization configuration */
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struct bma4_dev bma = { 0 };
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/* Variable to store accel data ready interrupt status */
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uint16_t int_status = 0;
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/* Variable that holds the accelerometer sample count */
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uint8_t n_data = 1;
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struct bma4_accel sens_data = { 0 };
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float x = 0, y = 0, z = 0;
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struct bma4_accel_config accel_conf = { 0 };
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/* Interface reference is given as a parameter
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* For I2C : BMA4_I2C_INTF
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* For SPI : BMA4_SPI_INTF
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* Variant information given as parameter - BMA45X_VARIANT
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*/
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rslt = bma4_interface_init(&bma, BMA4_I2C_INTF, BMA45X_VARIANT);
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bma4_error_codes_print_result("bma4_interface_init", rslt);
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/* Sensor initialization */
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rslt = bma456h_init(&bma);
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bma4_error_codes_print_result("bma456h_init status", rslt);
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/* Upload the configuration file to enable the features of the sensor. */
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rslt = bma456h_write_config_file(&bma);
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bma4_error_codes_print_result("bma456h_write_config status", rslt);
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/* Mapping data ready interrupt with interrupt pin 1 to get interrupt status once getting new accel data */
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rslt = bma456h_map_interrupt(BMA4_INTR1_MAP, BMA4_DATA_RDY_INT, BMA4_ENABLE, &bma);
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bma4_error_codes_print_result("bma456h_map_interrupt status", rslt);
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/* Accelerometer configuration settings */
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/* Output data Rate */
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accel_conf.odr = BMA4_OUTPUT_DATA_RATE_50HZ;
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/* Gravity range of the sensor (+/- 2G, 4G, 8G, 16G) */
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accel_conf.range = BMA4_ACCEL_RANGE_2G;
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/* The bandwidth parameter is used to configure the number of sensor samples that are averaged
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* if it is set to 2, then 2^(bandwidth parameter) samples
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* are averaged, resulting in 4 averaged samples
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* Note1 : For more information, refer the datasheet.
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* Note2 : A higher number of averaged samples will result in a less noisier signal, but
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* this has an adverse effect on the power consumed.
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*/
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accel_conf.bandwidth = BMA4_ACCEL_NORMAL_AVG4;
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/* Enable the filter performance mode where averaging of samples
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* will be done based on above set bandwidth and ODR.
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* There are two modes
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* 0 -> Averaging samples (Default)
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* 1 -> No averaging
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* For more info on No Averaging mode refer datasheet.
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*/
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accel_conf.perf_mode = BMA4_CIC_AVG_MODE;
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/* Set the accel configurations */
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rslt = bma4_set_accel_config(&accel_conf, &bma);
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bma4_error_codes_print_result("bma4_set_accel_config status", rslt);
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/* NOTE : Enable accel after set of configurations */
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rslt = bma4_set_accel_enable(BMA4_ENABLE, &bma);
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bma4_error_codes_print_result("bma4_set_accel_enable status", rslt);
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printf("Data, Acc_Raw_X, Acc_Raw_Y, Acc_Raw_Z, Acc_ms2_X, Acc_ms2_Y, Acc_ms2_Z\n");
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for (;;)
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{
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/* Read interrupt status */
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rslt = bma456h_read_int_status(&int_status, &bma);
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bma4_error_codes_print_result("bma456h_read_int_status", rslt);
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/* Filtering only the accel data ready interrupt */
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if ((rslt == BMA4_OK) && (int_status & BMA4_ACCEL_DATA_RDY_INT))
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{
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/* Read the accel x, y, z data */
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rslt = bma4_read_accel_xyz(&sens_data, &bma);
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bma4_error_codes_print_result("bma4_read_accel_xyz status", rslt);
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if (rslt == BMA4_OK)
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{
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/* Converting lsb to meter per second squared for 16 bit resolution at 2G range */
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x = lsb_to_ms2(sens_data.x, (float)2, bma.resolution);
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y = lsb_to_ms2(sens_data.y, (float)2, bma.resolution);
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z = lsb_to_ms2(sens_data.z, (float)2, bma.resolution);
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/* Print the data in m/s2 */
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printf("%d, %d, %d, %d, %4.2f, %4.2f, %4.2f\n", n_data, sens_data.x, sens_data.y, sens_data.z, x, y, z);
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}
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/* Increment the count that determines the number of samples to be printed */
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n_data++;
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/* When the count reaches more than ACCEL_SAMPLE_COUNT, break and exit the loop */
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if (n_data > ACCEL_SAMPLE_COUNT)
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{
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break;
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}
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}
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}
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bma4_coines_deinit();
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return rslt;
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}
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/*!
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* @brief This internal API converts raw sensor values(LSB) to meters per seconds square.
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*/
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static float lsb_to_ms2(int16_t val, float g_range, uint8_t bit_width)
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{
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double power = 2;
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float half_scale = (float)((pow((double)power, (double)bit_width) / 2.0f));
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return (GRAVITY_EARTH * val * g_range) / half_scale;
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}
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