#include #include #include #include #include #include #include #include #include #include #include "AP_InertialSensor.h" #include "AP_InertialSensor_BMI160.h" #include "AP_InertialSensor_Backend.h" #include "AP_InertialSensor_HIL.h" #include "AP_InertialSensor_L3G4200D.h" #include "AP_InertialSensor_LSM9DS0.h" #include "AP_InertialSensor_LSM9DS1.h" #include "AP_InertialSensor_Invensense.h" #include "AP_InertialSensor_PX4.h" #include "AP_InertialSensor_SITL.h" #include "AP_InertialSensor_RST.h" #include "AP_InertialSensor_Revo.h" #include "AP_InertialSensor_BMI055.h" /* Define INS_TIMING_DEBUG to track down scheduling issues with the main loop. * Output is on the debug console. */ #ifdef INS_TIMING_DEBUG #include #define timing_printf(fmt, args...) do { printf("[timing] " fmt, ##args); } while(0) #else #define timing_printf(fmt, args...) #endif extern const AP_HAL::HAL& hal; #if APM_BUILD_TYPE(APM_BUILD_ArduCopter) #define DEFAULT_GYRO_FILTER 20 #define DEFAULT_ACCEL_FILTER 20 #define DEFAULT_STILL_THRESH 2.5f #elif APM_BUILD_TYPE(APM_BUILD_APMrover2) #define DEFAULT_GYRO_FILTER 4 #define DEFAULT_ACCEL_FILTER 10 #define DEFAULT_STILL_THRESH 0.1f #else #define DEFAULT_GYRO_FILTER 20 #define DEFAULT_ACCEL_FILTER 20 #define DEFAULT_STILL_THRESH 0.1f #endif #define SAMPLE_UNIT 1 #define GYRO_INIT_MAX_DIFF_DPS 0.1f // Class level parameters const AP_Param::GroupInfo AP_InertialSensor::var_info[] = { // @Param: PRODUCT_ID // @DisplayName: IMU Product ID // @Description: unused // @User: Advanced AP_GROUPINFO("PRODUCT_ID", 0, AP_InertialSensor, _old_product_id, 0), /* The following parameter indexes and reserved from previous use as accel offsets and scaling from before the 16g change in the PX4 backend: ACCSCAL : 1 ACCOFFS : 2 MPU6K_FILTER: 4 ACC2SCAL : 5 ACC2OFFS : 6 ACC3SCAL : 8 ACC3OFFS : 9 CALSENSFRAME : 11 */ // @Param: GYROFFS_X // @DisplayName: Gyro offsets of X axis // @Description: Gyro sensor offsets of X axis. This is setup on each boot during gyro calibrations // @Units: rad/s // @User: Advanced // @Param: GYROFFS_Y // @DisplayName: Gyro offsets of Y axis // @Description: Gyro sensor offsets of Y axis. This is setup on each boot during gyro calibrations // @Units: rad/s // @User: Advanced // @Param: GYROFFS_Z // @DisplayName: Gyro offsets of Z axis // @Description: Gyro sensor offsets of Z axis. This is setup on each boot during gyro calibrations // @Units: rad/s // @User: Advanced AP_GROUPINFO("GYROFFS", 3, AP_InertialSensor, _gyro_offset[0], 0), // @Param: GYR2OFFS_X // @DisplayName: Gyro2 offsets of X axis // @Description: Gyro2 sensor offsets of X axis. This is setup on each boot during gyro calibrations // @Units: rad/s // @User: Advanced // @Param: GYR2OFFS_Y // @DisplayName: Gyro2 offsets of Y axis // @Description: Gyro2 sensor offsets of Y axis. This is setup on each boot during gyro calibrations // @Units: rad/s // @User: Advanced // @Param: GYR2OFFS_Z // @DisplayName: Gyro2 offsets of Z axis // @Description: Gyro2 sensor offsets of Z axis. This is setup on each boot during gyro calibrations // @Units: rad/s // @User: Advanced AP_GROUPINFO("GYR2OFFS", 7, AP_InertialSensor, _gyro_offset[1], 0), // @Param: GYR3OFFS_X // @DisplayName: Gyro3 offsets of X axis // @Description: Gyro3 sensor offsets of X axis. This is setup on each boot during gyro calibrations // @Units: rad/s // @User: Advanced // @Param: GYR3OFFS_Y // @DisplayName: Gyro3 offsets of Y axis // @Description: Gyro3 sensor offsets of Y axis. This is setup on each boot during gyro calibrations // @Units: rad/s // @User: Advanced // @Param: GYR3OFFS_Z // @DisplayName: Gyro3 offsets of Z axis // @Description: Gyro3 sensor offsets of Z axis. This is setup on each boot during gyro calibrations // @Units: rad/s // @User: Advanced AP_GROUPINFO("GYR3OFFS", 10, AP_InertialSensor, _gyro_offset[2], 0), // @Param: ACCSCAL_X // @DisplayName: Accelerometer scaling of X axis // @Description: Accelerometer scaling of X axis. Calculated during acceleration calibration routine // @Range: 0.8 1.2 // @User: Advanced // @Param: ACCSCAL_Y // @DisplayName: Accelerometer scaling of Y axis // @Description: Accelerometer scaling of Y axis Calculated during acceleration calibration routine // @Range: 0.8 1.2 // @User: Advanced // @Param: ACCSCAL_Z // @DisplayName: Accelerometer scaling of Z axis // @Description: Accelerometer scaling of Z axis Calculated during acceleration calibration routine // @Range: 0.8 1.2 // @User: Advanced AP_GROUPINFO("ACCSCAL", 12, AP_InertialSensor, _accel_scale[0], 0), // @Param: ACCOFFS_X // @DisplayName: Accelerometer offsets of X axis // @Description: Accelerometer offsets of X axis. This is setup using the acceleration calibration or level operations // @Units: m/s/s // @Range: -3.5 3.5 // @User: Advanced // @Param: ACCOFFS_Y // @DisplayName: Accelerometer offsets of Y axis // @Description: Accelerometer offsets of Y axis. This is setup using the acceleration calibration or level operations // @Units: m/s/s // @Range: -3.5 3.5 // @User: Advanced // @Param: ACCOFFS_Z // @DisplayName: Accelerometer offsets of Z axis // @Description: Accelerometer offsets of Z axis. This is setup using the acceleration calibration or level operations // @Units: m/s/s // @Range: -3.5 3.5 // @User: Advanced AP_GROUPINFO("ACCOFFS", 13, AP_InertialSensor, _accel_offset[0], 0), // @Param: ACC2SCAL_X // @DisplayName: Accelerometer2 scaling of X axis // @Description: Accelerometer2 scaling of X axis. Calculated during acceleration calibration routine // @Range: 0.8 1.2 // @User: Advanced // @Param: ACC2SCAL_Y // @DisplayName: Accelerometer2 scaling of Y axis // @Description: Accelerometer2 scaling of Y axis Calculated during acceleration calibration routine // @Range: 0.8 1.2 // @User: Advanced // @Param: ACC2SCAL_Z // @DisplayName: Accelerometer2 scaling of Z axis // @Description: Accelerometer2 scaling of Z axis Calculated during acceleration calibration routine // @Range: 0.8 1.2 // @User: Advanced AP_GROUPINFO("ACC2SCAL", 14, AP_InertialSensor, _accel_scale[1], 0), // @Param: ACC2OFFS_X // @DisplayName: Accelerometer2 offsets of X axis // @Description: Accelerometer2 offsets of X axis. This is setup using the acceleration calibration or level operations // @Units: m/s/s // @Range: -3.5 3.5 // @User: Advanced // @Param: ACC2OFFS_Y // @DisplayName: Accelerometer2 offsets of Y axis // @Description: Accelerometer2 offsets of Y axis. This is setup using the acceleration calibration or level operations // @Units: m/s/s // @Range: -3.5 3.5 // @User: Advanced // @Param: ACC2OFFS_Z // @DisplayName: Accelerometer2 offsets of Z axis // @Description: Accelerometer2 offsets of Z axis. This is setup using the acceleration calibration or level operations // @Units: m/s/s // @Range: -3.5 3.5 // @User: Advanced AP_GROUPINFO("ACC2OFFS", 15, AP_InertialSensor, _accel_offset[1], 0), // @Param: ACC3SCAL_X // @DisplayName: Accelerometer3 scaling of X axis // @Description: Accelerometer3 scaling of X axis. Calculated during acceleration calibration routine // @Range: 0.8 1.2 // @User: Advanced // @Param: ACC3SCAL_Y // @DisplayName: Accelerometer3 scaling of Y axis // @Description: Accelerometer3 scaling of Y axis Calculated during acceleration calibration routine // @Range: 0.8 1.2 // @User: Advanced // @Param: ACC3SCAL_Z // @DisplayName: Accelerometer3 scaling of Z axis // @Description: Accelerometer3 scaling of Z axis Calculated during acceleration calibration routine // @Range: 0.8 1.2 // @User: Advanced AP_GROUPINFO("ACC3SCAL", 16, AP_InertialSensor, _accel_scale[2], 0), // @Param: ACC3OFFS_X // @DisplayName: Accelerometer3 offsets of X axis // @Description: Accelerometer3 offsets of X axis. This is setup using the acceleration calibration or level operations // @Units: m/s/s // @Range: -3.5 3.5 // @User: Advanced // @Param: ACC3OFFS_Y // @DisplayName: Accelerometer3 offsets of Y axis // @Description: Accelerometer3 offsets of Y axis. This is setup using the acceleration calibration or level operations // @Units: m/s/s // @Range: -3.5 3.5 // @User: Advanced // @Param: ACC3OFFS_Z // @DisplayName: Accelerometer3 offsets of Z axis // @Description: Accelerometer3 offsets of Z axis. This is setup using the acceleration calibration or level operations // @Units: m/s/s // @Range: -3.5 3.5 // @User: Advanced AP_GROUPINFO("ACC3OFFS", 17, AP_InertialSensor, _accel_offset[2], 0), // @Param: GYRO_FILTER // @DisplayName: Gyro filter cutoff frequency // @Description: Filter cutoff frequency for gyroscopes. This can be set to a lower value to try to cope with very high vibration levels in aircraft. This option takes effect on the next reboot. A value of zero means no filtering (not recommended!) // @Units: Hz // @Range: 0 127 // @User: Advanced AP_GROUPINFO("GYRO_FILTER", 18, AP_InertialSensor, _gyro_filter_cutoff, DEFAULT_GYRO_FILTER), // @Param: ACCEL_FILTER // @DisplayName: Accel filter cutoff frequency // @Description: Filter cutoff frequency for accelerometers. This can be set to a lower value to try to cope with very high vibration levels in aircraft. This option takes effect on the next reboot. A value of zero means no filtering (not recommended!) // @Units: Hz // @Range: 0 127 // @User: Advanced AP_GROUPINFO("ACCEL_FILTER", 19, AP_InertialSensor, _accel_filter_cutoff, DEFAULT_ACCEL_FILTER), // @Param: USE // @DisplayName: Use first IMU for attitude, velocity and position estimates // @Description: Use first IMU for attitude, velocity and position estimates // @Values: 0:Disabled,1:Enabled // @User: Advanced AP_GROUPINFO("USE", 20, AP_InertialSensor, _use[0], 1), // @Param: USE2 // @DisplayName: Use second IMU for attitude, velocity and position estimates // @Description: Use second IMU for attitude, velocity and position estimates // @Values: 0:Disabled,1:Enabled // @User: Advanced AP_GROUPINFO("USE2", 21, AP_InertialSensor, _use[1], 1), // @Param: USE3 // @DisplayName: Use third IMU for attitude, velocity and position estimates // @Description: Use third IMU for attitude, velocity and position estimates // @Values: 0:Disabled,1:Enabled // @User: Advanced AP_GROUPINFO("USE3", 22, AP_InertialSensor, _use[2], 0), // @Param: STILL_THRESH // @DisplayName: Stillness threshold for detecting if we are moving // @Description: Threshold to tolerate vibration to determine if vehicle is motionless. This depends on the frame type and if there is a constant vibration due to motors before launch or after landing. Total motionless is about 0.05. Suggested values: Planes/rover use 0.1, multirotors use 1, tradHeli uses 5 // @Range: 0.05 50 // @User: Advanced AP_GROUPINFO("STILL_THRESH", 23, AP_InertialSensor, _still_threshold, DEFAULT_STILL_THRESH), // @Param: GYR_CAL // @DisplayName: Gyro Calibration scheme // @Description: Conrols when automatic gyro calibration is performed // @Values: 0:Never, 1:Start-up only // @User: Advanced AP_GROUPINFO("GYR_CAL", 24, AP_InertialSensor, _gyro_cal_timing, 1), // @Param: TRIM_OPTION // @DisplayName: Accel cal trim option // @Description: Specifies how the accel cal routine determines the trims // @User: Advanced // @Values: 0:Don't adjust the trims,1:Assume first orientation was level,2:Assume ACC_BODYFIX is perfectly aligned to the vehicle AP_GROUPINFO("TRIM_OPTION", 25, AP_InertialSensor, _trim_option, 1), // @Param: ACC_BODYFIX // @DisplayName: Body-fixed accelerometer // @Description: The body-fixed accelerometer to be used for trim calculation // @User: Advanced // @Values: 1:IMU 1,2:IMU 2,3:IMU 3 AP_GROUPINFO("ACC_BODYFIX", 26, AP_InertialSensor, _acc_body_aligned, 2), // @Param: POS1_X // @DisplayName: IMU accelerometer X position // @Description: X position of the first IMU Accelerometer in body frame. Positive X is forward of the origin. Attention: The IMU should be located as close to the vehicle c.g. as practical so that the value of this parameter is minimised. Failure to do so can result in noisy navigation velocity measurements due to vibration and IMU gyro noise. If the IMU cannot be moved and velocity noise is a problem, a location closer to the IMU can be used as the body frame origin. // @Units: m // @User: Advanced // @Param: POS1_Y // @DisplayName: IMU accelerometer Y position // @Description: Y position of the first IMU accelerometer in body frame. Positive Y is to the right of the origin. Attention: The IMU should be located as close to the vehicle c.g. as practical so that the value of this parameter is minimised. Failure to do so can result in noisy navigation velocity measurements due to vibration and IMU gyro noise. If the IMU cannot be moved and velocity noise is a problem, a location closer to the IMU can be used as the body frame origin. // @Units: m // @User: Advanced // @Param: POS1_Z // @DisplayName: IMU accelerometer Z position // @Description: Z position of the first IMU accelerometer in body frame. Positive Z is down from the origin. Attention: The IMU should be located as close to the vehicle c.g. as practical so that the value of this parameter is minimised. Failure to do so can result in noisy navigation velocity measurements due to vibration and IMU gyro noise. If the IMU cannot be moved and velocity noise is a problem, a location closer to the IMU can be used as the body frame origin. // @Units: m // @User: Advanced AP_GROUPINFO("POS1", 27, AP_InertialSensor, _accel_pos[0], 0.0f), // @Param: POS2_X // @DisplayName: IMU accelerometer X position // @Description: X position of the second IMU accelerometer in body frame. Positive X is forward of the origin. Attention: The IMU should be located as close to the vehicle c.g. as practical so that the value of this parameter is minimised. Failure to do so can result in noisy navigation velocity measurements due to vibration and IMU gyro noise. If the IMU cannot be moved and velocity noise is a problem, a location closer to the IMU can be used as the body frame origin. // @Units: m // @User: Advanced // @Param: POS2_Y // @DisplayName: IMU accelerometer Y position // @Description: Y position of the second IMU accelerometer in body frame. Positive Y is to the right of the origin. Attention: The IMU should be located as close to the vehicle c.g. as practical so that the value of this parameter is minimised. Failure to do so can result in noisy navigation velocity measurements due to vibration and IMU gyro noise. If the IMU cannot be moved and velocity noise is a problem, a location closer to the IMU can be used as the body frame origin. // @Units: m // @User: Advanced // @Param: POS2_Z // @DisplayName: IMU accelerometer Z position // @Description: Z position of the second IMU accelerometer in body frame. Positive Z is down from the origin. Attention: The IMU should be located as close to the vehicle c.g. as practical so that the value of this parameter is minimised. Failure to do so can result in noisy navigation velocity measurements due to vibration and IMU gyro noise. If the IMU cannot be moved and velocity noise is a problem, a location closer to the IMU can be used as the body frame origin. // @Units: m // @User: Advanced AP_GROUPINFO("POS2", 28, AP_InertialSensor, _accel_pos[1], 0.0f), // @Param: POS3_X // @DisplayName: IMU accelerometer X position // @Description: X position of the third IMU accelerometer in body frame. Positive X is forward of the origin. Attention: The IMU should be located as close to the vehicle c.g. as practical so that the value of this parameter is minimised. Failure to do so can result in noisy navigation velocity measurements due to vibration and IMU gyro noise. If the IMU cannot be moved and velocity noise is a problem, a location closer to the IMU can be used as the body frame origin. // @Units: m // @User: Advanced // @Param: POS3_Y // @DisplayName: IMU accelerometer Y position // @Description: Y position of the third IMU accelerometer in body frame. Positive Y is to the right of the origin. Attention: The IMU should be located as close to the vehicle c.g. as practical so that the value of this parameter is minimised. Failure to do so can result in noisy navigation velocity measurements due to vibration and IMU gyro noise. If the IMU cannot be moved and velocity noise is a problem, a location closer to the IMU can be used as the body frame origin. // @Units: m // @User: Advanced // @Param: POS3_Z // @DisplayName: IMU accelerometer Z position // @Description: Z position of the third IMU accelerometer in body frame. Positive Z is down from the origin. Attention: The IMU should be located as close to the vehicle c.g. as practical so that the value of this parameter is minimised. Failure to do so can result in noisy navigation velocity measurements due to vibration and IMU gyro noise. If the IMU cannot be moved and velocity noise is a problem, a location closer to the IMU can be used as the body frame origin. // @Units: m // @User: Advanced AP_GROUPINFO("POS3", 29, AP_InertialSensor, _accel_pos[2], 0.0f), // @Param: GYR_ID // @DisplayName: Gyro ID // @Description: Gyro sensor ID, taking into account its type, bus and instance // @ReadOnly: True // @User: Advanced AP_GROUPINFO("GYR_ID", 30, AP_InertialSensor, _gyro_id[0], 0), // @Param: GYR2_ID // @DisplayName: Gyro2 ID // @Description: Gyro2 sensor ID, taking into account its type, bus and instance // @ReadOnly: True // @User: Advanced AP_GROUPINFO("GYR2_ID", 31, AP_InertialSensor, _gyro_id[1], 0), // @Param: GYR3_ID // @DisplayName: Gyro3 ID // @Description: Gyro3 sensor ID, taking into account its type, bus and instance // @ReadOnly: True // @User: Advanced AP_GROUPINFO("GYR3_ID", 32, AP_InertialSensor, _gyro_id[2], 0), // @Param: ACC_ID // @DisplayName: Accelerometer ID // @Description: Accelerometer sensor ID, taking into account its type, bus and instance // @ReadOnly: True // @User: Advanced AP_GROUPINFO("ACC_ID", 33, AP_InertialSensor, _accel_id[0], 0), // @Param: ACC2_ID // @DisplayName: Accelerometer2 ID // @Description: Accelerometer2 sensor ID, taking into account its type, bus and instance // @ReadOnly: True // @User: Advanced AP_GROUPINFO("ACC2_ID", 34, AP_InertialSensor, _accel_id[1], 0), // @Param: ACC3_ID // @DisplayName: Accelerometer3 ID // @Description: Accelerometer3 sensor ID, taking into account its type, bus and instance // @ReadOnly: True // @User: Advanced AP_GROUPINFO("ACC3_ID", 35, AP_InertialSensor, _accel_id[2], 0), // @Param: FAST_SAMPLE // @DisplayName: Fast sampling mask // @Description: Mask of IMUs to enable fast sampling on, if available // @User: Advanced // @Values: 1:FirstIMUOnly,3:FirstAndSecondIMU // @Bitmask: 0:FirstIMU,1:SecondIMU,2:ThirdIMU AP_GROUPINFO("FAST_SAMPLE", 36, AP_InertialSensor, _fast_sampling_mask, 0), // @Group: NOTCH_ // @Path: ../Filter/NotchFilter.cpp AP_SUBGROUPINFO(_notch_filter, "NOTCH_", 37, AP_InertialSensor, NotchFilterVector3fParam), // @Group: LOG_ // @Path: ../AP_InertialSensor/BatchSampler.cpp AP_SUBGROUPINFO(batchsampler, "LOG_", 39, AP_InertialSensor, AP_InertialSensor::BatchSampler), // @Group: ENABLE_MASK // @DisplayName: IMU enable mask // @Description: This is a bitmask of IMUs to enable. It can be used to prevent startup of specific detected IMUs // @User: Advanced // @Values: 1:FirstIMUOnly,3:FirstAndSecondIMU,7:FirstSecondAndThirdIMU,127:AllIMUs // @Bitmask: 0:FirstIMU,1:SecondIMU,2:ThirdIMU AP_GROUPINFO("ENABLE_MASK", 40, AP_InertialSensor, _enable_mask, 0x7F), /* NOTE: parameter indexes have gaps above. When adding new parameters check for conflicts carefully */ AP_GROUPEND }; AP_InertialSensor *AP_InertialSensor::_s_instance = nullptr; AP_InertialSensor::AP_InertialSensor() : _board_orientation(ROTATION_NONE), _log_raw_bit(-1) { if (_s_instance) { AP_HAL::panic("Too many inertial sensors"); } _s_instance = this; AP_Param::setup_object_defaults(this, var_info); for (uint8_t i=0; istart(); } if (_gyro_count == 0 || _accel_count == 0) { AP_HAL::panic("INS needs at least 1 gyro and 1 accel"); } // clear IDs for unused sensor instances for (uint8_t i=get_accel_count(); iget_id(); if (id < 0 || id != backend_id) { continue; } if (instance == found) { return _backends[i]; } else { found++; } } return nullptr; } void AP_InertialSensor::init(uint16_t sample_rate) { // remember the sample rate _sample_rate = sample_rate; _loop_delta_t = 1.0f / sample_rate; // we don't allow deltat values greater than 10x the normal loop // time to be exposed outside of INS. Large deltat values can // cause divergence of state estimators _loop_delta_t_max = 10 * _loop_delta_t; if (_gyro_count == 0 && _accel_count == 0) { _start_backends(); } // initialise accel scale if need be. This is needed as we can't // give non-zero default values for vectors in AP_Param for (uint8_t i=0; iget_device(HAL_INS_MPU60x0_NAME), HAL_INS_DEFAULT_ROTATION)); #elif HAL_INS_DEFAULT == HAL_INS_MPU60XX_SPI && defined(HAL_INS_DEFAULT_ROTATION) ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device(HAL_INS_MPU60x0_NAME), HAL_INS_DEFAULT_ROTATION)); #elif HAL_INS_DEFAULT == HAL_INS_MPU60XX_SPI ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device(HAL_INS_MPU60x0_NAME))); #elif HAL_INS_DEFAULT == HAL_INS_MPU60XX_I2C && defined(HAL_INS_DEFAULT_ROTATION) ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.i2c_mgr->get_device(HAL_INS_MPU60x0_I2C_BUS, HAL_INS_MPU60x0_I2C_ADDR), HAL_INS_DEFAULT_ROTATION)); #elif HAL_INS_DEFAULT == HAL_INS_MPU60XX_I2C ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.i2c_mgr->get_device(HAL_INS_MPU60x0_I2C_BUS, HAL_INS_MPU60x0_I2C_ADDR))); #elif HAL_INS_DEFAULT == HAL_INS_BH ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.i2c_mgr->get_device(HAL_INS_MPU60x0_I2C_BUS, HAL_INS_MPU60x0_I2C_ADDR))); ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device(HAL_INS_MPU9250_NAME))); #elif AP_FEATURE_BOARD_DETECT switch (AP_BoardConfig::get_board_type()) { case AP_BoardConfig::PX4_BOARD_PX4V1: ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device(HAL_INS_MPU60x0_NAME))); break; case AP_BoardConfig::PX4_BOARD_PIXHAWK: ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device(HAL_INS_MPU60x0_NAME), ROTATION_ROLL_180)); ADD_BACKEND(AP_InertialSensor_LSM9DS0::probe(*this, hal.spi->get_device(HAL_INS_LSM9DS0_G_NAME), hal.spi->get_device(HAL_INS_LSM9DS0_A_NAME), ROTATION_ROLL_180, ROTATION_ROLL_180_YAW_270, ROTATION_PITCH_180)); break; case AP_BoardConfig::PX4_BOARD_PIXHAWK2: // older Pixhawk2 boards have the MPU6000 instead of MPU9250 _fast_sampling_mask.set_default(1); ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device(HAL_INS_MPU9250_EXT_NAME), ROTATION_PITCH_180)); ADD_BACKEND(AP_InertialSensor_LSM9DS0::probe(*this, hal.spi->get_device(HAL_INS_LSM9DS0_EXT_G_NAME), hal.spi->get_device(HAL_INS_LSM9DS0_EXT_A_NAME), ROTATION_ROLL_180_YAW_270, ROTATION_ROLL_180_YAW_90, ROTATION_ROLL_180_YAW_90)); ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device(HAL_INS_MPU9250_NAME), ROTATION_YAW_270)); break; case AP_BoardConfig::PX4_BOARD_FMUV5: _fast_sampling_mask.set_default(1); ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device("icm20689"), ROTATION_NONE)); ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device("icm20602"), ROTATION_NONE)); ADD_BACKEND(AP_InertialSensor_BMI055::probe(*this, hal.spi->get_device("bmi055_a"), hal.spi->get_device("bmi055_g"), ROTATION_ROLL_180_YAW_90)); break; case AP_BoardConfig::PX4_BOARD_SP01: _fast_sampling_mask.set_default(1); ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device(HAL_INS_MPU9250_EXT_NAME), ROTATION_NONE)); ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device(HAL_INS_MPU9250_NAME), ROTATION_NONE)); break; case AP_BoardConfig::PX4_BOARD_PIXRACER: // only do fast samplng on ICM-20608. The MPU9250 doesn't handle high rate well when it has a mag enabled _fast_sampling_mask.set_default(1); ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device(HAL_INS_ICM20608_NAME), ROTATION_ROLL_180_YAW_90)); ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device(HAL_INS_MPU9250_NAME), ROTATION_ROLL_180_YAW_90)); break; case AP_BoardConfig::PX4_BOARD_PIXHAWK_PRO: _fast_sampling_mask.set_default(3); ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device(HAL_INS_ICM20608_NAME), ROTATION_ROLL_180_YAW_90)); ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device(HAL_INS_MPU9250_NAME), ROTATION_ROLL_180_YAW_90)); break; case AP_BoardConfig::PX4_BOARD_PHMINI: // PHMINI uses ICM20608 on the ACCEL_MAG device and a MPU9250 on the old MPU6000 CS line _fast_sampling_mask.set_default(3); ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device(HAL_INS_ICM20608_AM_NAME), ROTATION_ROLL_180)); ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device(HAL_INS_MPU9250_NAME), ROTATION_ROLL_180)); break; case AP_BoardConfig::PX4_BOARD_AUAV21: // AUAV2.1 uses ICM20608 on the ACCEL_MAG device and a MPU9250 on the old MPU6000 CS line _fast_sampling_mask.set_default(3); ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device(HAL_INS_ICM20608_AM_NAME), ROTATION_ROLL_180_YAW_90)); ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device(HAL_INS_MPU9250_NAME), ROTATION_ROLL_180_YAW_90)); break; case AP_BoardConfig::PX4_BOARD_PH2SLIM: _fast_sampling_mask.set_default(1); ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device(HAL_INS_MPU9250_NAME), ROTATION_YAW_270)); break; case AP_BoardConfig::PX4_BOARD_AEROFC: _fast_sampling_mask.set_default(1); ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device(HAL_INS_MPU6500_NAME), ROTATION_YAW_270)); break; case AP_BoardConfig::PX4_BOARD_MINDPXV2: ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device(HAL_INS_MPU6500_NAME), ROTATION_NONE)); ADD_BACKEND(AP_InertialSensor_LSM9DS0::probe(*this, hal.spi->get_device(HAL_INS_LSM9DS0_G_NAME), hal.spi->get_device(HAL_INS_LSM9DS0_A_NAME), ROTATION_YAW_90, ROTATION_YAW_90, ROTATION_YAW_90)); break; case AP_BoardConfig::VRX_BOARD_BRAIN54: _fast_sampling_mask.set_default(7); ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device(HAL_INS_MPU60x0_NAME), ROTATION_YAW_180)); ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device(HAL_INS_MPU60x0_EXT_NAME), ROTATION_YAW_180)); #ifdef HAL_INS_MPU60x0_IMU_NAME ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device(HAL_INS_MPU60x0_IMU_NAME), ROTATION_YAW_180)); #endif break; case AP_BoardConfig::VRX_BOARD_BRAIN51: case AP_BoardConfig::VRX_BOARD_BRAIN52: case AP_BoardConfig::VRX_BOARD_BRAIN52E: case AP_BoardConfig::VRX_BOARD_CORE10: case AP_BoardConfig::VRX_BOARD_UBRAIN51: case AP_BoardConfig::VRX_BOARD_UBRAIN52: ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device(HAL_INS_MPU60x0_NAME), ROTATION_YAW_180)); break; case AP_BoardConfig::PX4_BOARD_PCNC1: _add_backend(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device(HAL_INS_MPU60x0_NAME), ROTATION_ROLL_180)); break; default: break; } #if CONFIG_HAL_BOARD == HAL_BOARD_PX4 // also add any PX4 backends (eg. canbus sensors) ADD_BACKEND(AP_InertialSensor_PX4::detect(*this)); #endif #elif HAL_INS_DEFAULT == HAL_INS_MPU9250_SPI && defined(HAL_INS_DEFAULT_ROTATION) ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device(HAL_INS_MPU9250_NAME), HAL_INS_DEFAULT_ROTATION)); #elif HAL_INS_DEFAULT == HAL_INS_MPU9250_SPI ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device(HAL_INS_MPU9250_NAME))); #elif HAL_INS_DEFAULT == HAL_INS_EDGE ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device(HAL_INS_MPU60x0_NAME), ROTATION_YAW_90)); ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device(HAL_INS_MPU60x0_NAME_EXT), ROTATION_YAW_90)); #elif HAL_INS_DEFAULT == HAL_INS_LSM9DS1 ADD_BACKEND(AP_InertialSensor_LSM9DS1::probe(*this, hal.spi->get_device(HAL_INS_LSM9DS1_NAME))); #elif HAL_INS_DEFAULT == HAL_INS_LSM9DS0 ADD_BACKEND(AP_InertialSensor_LSM9DS0::probe(*this, hal.spi->get_device(HAL_INS_LSM9DS0_G_NAME), hal.spi->get_device(HAL_INS_LSM9DS0_A_NAME))); #elif HAL_INS_DEFAULT == HAL_INS_L3G4200D ADD_BACKEND(AP_InertialSensor_L3G4200D::probe(*this, hal.i2c_mgr->get_device(HAL_INS_L3G4200D_I2C_BUS, HAL_INS_L3G4200D_I2C_ADDR))); #elif HAL_INS_DEFAULT == HAL_INS_MPU9250_I2C ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.i2c_mgr->get_device(HAL_INS_MPU9250_I2C_BUS, HAL_INS_MPU9250_I2C_ADDR))); #elif HAL_INS_DEFAULT == HAL_INS_BBBMINI ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device(HAL_INS_MPU9250_NAME))); ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device(HAL_INS_MPU9250_NAME_EXT))); #elif HAL_INS_DEFAULT == HAL_INS_AERO ADD_BACKEND(AP_InertialSensor_BMI160::probe(*this, hal.spi->get_device("bmi160"))); #elif HAL_INS_DEFAULT == HAL_INS_RST ADD_BACKEND(AP_InertialSensor_RST::probe(*this, hal.spi->get_device(HAL_INS_RST_G_NAME), hal.spi->get_device(HAL_INS_RST_A_NAME), HAL_INS_DEFAULT_G_ROTATION, HAL_INS_DEFAULT_A_ROTATION)); #elif HAL_INS_DEFAULT == HAL_INS_ICM20789_SPI ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device("icm20789"))); #elif CONFIG_HAL_BOARD_SUBTYPE == HAL_BOARD_SUBTYPE_CHIBIOS_OMNIBUSF7V2 ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device("mpu6000"), ROTATION_NONE)); ADD_BACKEND(AP_InertialSensor_Invensense::probe(*this, hal.spi->get_device("mpu6500"), ROTATION_NONE)); #elif HAL_INS_DEFAULT == HAL_INS_NONE // no INS device #else #error Unrecognised HAL_INS_TYPE setting #endif _enable_mask.set(found_mask); if (_backend_count == 0) { AP_BoardConfig::sensor_config_error("INS: unable to initialise driver"); } } // Armed, Copter, PixHawk: // ins_periodic: 57500 events, 0 overruns, 208754us elapsed, 3us avg, min 1us max 218us 40.662us rms void AP_InertialSensor::periodic() { batchsampler.periodic(); } /* _calculate_trim - calculates the x and y trim angles. The accel_sample must be correctly scaled, offset and oriented for the board */ bool AP_InertialSensor::_calculate_trim(const Vector3f &accel_sample, float& trim_roll, float& trim_pitch) { trim_pitch = atan2f(accel_sample.x, norm(accel_sample.y, accel_sample.z)); trim_roll = atan2f(-accel_sample.y, -accel_sample.z); if (fabsf(trim_roll) > radians(10) || fabsf(trim_pitch) > radians(10)) { hal.console->printf("trim over maximum of 10 degrees\n"); return false; } hal.console->printf("Trim OK: roll=%.2f pitch=%.2f\n", (double)degrees(trim_roll), (double)degrees(trim_pitch)); return true; } void AP_InertialSensor::init_gyro() { _init_gyro(); // save calibration _save_gyro_calibration(); } // accelerometer clipping reporting uint32_t AP_InertialSensor::get_accel_clip_count(uint8_t instance) const { if (instance >= get_accel_count()) { return 0; } return _accel_clip_count[instance]; } // get_gyro_health_all - return true if all gyros are healthy bool AP_InertialSensor::get_gyro_health_all(void) const { for (uint8_t i=0; i 0); } // gyro_calibration_ok_all - returns true if all gyros were calibrated successfully bool AP_InertialSensor::gyro_calibrated_ok_all() const { for (uint8_t i=0; i 0); } // return true if gyro instance should be used (must be healthy and have it's use parameter set to 1) bool AP_InertialSensor::use_gyro(uint8_t instance) const { if (instance >= INS_MAX_INSTANCES) { return false; } return (get_gyro_health(instance) && _use[instance]); } // get_accel_health_all - return true if all accels are healthy bool AP_InertialSensor::get_accel_health_all(void) const { for (uint8_t i=0; i 0); } /* calculate the trim_roll and trim_pitch. This is used for redoing the trim without needing a full accel cal */ bool AP_InertialSensor::calibrate_trim(float &trim_roll, float &trim_pitch) { Vector3f level_sample; // exit immediately if calibration is already in progress if (_calibrating) { return false; } _calibrating = true; const uint8_t update_dt_milliseconds = (uint8_t)(1000.0f/get_sample_rate()+0.5f); // wait 100ms for ins filter to rise for (uint8_t k=0; k<100/update_dt_milliseconds; k++) { wait_for_sample(); update(); hal.scheduler->delay(update_dt_milliseconds); } uint32_t num_samples = 0; while (num_samples < 400/update_dt_milliseconds) { wait_for_sample(); // read samples from ins update(); // capture sample Vector3f samp; samp = get_accel(0); level_sample += samp; if (!get_accel_health(0)) { goto failed; } hal.scheduler->delay(update_dt_milliseconds); num_samples++; } level_sample /= num_samples; if (!_calculate_trim(level_sample, trim_roll, trim_pitch)) { goto failed; } _calibrating = false; return true; failed: _calibrating = false; return false; } /* check if the accelerometers are calibrated in 3D and that current number of accels matched number when calibrated */ bool AP_InertialSensor::accel_calibrated_ok_all() const { // calibration is not applicable for HIL mode if (_hil_mode) { return true; } // check each accelerometer has offsets saved for (uint8_t i=0; i= INS_MAX_INSTANCES) { return false; } return (get_accel_health(instance) && _use[instance]); } void AP_InertialSensor::_init_gyro() { uint8_t num_gyros = MIN(get_gyro_count(), INS_MAX_INSTANCES); Vector3f last_average[INS_MAX_INSTANCES], best_avg[INS_MAX_INSTANCES]; Vector3f new_gyro_offset[INS_MAX_INSTANCES]; float best_diff[INS_MAX_INSTANCES]; bool converged[INS_MAX_INSTANCES]; // exit immediately if calibration is already in progress if (_calibrating) { return; } // record we are calibrating _calibrating = true; // flash leds to tell user to keep the IMU still AP_Notify::flags.initialising = true; // cold start hal.console->printf("Init Gyro"); /* we do the gyro calibration with no board rotation. This avoids having to rotate readings during the calibration */ enum Rotation saved_orientation = _board_orientation; _board_orientation = ROTATION_NONE; // remove existing gyro offsets for (uint8_t k=0; kdelay(5); update(); } // the strategy is to average 50 points over 0.5 seconds, then do it // again and see if the 2nd average is within a small margin of // the first uint8_t num_converged = 0; // we try to get a good calibration estimate for up to 30 seconds // if the gyros are stable, we should get it in 1 second for (int16_t j = 0; j <= 30*4 && num_converged < num_gyros; j++) { Vector3f gyro_sum[INS_MAX_INSTANCES], gyro_avg[INS_MAX_INSTANCES], gyro_diff[INS_MAX_INSTANCES]; Vector3f accel_start; float diff_norm[INS_MAX_INSTANCES]; uint8_t i; memset(diff_norm, 0, sizeof(diff_norm)); hal.console->printf("*"); for (uint8_t k=0; kdelay(5); } Vector3f accel_diff = get_accel(0) - accel_start; if (accel_diff.length() > 0.2f) { // the accelerometers changed during the gyro sum. Skip // this sample. This copes with doing gyro cal on a // steadily moving platform. The value 0.2 corresponds // with around 5 degrees/second of rotation. continue; } for (uint8_t k=0; kprintf("\n"); for (uint8_t k=0; kprintf("gyro[%u] did not converge: diff=%f dps (expected < %f)\n", (unsigned)k, (double)ToDeg(best_diff[k]), (double)GYRO_INIT_MAX_DIFF_DPS); _gyro_offset[k] = best_avg[k]; // flag calibration as failed for this gyro _gyro_cal_ok[k] = false; } else { _gyro_cal_ok[k] = true; _gyro_offset[k] = new_gyro_offset[k]; } } // restore orientation _board_orientation = saved_orientation; // record calibration complete _calibrating = false; // stop flashing leds AP_Notify::flags.initialising = false; } // save parameters to eeprom void AP_InertialSensor::_save_gyro_calibration() { for (uint8_t i=0; i<_gyro_count; i++) { _gyro_offset[i].save(); _gyro_id[i].save(); } for (uint8_t i=_gyro_count; iupdate(); } // clear accumulators for (uint8_t i = 0; i < INS_MAX_INSTANCES; i++) { _delta_velocity_acc[i].zero(); _delta_velocity_acc_dt[i] = 0; _delta_angle_acc[i].zero(); _delta_angle_acc_dt[i] = 0; } if (!_startup_error_counts_set) { for (uint8_t i=0; i 2000) { _startup_error_counts_set = true; } } for (uint8_t i=0; i _gyro_startup_error_count[i] && have_zero_gyro_error_count) { // we prefer not to use a gyro that has had errors _gyro_healthy[i] = false; } if (_accel_healthy[i] && _accel_error_count[i] > _accel_startup_error_count[i] && have_zero_accel_error_count) { // we prefer not to use a accel that has had errors _accel_healthy[i] = false; } } // set primary to first healthy accel and gyro for (uint8_t i=0; idelay_microseconds_boost(wait_usec); uint32_t now2 = AP_HAL::micros(); if (now2+100 < _next_sample_usec) { timing_printf("shortsleep %u\n", (unsigned)(_next_sample_usec-now2)); } if (now2 > _next_sample_usec+400) { timing_printf("longsleep %u wait_usec=%u\n", (unsigned)(now2-_next_sample_usec), (unsigned)wait_usec); } _next_sample_usec += _sample_period_usec; } else if (now - _next_sample_usec < _sample_period_usec/8) { // we've overshot, but only by a small amount, keep on // schedule with no delay timing_printf("overshoot1 %u\n", (unsigned)(now-_next_sample_usec)); _next_sample_usec += _sample_period_usec; } else { // we've overshot by a larger amount, re-zero scheduling with // no delay timing_printf("overshoot2 %u\n", (unsigned)(now-_next_sample_usec)); _next_sample_usec = now + _sample_period_usec; } check_sample: if (!_hil_mode) { // we also wait for at least one backend to have a sample of both // accel and gyro. This normally completes immediately. bool gyro_available = false; bool accel_available = false; while (true) { for (uint8_t i=0; i<_backend_count; i++) { _backends[i]->accumulate(); } for (uint8_t i=0; idelay_microseconds(100); } } now = AP_HAL::micros(); if (_hil_mode && _hil.delta_time > 0) { _delta_time = _hil.delta_time; _hil.delta_time = 0; } else { _delta_time = (now - _last_sample_usec) * 1.0e-6f; } _last_sample_usec = now; #if 0 { static uint64_t delta_time_sum; static uint16_t counter; if (delta_time_sum == 0) { delta_time_sum = _sample_period_usec; } delta_time_sum += _delta_time * 1.0e6f; if (counter++ == 400) { counter = 0; hal.console->printf("now=%lu _delta_time_sum=%lu diff=%ld\n", (unsigned long)now, (unsigned long)delta_time_sum, (long)(now - delta_time_sum)); } } #endif _have_sample = true; } /* get delta angles */ bool AP_InertialSensor::get_delta_angle(uint8_t i, Vector3f &delta_angle) const { if (_delta_angle_valid[i]) { delta_angle = _delta_angle[i]; return true; } else if (get_gyro_health(i)) { // provide delta angle from raw gyro, so we use the same code // at higher level delta_angle = get_gyro(i) * get_delta_time(); return true; } return false; } /* get delta velocity if available */ bool AP_InertialSensor::get_delta_velocity(uint8_t i, Vector3f &delta_velocity) const { if (_delta_velocity_valid[i]) { delta_velocity = _delta_velocity[i]; return true; } else if (get_accel_health(i)) { delta_velocity = get_accel(i) * get_delta_time(); return true; } return false; } /* return delta_time for the delta_velocity */ float AP_InertialSensor::get_delta_velocity_dt(uint8_t i) const { float ret; if (_delta_velocity_valid[i]) { ret = _delta_velocity_dt[i]; } else { ret = get_delta_time(); } ret = MIN(ret, _loop_delta_t_max); return ret; } /* return delta_time for the delta_angle */ float AP_InertialSensor::get_delta_angle_dt(uint8_t i) const { float ret; if (_delta_angle_valid[i] && _delta_angle_dt[i] > 0) { ret = _delta_angle_dt[i]; } else { ret = get_delta_time(); } ret = MIN(ret, _loop_delta_t_max); return ret; } /* support for setting accel and gyro vectors, for use by HIL */ void AP_InertialSensor::set_accel(uint8_t instance, const Vector3f &accel) { if (_accel_count == 0) { // we haven't initialised yet return; } if (instance < INS_MAX_INSTANCES) { _accel[instance] = accel; _accel_healthy[instance] = true; if (_accel_count <= instance) { _accel_count = instance+1; } if (!_accel_healthy[_primary_accel]) { _primary_accel = instance; } } } void AP_InertialSensor::set_gyro(uint8_t instance, const Vector3f &gyro) { if (_gyro_count == 0) { // we haven't initialised yet return; } if (instance < INS_MAX_INSTANCES) { _gyro[instance] = gyro; _gyro_healthy[instance] = true; if (_gyro_count <= instance) { _gyro_count = instance+1; _gyro_cal_ok[instance] = true; } if (!_accel_healthy[_primary_accel]) { _primary_accel = instance; } } } /* set delta time for next ins.update() */ void AP_InertialSensor::set_delta_time(float delta_time) { _hil.delta_time = delta_time; } /* set delta velocity for next update */ void AP_InertialSensor::set_delta_velocity(uint8_t instance, float deltavt, const Vector3f &deltav) { if (instance < INS_MAX_INSTANCES) { _delta_velocity_valid[instance] = true; _delta_velocity[instance] = deltav; _delta_velocity_dt[instance] = deltavt; } } /* set delta angle for next update */ void AP_InertialSensor::set_delta_angle(uint8_t instance, const Vector3f &deltaa, float deltaat) { if (instance < INS_MAX_INSTANCES) { _delta_angle_valid[instance] = true; _delta_angle[instance] = deltaa; _delta_angle_dt[instance] = deltaat; } } /* * Get an AuxiliaryBus of N @instance of backend identified by @backend_id */ AuxiliaryBus *AP_InertialSensor::get_auxiliary_bus(int16_t backend_id, uint8_t instance) { detect_backends(); AP_InertialSensor_Backend *backend = _find_backend(backend_id, instance); if (backend == nullptr) { return nullptr; } return backend->get_auxiliary_bus(); } // calculate vibration levels and check for accelerometer clipping (called by a backends) void AP_InertialSensor::calc_vibration_and_clipping(uint8_t instance, const Vector3f &accel, float dt) { // check for clipping if (fabsf(accel.x) > AP_INERTIAL_SENSOR_ACCEL_CLIP_THRESH_MSS || fabsf(accel.y) > AP_INERTIAL_SENSOR_ACCEL_CLIP_THRESH_MSS || fabsf(accel.z) > AP_INERTIAL_SENSOR_ACCEL_CLIP_THRESH_MSS) { _accel_clip_count[instance]++; } // calculate vibration levels if (instance < INS_VIBRATION_CHECK_INSTANCES) { // filter accel at 5hz Vector3f accel_filt = _accel_vibe_floor_filter[instance].apply(accel, dt); // calc difference from this sample and 5hz filtered value, square and filter at 2hz Vector3f accel_diff = (accel - accel_filt); accel_diff.x *= accel_diff.x; accel_diff.y *= accel_diff.y; accel_diff.z *= accel_diff.z; _accel_vibe_filter[instance].apply(accel_diff, dt); } } // peak hold detector for slower mechanisms to detect spikes void AP_InertialSensor::set_accel_peak_hold(uint8_t instance, const Vector3f &accel) { if (instance != _primary_accel) { // we only record for primary accel return; } uint32_t now = AP_HAL::millis(); // negative x peak(min) hold detector if (accel.x < _peak_hold_state.accel_peak_hold_neg_x || _peak_hold_state.accel_peak_hold_neg_x_age <= now) { _peak_hold_state.accel_peak_hold_neg_x = accel.x; _peak_hold_state.accel_peak_hold_neg_x_age = now + AP_INERTIAL_SENSOR_ACCEL_PEAK_DETECT_TIMEOUT_MS; } } // retrieve latest calculated vibration levels Vector3f AP_InertialSensor::get_vibration_levels(uint8_t instance) const { Vector3f vibe; if (instance < INS_VIBRATION_CHECK_INSTANCES) { vibe = _accel_vibe_filter[instance].get(); vibe.x = safe_sqrt(vibe.x); vibe.y = safe_sqrt(vibe.y); vibe.z = safe_sqrt(vibe.z); } return vibe; } // check for vibration movement. Return true if all axis show nearly zero movement bool AP_InertialSensor::is_still() { Vector3f vibe = get_vibration_levels(); return (vibe.x < _still_threshold) && (vibe.y < _still_threshold) && (vibe.z < _still_threshold); } // initialise and register accel calibrator // called during the startup of accel cal void AP_InertialSensor::acal_init() { // NOTE: these objects are never deallocated because the pre-arm checks force a reboot if (_acal == nullptr) { _acal = new AP_AccelCal; } if (_accel_calibrator == nullptr) { _accel_calibrator = new AccelCalibrator[INS_MAX_INSTANCES]; } } // update accel calibrator void AP_InertialSensor::acal_update() { if(_acal == nullptr) { return; } _acal->update(); if (hal.util->get_soft_armed() && _acal->get_status() != ACCEL_CAL_NOT_STARTED) { _acal->cancel(); } } /* set and save accelerometer bias along with trim calculation */ void AP_InertialSensor::_acal_save_calibrations() { Vector3f bias, gain; for (uint8_t i=0; i<_accel_count; i++) { if (_accel_calibrator[i].get_status() == ACCEL_CAL_SUCCESS) { _accel_calibrator[i].get_calibration(bias, gain); _accel_offset[i].set_and_save(bias); _accel_scale[i].set_and_save(gain); _accel_id[i].save(); _accel_id_ok[i] = true; } else { _accel_offset[i].set_and_save(Vector3f()); _accel_scale[i].set_and_save(Vector3f()); } } // clear any unused accels for (uint8_t i=_accel_count; i radians(10) || fabsf(_trim_pitch) > radians(10)) { hal.console->printf("ERR: Trim over maximum of 10 degrees!!"); _new_trim = false; //we have either got faulty level during acal or highly misaligned accelerometers } _accel_cal_requires_reboot = true; } void AP_InertialSensor::_acal_event_failure() { for (uint8_t i=0; i<_accel_count; i++) { _accel_offset[i].set_and_notify(Vector3f(0,0,0)); _accel_scale[i].set_and_notify(Vector3f(1,1,1)); } } /* Returns true if new valid trim values are available and passes them to reference vars */ bool AP_InertialSensor::get_new_trim(float& trim_roll, float &trim_pitch) { if (_new_trim) { trim_roll = _trim_roll; trim_pitch = _trim_pitch; _new_trim = false; return true; } return false; } /* Returns body fixed accelerometer level data averaged during accel calibration's first step */ bool AP_InertialSensor::get_fixed_mount_accel_cal_sample(uint8_t sample_num, Vector3f& ret) const { if (_accel_count <= (_acc_body_aligned-1) || _accel_calibrator[2].get_status() != ACCEL_CAL_SUCCESS || sample_num>=_accel_calibrator[2].get_num_samples_collected()) { return false; } _accel_calibrator[_acc_body_aligned-1].get_sample_corrected(sample_num, ret); if (_board_orientation == ROTATION_CUSTOM && _custom_rotation) { ret = *_custom_rotation * ret; } else { ret.rotate(_board_orientation); } return true; } /* Returns Primary accelerometer level data averaged during accel calibration's first step */ bool AP_InertialSensor::get_primary_accel_cal_sample_avg(uint8_t sample_num, Vector3f& ret) const { uint8_t count = 0; Vector3f avg = Vector3f(0,0,0); for (uint8_t i=0; i=_accel_calibrator[i].get_num_samples_collected()) { continue; } Vector3f sample; _accel_calibrator[i].get_sample_corrected(sample_num, sample); avg += sample; count++; } if (count == 0) { return false; } avg /= count; ret = avg; if (_board_orientation == ROTATION_CUSTOM && _custom_rotation) { ret = *_custom_rotation * ret; } else { ret.rotate(_board_orientation); } return true; } /* perform a simple 1D accel calibration, returning mavlink result code */ MAV_RESULT AP_InertialSensor::simple_accel_cal() { uint8_t num_accels = MIN(get_accel_count(), INS_MAX_INSTANCES); Vector3f last_average[INS_MAX_INSTANCES]; Vector3f new_accel_offset[INS_MAX_INSTANCES]; Vector3f saved_offsets[INS_MAX_INSTANCES]; Vector3f saved_scaling[INS_MAX_INSTANCES]; bool converged[INS_MAX_INSTANCES]; const float accel_convergence_limit = 0.05; Vector3f rotated_gravity(0, 0, -GRAVITY_MSS); // exit immediately if calibration is already in progress if (_calibrating) { return MAV_RESULT_TEMPORARILY_REJECTED; } // record we are calibrating _calibrating = true; // flash leds to tell user to keep the IMU still AP_Notify::flags.initialising = true; hal.console->printf("Simple accel cal"); /* we do the accel calibration with no board rotation. This avoids having to rotate readings during the calibration */ enum Rotation saved_orientation = _board_orientation; _board_orientation = ROTATION_NONE; // get the rotated gravity vector which will need to be applied to the offsets rotated_gravity.rotate_inverse(saved_orientation); // save existing accel offsets for (uint8_t k=0; kdelay(5); update(); } // the strategy is to average 50 points over 0.5 seconds, then do it // again and see if the 2nd average is within a small margin of // the first uint8_t num_converged = 0; // we try to get a good calibration estimate for up to 10 seconds // if the accels are stable, we should get it in 1 second for (int16_t j = 0; j <= 10*4 && num_converged < num_accels; j++) { Vector3f accel_sum[INS_MAX_INSTANCES], accel_avg[INS_MAX_INSTANCES], accel_diff[INS_MAX_INSTANCES]; float diff_norm[INS_MAX_INSTANCES]; uint8_t i; memset(diff_norm, 0, sizeof(diff_norm)); hal.console->printf("*"); for (uint8_t k=0; kdelay(5); } for (uint8_t k=0; k 0 && diff_norm[k] < accel_convergence_limit) { last_average[k] = (accel_avg[k] * 0.5f) + (last_average[k] * 0.5f); if (!converged[k] || last_average[k].length() < new_accel_offset[k].length()) { new_accel_offset[k] = last_average[k]; } if (!converged[k]) { converged[k] = true; num_converged++; } } else { last_average[k] = accel_avg[k]; } } } MAV_RESULT result = MAV_RESULT_ACCEPTED; // see if we've passed for (uint8_t k=0; kprintf("\nPASSED\n"); for (uint8_t k=0; kprintf("\nFAILED\n"); // restore old values for (uint8_t k=0; k