Multitech mDot/UDK support.
Dependencies: ST_INTERFACES X_NUCLEO_COMMON
Fork of X_NUCLEO_IKS01A1 by
Components/lsm6ds0/lsm6ds0_class.cpp
- Committer:
- Wolfgang Betz
- Date:
- 2015-06-03
- Revision:
- 24:92cc9c6e4b2b
- Parent:
- 7:a2bb3d5e12e9
- Child:
- 57:04563dd74269
File content as of revision 24:92cc9c6e4b2b:
/** ****************************************************************************** * @file lsm6ds0_class.cpp * @author AST / EST * @version V0.0.1 * @date 14-April-2015 * @brief Implementation file for the LSM6DS0 driver class ****************************************************************************** * @attention * * <h2><center>© COPYRIGHT(c) 2015 STMicroelectronics</center></h2> * * Redistribution and use in source and binary forms, with or without modification, * are permitted provided that the following conditions are met: * 1. Redistributions of source code must retain the above copyright notice, * this list of conditions and the following disclaimer. * 2. Redistributions in binary form must reproduce the above copyright notice, * this list of conditions and the following disclaimer in the documentation * and/or other materials provided with the distribution. * 3. Neither the name of STMicroelectronics nor the names of its contributors * may be used to endorse or promote products derived from this software * without specific prior written permission. * * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS "AS IS" * AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT LIMITED TO, THE * IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS FOR A PARTICULAR PURPOSE ARE * DISCLAIMED. IN NO EVENT SHALL THE COPYRIGHT HOLDER OR CONTRIBUTORS BE LIABLE * FOR ANY DIRECT, INDIRECT, INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL * DAMAGES (INCLUDING, BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR * SERVICES; LOSS OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER * CAUSED AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT LIABILITY, * OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN ANY WAY OUT OF THE USE * OF THIS SOFTWARE, EVEN IF ADVISED OF THE POSSIBILITY OF SUCH DAMAGE. * ****************************************************************************** */ /* Includes ------------------------------------------------------------------*/ #include "mbed.h" #include "lsm6ds0_class.h" #include "lsm6ds0.h" #include "../../x_nucleo_iks01a1_targets.h" /* Methods -------------------------------------------------------------------*/ /* betzw - based on: X-CUBE-MEMS1/trunk/Drivers/BSP/Components/lsm6ds0/lsm6ds0.c: revision #400, X-CUBE-MEMS1/trunk: revision #402 */ /** * @brief Set LSM6DS0 Initialization * @param LSM6DS0_Init the configuration setting for the LSM6DS0 * @retval IMU_6AXES_OK in case of success, an error code otherwise */ IMU_6AXES_StatusTypeDef LSM6DS0::LSM6DS0_Init(IMU_6AXES_InitTypeDef *LSM6DS0_Init) { /* Configure the low level interface ---------------------------------------*/ if(LSM6DS0_IO_Init() != IMU_6AXES_OK) { return IMU_6AXES_ERROR; } /******* Gyroscope init *******/ if(LSM6DS0_G_Set_ODR( LSM6DS0_Init->G_OutputDataRate ) != IMU_6AXES_OK) { return IMU_6AXES_ERROR; } if(LSM6DS0_G_Set_FS( LSM6DS0_Init->G_FullScale ) != IMU_6AXES_OK) { return IMU_6AXES_ERROR; } if(LSM6DS0_G_Set_Axes_Status(LSM6DS0_Init->G_X_Axis, LSM6DS0_Init->G_Y_Axis, LSM6DS0_Init->G_Z_Axis) != IMU_6AXES_OK) { return IMU_6AXES_ERROR; } /******************************/ /***** Accelerometer init *****/ if(LSM6DS0_X_Set_ODR( LSM6DS0_Init->X_OutputDataRate ) != IMU_6AXES_OK) { return IMU_6AXES_ERROR; } if(LSM6DS0_X_Set_FS( LSM6DS0_Init->X_FullScale ) != IMU_6AXES_OK) { return IMU_6AXES_ERROR; } if(LSM6DS0_X_Set_Axes_Status(LSM6DS0_Init->X_X_Axis, LSM6DS0_Init->X_Y_Axis, LSM6DS0_Init->X_Z_Axis) != IMU_6AXES_OK) { return IMU_6AXES_ERROR; } /* Configure interrupt lines */ LSM6DS0_IO_ITConfig(); return IMU_6AXES_OK; /******************************/ } /** * @brief Read ID of LSM6DS0 Accelerometer and Gyroscope * @param xg_id the pointer where the ID of the device is stored * @retval IMU_6AXES_OK in case of success, an error code otherwise */ IMU_6AXES_StatusTypeDef LSM6DS0::LSM6DS0_Read_XG_ID(uint8_t *xg_id) { if(!xg_id) { return IMU_6AXES_ERROR; } return LSM6DS0_IO_Read(xg_id, LSM6DS0_XG_WHO_AM_I_ADDR, 1); } /** * @brief Read raw data from LSM6DS0 Accelerometer output register * @param pData the pointer where the accelerometer raw data are stored * @retval IMU_6AXES_OK in case of success, an error code otherwise */ IMU_6AXES_StatusTypeDef LSM6DS0::LSM6DS0_X_GetAxesRaw(int16_t *pData) { uint8_t tempReg[2] = {0, 0}; if(LSM6DS0_IO_Read(&tempReg[0], (LSM6DS0_XG_OUT_X_L_XL | LSM6DS0_I2C_MULTIPLEBYTE_CMD), 2) != IMU_6AXES_OK) { return IMU_6AXES_ERROR; } pData[0] = ((((int16_t)tempReg[1]) << 8) + (int16_t)tempReg[0]); if(LSM6DS0_IO_Read(&tempReg[0], (LSM6DS0_XG_OUT_Y_L_XL | LSM6DS0_I2C_MULTIPLEBYTE_CMD), 2) != IMU_6AXES_OK) { return IMU_6AXES_ERROR; } pData[1] = ((((int16_t)tempReg[1]) << 8) + (int16_t)tempReg[0]); if(LSM6DS0_IO_Read(&tempReg[0], (LSM6DS0_XG_OUT_Z_L_XL | LSM6DS0_I2C_MULTIPLEBYTE_CMD), 2) != IMU_6AXES_OK) { return IMU_6AXES_ERROR; } pData[2] = ((((int16_t)tempReg[1]) << 8) + (int16_t)tempReg[0]); return IMU_6AXES_OK; } /** * @brief Read data from LSM6DS0 Accelerometer and calculate linear acceleration in mg * @param pData the pointer where the accelerometer data are stored * @retval IMU_6AXES_OK in case of success, an error code otherwise */ IMU_6AXES_StatusTypeDef LSM6DS0::LSM6DS0_X_GetAxes(int32_t *pData) { int16_t pDataRaw[3]; float sensitivity = 0; if(LSM6DS0_X_GetAxesRaw(pDataRaw) != IMU_6AXES_OK) { return IMU_6AXES_ERROR; } if(LSM6DS0_X_GetSensitivity( &sensitivity ) != IMU_6AXES_OK) { return IMU_6AXES_ERROR; } pData[0] = (int32_t)(pDataRaw[0] * sensitivity); pData[1] = (int32_t)(pDataRaw[1] * sensitivity); pData[2] = (int32_t)(pDataRaw[2] * sensitivity); return IMU_6AXES_OK; } /** * @brief Read raw data from LSM6DS0 Gyroscope output register * @param pData the pointer where the gyroscope raw data are stored * @retval IMU_6AXES_OK in case of success, an error code otherwise */ IMU_6AXES_StatusTypeDef LSM6DS0::LSM6DS0_G_GetAxesRaw(int16_t *pData) { uint8_t tempReg[2] = {0, 0}; if(LSM6DS0_IO_Read(&tempReg[0], (LSM6DS0_XG_OUT_X_L_G | LSM6DS0_I2C_MULTIPLEBYTE_CMD), 2) != IMU_6AXES_OK) { return IMU_6AXES_ERROR; } pData[0] = ((((int16_t)tempReg[1]) << 8) + (int16_t)tempReg[0]); if(LSM6DS0_IO_Read(&tempReg[0], (LSM6DS0_XG_OUT_Y_L_G | LSM6DS0_I2C_MULTIPLEBYTE_CMD), 2) != IMU_6AXES_OK) { return IMU_6AXES_ERROR; } pData[1] = ((((int16_t)tempReg[1]) << 8) + (int16_t)tempReg[0]); if(LSM6DS0_IO_Read(&tempReg[0], (LSM6DS0_XG_OUT_Z_L_G | LSM6DS0_I2C_MULTIPLEBYTE_CMD), 2) != IMU_6AXES_OK) { return IMU_6AXES_ERROR; } pData[2] = ((((int16_t)tempReg[1]) << 8) + (int16_t)tempReg[0]); return IMU_6AXES_OK; } /** * @brief Set the status of the axes for accelerometer * @param enableX the status of the x axis to be set * @param enableY the status of the y axis to be set * @param enableZ the status of the z axis to be set * @retval IMU_6AXES_OK in case of success, an error code otherwise */ IMU_6AXES_StatusTypeDef LSM6DS0::LSM6DS0_X_Set_Axes_Status(uint8_t enableX, uint8_t enableY, uint8_t enableZ) { uint8_t tmp1 = 0x00; uint8_t eX = 0x00; uint8_t eY = 0x00; uint8_t eZ = 0x00; eX = ( enableX == 0 ) ? LSM6DS0_XL_XEN_DISABLE : LSM6DS0_XL_XEN_ENABLE; eY = ( enableY == 0 ) ? LSM6DS0_XL_YEN_DISABLE : LSM6DS0_XL_YEN_ENABLE; eZ = ( enableZ == 0 ) ? LSM6DS0_XL_ZEN_DISABLE : LSM6DS0_XL_ZEN_ENABLE; if(LSM6DS0_IO_Read(&tmp1, LSM6DS0_XG_CTRL_REG5_XL, 1) != IMU_6AXES_OK) { return IMU_6AXES_ERROR; } /* Enable X axis selection */ tmp1 &= ~(LSM6DS0_XL_XEN_MASK); tmp1 |= eX; /* Enable Y axis selection */ tmp1 &= ~(LSM6DS0_XL_YEN_MASK); tmp1 |= eY; /* Enable Z axis selection */ tmp1 &= ~(LSM6DS0_XL_ZEN_MASK); tmp1 |= eZ; if(LSM6DS0_IO_Write(&tmp1, LSM6DS0_XG_CTRL_REG5_XL, 1) != IMU_6AXES_OK) { return IMU_6AXES_ERROR; } return IMU_6AXES_OK; } /** * @brief Set the status of the axes for gyroscope * @param enableX the status of the x axis to be set * @param enableY the status of the y axis to be set * @param enableZ the status of the z axis to be set * @retval IMU_6AXES_OK in case of success, an error code otherwise */ IMU_6AXES_StatusTypeDef LSM6DS0::LSM6DS0_G_Set_Axes_Status(uint8_t enableX, uint8_t enableY, uint8_t enableZ) { uint8_t tmp1 = 0x00; uint8_t eX = 0x00; uint8_t eY = 0x00; uint8_t eZ = 0x00; eX = ( enableX == 0 ) ? LSM6DS0_G_XEN_DISABLE : LSM6DS0_G_XEN_ENABLE; eY = ( enableY == 0 ) ? LSM6DS0_G_YEN_DISABLE : LSM6DS0_G_YEN_ENABLE; eZ = ( enableZ == 0 ) ? LSM6DS0_G_ZEN_DISABLE : LSM6DS0_G_ZEN_ENABLE; if(LSM6DS0_IO_Read(&tmp1, LSM6DS0_XG_CTRL_REG4, 1) != IMU_6AXES_OK) { return IMU_6AXES_ERROR; } /* Enable X axis selection */ tmp1 &= ~(LSM6DS0_G_XEN_MASK); tmp1 |= eX; /* Enable Y axis selection */ tmp1 &= ~(LSM6DS0_G_YEN_MASK); tmp1 |= eY; /* Enable Z axis selection */ tmp1 &= ~(LSM6DS0_G_ZEN_MASK); tmp1 |= eZ; if(LSM6DS0_IO_Write(&tmp1, LSM6DS0_XG_CTRL_REG4, 1) != IMU_6AXES_OK) { return IMU_6AXES_ERROR; } return IMU_6AXES_OK; } /** * @brief Read data from LSM6DS0 Gyroscope and calculate angular rate in mdps * @param pData the pointer where the gyroscope data are stored * @retval IMU_6AXES_OK in case of success, an error code otherwise */ IMU_6AXES_StatusTypeDef LSM6DS0::LSM6DS0_G_GetAxes(int32_t *pData) { int16_t pDataRaw[3]; float sensitivity = 0; if(LSM6DS0_G_GetAxesRaw(pDataRaw) != IMU_6AXES_OK) { return IMU_6AXES_ERROR; } if(LSM6DS0_G_GetSensitivity( &sensitivity ) != IMU_6AXES_OK) { return IMU_6AXES_ERROR; } pData[0] = (int32_t)(pDataRaw[0] * sensitivity); pData[1] = (int32_t)(pDataRaw[1] * sensitivity); pData[2] = (int32_t)(pDataRaw[2] * sensitivity); return IMU_6AXES_OK; } /** * @brief Read Accelero Output Data Rate * @param odr the pointer where the accelerometer output data rate is stored * @retval IMU_6AXES_OK in case of success, an error code otherwise */ IMU_6AXES_StatusTypeDef LSM6DS0::LSM6DS0_X_Get_ODR( float *odr ) { /*Here we have to add the check if the parameters are valid*/ uint8_t tempReg = 0x00; if(LSM6DS0_IO_Read( &tempReg, LSM6DS0_XG_CTRL_REG6_XL, 1 ) != IMU_6AXES_OK) { return IMU_6AXES_ERROR; } tempReg &= LSM6DS0_XL_ODR_MASK; switch( tempReg ) { case LSM6DS0_XL_ODR_PD: *odr = 0.0f; break; case LSM6DS0_XL_ODR_10HZ: *odr = 10.0f; break; case LSM6DS0_XL_ODR_50HZ: *odr = 50.0f; break; case LSM6DS0_XL_ODR_119HZ: *odr = 119.0f; break; case LSM6DS0_XL_ODR_238HZ: *odr = 238.0f; break; case LSM6DS0_XL_ODR_476HZ: *odr = 476.0f; break; case LSM6DS0_XL_ODR_952HZ: *odr = 952.0f; break; default: break; } return IMU_6AXES_OK; } /** * @brief Write Accelero Output Data Rate * @param odr the accelerometer output data rate to be set * @retval IMU_6AXES_OK in case of success, an error code otherwise */ IMU_6AXES_StatusTypeDef LSM6DS0::LSM6DS0_X_Set_ODR( float odr ) { uint8_t new_odr = 0x00; uint8_t tempReg = 0x00; new_odr = ( odr <= 0.0f ) ? LSM6DS0_XL_ODR_PD /* Power Down */ : ( odr <= 10.0f ) ? LSM6DS0_XL_ODR_10HZ : ( odr <= 50.0f ) ? LSM6DS0_XL_ODR_50HZ : ( odr <= 119.0f ) ? LSM6DS0_XL_ODR_119HZ : ( odr <= 238.0f ) ? LSM6DS0_XL_ODR_238HZ : ( odr <= 476.0f ) ? LSM6DS0_XL_ODR_476HZ : LSM6DS0_XL_ODR_952HZ; if(LSM6DS0_IO_Read( &tempReg, LSM6DS0_XG_CTRL_REG6_XL, 1 ) != IMU_6AXES_OK) { return IMU_6AXES_ERROR; } tempReg &= ~(LSM6DS0_XL_ODR_MASK); tempReg |= new_odr; if(LSM6DS0_IO_Write(&tempReg, LSM6DS0_XG_CTRL_REG6_XL, 1) != IMU_6AXES_OK) { return IMU_6AXES_ERROR; } return IMU_6AXES_OK; } /** * @brief Read Accelero Sensitivity * @param pfData the pointer where the accelerometer sensitivity is stored * @retval IMU_6AXES_OK in case of success, an error code otherwise */ IMU_6AXES_StatusTypeDef LSM6DS0::LSM6DS0_X_GetSensitivity( float *pfData ) { /*Here we have to add the check if the parameters are valid*/ uint8_t tempReg = 0x00; if(LSM6DS0_IO_Read( &tempReg, LSM6DS0_XG_CTRL_REG6_XL, 1 ) != IMU_6AXES_OK) { return IMU_6AXES_ERROR; } tempReg &= LSM6DS0_XL_FS_MASK; switch( tempReg ) { case LSM6DS0_XL_FS_2G: *pfData = 0.061f; break; case LSM6DS0_XL_FS_4G: *pfData = 0.122f; break; case LSM6DS0_XL_FS_8G: *pfData = 0.244f; break; case LSM6DS0_XL_FS_16G: *pfData = 0.732f; break; default: break; } return IMU_6AXES_OK; } /** * @brief Read Accelero Full Scale * @param fullScale the pointer where the accelerometer full scale is stored * @retval IMU_6AXES_OK in case of success, an error code otherwise */ IMU_6AXES_StatusTypeDef LSM6DS0::LSM6DS0_X_Get_FS( float *fullScale ) { /*Here we have to add the check if the parameters are valid*/ uint8_t tempReg = 0x00; if(LSM6DS0_IO_Read( &tempReg, LSM6DS0_XG_CTRL_REG6_XL, 1 ) != IMU_6AXES_OK) { return IMU_6AXES_ERROR; } tempReg &= LSM6DS0_XL_FS_MASK; switch( tempReg ) { case LSM6DS0_XL_FS_2G: *fullScale = 2.0f; break; case LSM6DS0_XL_FS_4G: *fullScale = 4.0f; break; case LSM6DS0_XL_FS_8G: *fullScale = 8.0f; break; case LSM6DS0_XL_FS_16G: *fullScale = 16.0f; break; default: break; } return IMU_6AXES_OK; } /** * @brief Write Accelero Full Scale * @param fullScale the accelerometer full scale to be set * @retval IMU_6AXES_OK in case of success, an error code otherwise */ IMU_6AXES_StatusTypeDef LSM6DS0::LSM6DS0_X_Set_FS( float fullScale ) { uint8_t new_fs = 0x00; uint8_t tempReg = 0x00; new_fs = ( fullScale <= 2.0f ) ? LSM6DS0_XL_FS_2G : ( fullScale <= 4.0f ) ? LSM6DS0_XL_FS_4G : ( fullScale <= 8.0f ) ? LSM6DS0_XL_FS_8G : LSM6DS0_XL_FS_16G; if(LSM6DS0_IO_Read( &tempReg, LSM6DS0_XG_CTRL_REG6_XL, 1 ) != IMU_6AXES_OK) { return IMU_6AXES_ERROR; } tempReg &= ~(LSM6DS0_XL_FS_MASK); tempReg |= new_fs; if(LSM6DS0_IO_Write(&tempReg, LSM6DS0_XG_CTRL_REG6_XL, 1) != IMU_6AXES_OK) { return IMU_6AXES_ERROR; } return IMU_6AXES_OK; } /** * @brief Read Gyro Output Data Rate * @param odr the pointer where the gyroscope output data rate is stored * @retval IMU_6AXES_OK in case of success, an error code otherwise */ IMU_6AXES_StatusTypeDef LSM6DS0::LSM6DS0_G_Get_ODR( float *odr ) { /*Here we have to add the check if the parameters are valid*/ uint8_t tempReg = 0x00; if(LSM6DS0_IO_Read( &tempReg, LSM6DS0_XG_CTRL_REG1_G, 1 ) != IMU_6AXES_OK) { return IMU_6AXES_ERROR; } tempReg &= LSM6DS0_G_ODR_MASK; switch( tempReg ) { case LSM6DS0_G_ODR_PD: *odr = 0.0f; break; case LSM6DS0_G_ODR_14_9HZ: *odr = 14.9f; break; case LSM6DS0_G_ODR_59_5HZ: *odr = 59.5f; break; case LSM6DS0_G_ODR_119HZ: *odr = 119.0f; break; case LSM6DS0_G_ODR_238HZ: *odr = 238.0f; break; case LSM6DS0_G_ODR_476HZ: *odr = 476.0f; break; case LSM6DS0_G_ODR_952HZ: *odr = 952.0f; break; default: break; } return IMU_6AXES_OK; } /** * @brief Write Gyro Output Data Rate * @param odr the gyroscope output data rate to be set * @retval IMU_6AXES_OK in case of success, an error code otherwise */ IMU_6AXES_StatusTypeDef LSM6DS0::LSM6DS0_G_Set_ODR( float odr ) { uint8_t new_odr = 0x00; uint8_t tempReg = 0x00; new_odr = ( odr <= 0.0f ) ? LSM6DS0_G_ODR_PD /* Power Down */ : ( odr <= 14.9f ) ? LSM6DS0_G_ODR_14_9HZ : ( odr <= 59.5f ) ? LSM6DS0_G_ODR_59_5HZ : ( odr <= 119.0f ) ? LSM6DS0_G_ODR_119HZ : ( odr <= 238.0f ) ? LSM6DS0_G_ODR_238HZ : ( odr <= 476.0f ) ? LSM6DS0_G_ODR_476HZ : LSM6DS0_G_ODR_952HZ; if(LSM6DS0_IO_Read( &tempReg, LSM6DS0_XG_CTRL_REG1_G, 1 ) != IMU_6AXES_OK) { return IMU_6AXES_ERROR; } tempReg &= ~(LSM6DS0_G_ODR_MASK); tempReg |= new_odr; if(LSM6DS0_IO_Write(&tempReg, LSM6DS0_XG_CTRL_REG1_G, 1) != IMU_6AXES_OK) { return IMU_6AXES_ERROR; } return IMU_6AXES_OK; } /** * @brief Read Gyro Sensitivity * @param pfData the pointer where the gyroscope sensitivity is stored * @retval IMU_6AXES_OK in case of success, an error code otherwise */ IMU_6AXES_StatusTypeDef LSM6DS0::LSM6DS0_G_GetSensitivity( float *pfData ) { /*Here we have to add the check if the parameters are valid*/ uint8_t tempReg = 0x00; if(LSM6DS0_IO_Read( &tempReg, LSM6DS0_XG_CTRL_REG1_G, 1 ) != IMU_6AXES_OK) { return IMU_6AXES_ERROR; } tempReg &= LSM6DS0_G_FS_MASK; switch( tempReg ) { case LSM6DS0_G_FS_245: *pfData = 8.75f; break; case LSM6DS0_G_FS_500: *pfData = 17.50f; break; case LSM6DS0_G_FS_2000: *pfData = 70.0f; break; default: break; } return IMU_6AXES_OK; } /** * @brief Read Gyro Full Scale * @param fullScale the pointer where the gyroscope full scale is stored * @retval IMU_6AXES_OK in case of success, an error code otherwise */ IMU_6AXES_StatusTypeDef LSM6DS0::LSM6DS0_G_Get_FS( float *fullScale ) { /*Here we have to add the check if the parameters are valid*/ uint8_t tempReg = 0x00; if(LSM6DS0_IO_Read( &tempReg, LSM6DS0_XG_CTRL_REG1_G, 1 ) != IMU_6AXES_OK) { return IMU_6AXES_ERROR; } tempReg &= LSM6DS0_G_FS_MASK; switch( tempReg ) { case LSM6DS0_G_FS_245: *fullScale = 245.0f; break; case LSM6DS0_G_FS_500: *fullScale = 500.0f; break; case LSM6DS0_G_FS_2000: *fullScale = 2000.0f; break; default: break; } return IMU_6AXES_OK; } /** * @brief Write Gyro Full Scale * @param fullScale the gyroscope full scale to be set * @retval IMU_6AXES_OK in case of success, an error code otherwise */ IMU_6AXES_StatusTypeDef LSM6DS0::LSM6DS0_G_Set_FS( float fullScale ) { uint8_t new_fs = 0x00; uint8_t tempReg = 0x00; new_fs = ( fullScale <= 245.0f ) ? LSM6DS0_G_FS_245 : ( fullScale <= 500.0f ) ? LSM6DS0_G_FS_500 : LSM6DS0_G_FS_2000; if(LSM6DS0_IO_Read( &tempReg, LSM6DS0_XG_CTRL_REG1_G, 1 ) != IMU_6AXES_OK) { return IMU_6AXES_ERROR; } tempReg &= ~(LSM6DS0_G_FS_MASK); tempReg |= new_fs; if(LSM6DS0_IO_Write(&tempReg, LSM6DS0_XG_CTRL_REG1_G, 1) != IMU_6AXES_OK) { return IMU_6AXES_ERROR; } return IMU_6AXES_OK; } /************************ (C) COPYRIGHT STMicroelectronics *****END OF FILE****/