mirror of https://github.com/ArduPilot/ardupilot
AP_InertialSensor: converted flymaple driver to new API
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@ -316,6 +316,8 @@ AP_InertialSensor::_detect_backends(Sample_rate sample_rate)
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_backends[0] = AP_InertialSensor_Oilpan::detect(*this, sample_rate);
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#elif HAL_INS_DEFAULT == HAL_INS_MPU9250
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_backends[0] = AP_InertialSensor_MPU9250::detect(*this, sample_rate);
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#elif HAL_INS_DEFAULT == HAL_INS_FLYMAPLE
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_backends[0] = AP_InertialSensor_Flymaple::detect(*this, sample_rate);
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#else
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#error Unrecognised HAL_INS_TYPE setting
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#endif
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@ -277,6 +277,7 @@ private:
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#include "AP_InertialSensor_Oilpan.h"
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#include "AP_InertialSensor_MPU9250.h"
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#include "AP_InertialSensor_L3G4200D.h"
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#include "AP_InertialSensor_Flymaple.h"
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#include "AP_InertialSensor_HIL.h"
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#include "AP_InertialSensor_UserInteract_Stream.h"
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#include "AP_InertialSensor_UserInteract_MAVLink.h"
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@ -14,7 +14,7 @@
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along with this program. If not, see <http://www.gnu.org/licenses/>.
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*/
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/*
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Flymaple port by Mike McCauley
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Flymaple IMU driver by Mike McCauley
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*/
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// Interface to the Flymaple sensors:
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@ -28,20 +28,6 @@
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const extern AP_HAL::HAL& hal;
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/// Statics
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Vector3f AP_InertialSensor_Flymaple::_accel_filtered;
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uint32_t AP_InertialSensor_Flymaple::_accel_samples;
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Vector3f AP_InertialSensor_Flymaple::_gyro_filtered;
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uint32_t AP_InertialSensor_Flymaple::_gyro_samples;
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uint64_t AP_InertialSensor_Flymaple::_last_accel_timestamp;
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uint64_t AP_InertialSensor_Flymaple::_last_gyro_timestamp;
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LowPassFilter2p AP_InertialSensor_Flymaple::_accel_filter_x(800, 10);
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LowPassFilter2p AP_InertialSensor_Flymaple::_accel_filter_y(800, 10);
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LowPassFilter2p AP_InertialSensor_Flymaple::_accel_filter_z(800, 10);
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LowPassFilter2p AP_InertialSensor_Flymaple::_gyro_filter_x(800, 10);
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LowPassFilter2p AP_InertialSensor_Flymaple::_gyro_filter_y(800, 10);
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LowPassFilter2p AP_InertialSensor_Flymaple::_gyro_filter_z(800, 10);
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// This is how often we wish to make raw samples of the sensors in Hz
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const uint32_t raw_sample_rate_hz = 800;
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// And the equivalent time between samples in microseconds
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@ -77,24 +63,56 @@ const uint32_t raw_sample_interval_us = (1000000 / raw_sample_rate_hz);
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// Result wil be radians/sec
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#define FLYMAPLE_GYRO_SCALE_R_S (1.0f / 14.375f) * (3.1415926f / 180.0f)
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uint16_t AP_InertialSensor_Flymaple::_init_sensor( Sample_rate sample_rate )
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AP_InertialSensor_Flymaple::AP_InertialSensor_Flymaple(AP_InertialSensor &imu) :
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AP_InertialSensor_Backend(imu),
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_have_gyro_sample(false),
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_have_accel_sample(false),
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_accel_filter_x(raw_sample_rate_hz, 10),
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_accel_filter_y(raw_sample_rate_hz, 10),
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_accel_filter_z(raw_sample_rate_hz, 10),
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_gyro_filter_x(raw_sample_rate_hz, 10),
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_gyro_filter_y(raw_sample_rate_hz, 10),
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_gyro_filter_z(raw_sample_rate_hz, 10),
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_last_gyro_timestamp(0),
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_last_accel_timestamp(0)
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{}
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/*
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detect the sensor
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*/
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AP_InertialSensor_Backend *AP_InertialSensor_Flymaple::detect(AP_InertialSensor &_imu,
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AP_InertialSensor::Sample_rate sample_rate)
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{
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AP_InertialSensor_Flymaple *sensor = new AP_InertialSensor_Flymaple(_imu);
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if (sensor == NULL) {
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return NULL;
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}
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if (!sensor->_init_sensor(sample_rate)) {
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delete sensor;
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return NULL;
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}
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return sensor;
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}
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bool AP_InertialSensor_Flymaple::_init_sensor(AP_InertialSensor::Sample_rate sample_rate)
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{
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// Sensors are raw sampled at 800Hz.
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// Here we figure the divider to get the rate that update should be called
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switch (sample_rate) {
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case RATE_50HZ:
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_sample_divider = raw_sample_rate_hz / 50;
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case AP_InertialSensor::RATE_50HZ:
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_default_filter_hz = 10;
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break;
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case RATE_100HZ:
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_sample_divider = raw_sample_rate_hz / 100;
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case AP_InertialSensor::RATE_100HZ:
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_default_filter_hz = 20;
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break;
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case RATE_200HZ:
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case AP_InertialSensor::RATE_200HZ:
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_default_filter_hz = 20;
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break;
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case AP_InertialSensor::RATE_400HZ:
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_default_filter_hz = 30;
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break;
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default:
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_sample_divider = raw_sample_rate_hz / 200;
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_default_filter_hz = 20;
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break;
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return false;
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}
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// get pointer to i2c bus semaphore
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@ -146,12 +164,15 @@ uint16_t AP_InertialSensor_Flymaple::_init_sensor( Sample_rate sample_rate )
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hal.scheduler->delay(1);
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// Set up the filter desired
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_set_filter_frequency(_mpu6000_filter);
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_set_filter_frequency(_imu.get_filter());
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// give back i2c semaphore
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// give back i2c semaphore
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i2c_sem->give();
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return AP_PRODUCT_ID_FLYMAPLE;
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_gyro_instance = _imu.register_gyro();
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_accel_instance = _imu.register_accel();
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return true;
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}
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/*
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@ -170,109 +191,47 @@ void AP_InertialSensor_Flymaple::_set_filter_frequency(uint8_t filter_hz)
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_gyro_filter_z.set_cutoff_frequency(raw_sample_rate_hz, filter_hz);
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}
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/*================ AP_INERTIALSENSOR PUBLIC INTERFACE ==================== */
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// This takes about 20us to run
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bool AP_InertialSensor_Flymaple::update(void)
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{
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if (!wait_for_sample(100)) {
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return false;
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}
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Vector3f accel_scale = _accel_scale[0].get();
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Vector3f accel, gyro;
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uint32_t now = hal.scheduler->micros();
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// Not really needed since Flymaple _accumulate runs in the main thread
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hal.scheduler->suspend_timer_procs();
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// base the time on the gyro timestamp, as that is what is
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// multiplied by time to integrate in DCM
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_delta_time = (_last_gyro_timestamp - _last_update_usec) * 1.0e-6f;
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_last_update_usec = _last_gyro_timestamp;
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_previous_accel[0] = _accel[0];
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_accel[0] = _accel_filtered;
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_accel_samples = 0;
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_gyro[0] = _gyro_filtered;
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_gyro_samples = 0;
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accel = _accel_filtered;
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gyro = _gyro_filtered;
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_have_gyro_sample = false;
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_have_accel_sample = false;
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hal.scheduler->resume_timer_procs();
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// add offsets and rotation
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_accel[0].rotate(_board_orientation);
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// Adjust for chip scaling to get m/s/s
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_accel[0] *= FLYMAPLE_ACCELEROMETER_SCALE_M_S;
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// Now the calibration scale factor
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_accel[0].x *= accel_scale.x;
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_accel[0].y *= accel_scale.y;
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_accel[0].z *= accel_scale.z;
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_accel[0] -= _accel_offset[0];
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_gyro[0].rotate(_board_orientation);
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accel *= FLYMAPLE_ACCELEROMETER_SCALE_M_S;
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_rotate_and_offset_accel(_accel_instance, accel, now);
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// Adjust for chip scaling to get radians/sec
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_gyro[0] *= FLYMAPLE_GYRO_SCALE_R_S;
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_gyro[0] -= _gyro_offset[0];
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gyro *= FLYMAPLE_GYRO_SCALE_R_S;
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_rotate_and_offset_gyro(_gyro_instance, gyro, now);
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if (_last_filter_hz != _mpu6000_filter) {
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_set_filter_frequency(_mpu6000_filter);
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_last_filter_hz = _mpu6000_filter;
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if (_last_filter_hz != _imu.get_filter()) {
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_set_filter_frequency(_imu.get_filter());
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_last_filter_hz = _imu.get_filter();
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}
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return true;
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}
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bool AP_InertialSensor_Flymaple::get_gyro_health(void) const
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{
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if (_last_gyro_timestamp == 0) {
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// not initialised yet, show as healthy to prevent scary GCS
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// warnings
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return true;
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}
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uint64_t now = hal.scheduler->micros();
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if ((now - _last_gyro_timestamp) >= (2 * raw_sample_interval_us)) {
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// gyros have not updated
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return false;
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}
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return true;
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}
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bool AP_InertialSensor_Flymaple::get_accel_health(void) const
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{
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if (_last_accel_timestamp == 0) {
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// not initialised yet, show as healthy to prevent scary GCS
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// warnings
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return true;
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}
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uint64_t now = hal.scheduler->micros();
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if ((now - _last_accel_timestamp) >= (2 * raw_sample_interval_us)) {
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// gyros have not updated
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return false;
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}
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return true;
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}
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float AP_InertialSensor_Flymaple::get_delta_time(void) const
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{
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return _delta_time;
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}
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float AP_InertialSensor_Flymaple::get_gyro_drift_rate(void)
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{
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// Dont really know this for the ITG-3200.
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// 0.5 degrees/second/minute
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return ToRad(0.5/60);
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}
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// This needs to get called as often as possible.
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// Its job is to accumulate samples as fast as is reasonable for the accel and gyro
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// sensors.
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// Cant call this from within the system timers, since the long I2C reads (up to 1ms)
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// with interrupts disabled breaks lots of things
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// Therefore must call this as often as possible from
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// within the mainline and thropttle the reads here to suit the sensors
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// Note that this is called from gyro_sample_available() and
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// accel_sample_available(), which is really not good enough for
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// 800Hz, as it is common for the main loop to take more than 1.5ms
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// before wait_for_sample() is called again. We can't just call this
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// from a timer as timers run with interrupts disabled, and the I2C
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// operations take too long
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// So we are stuck with a suboptimal solution. The results are not so
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// good in terms of timing. It may be better with the FIFOs enabled
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void AP_InertialSensor_Flymaple::_accumulate(void)
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{
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// get pointer to i2c bus semaphore
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@ -285,7 +244,7 @@ void AP_InertialSensor_Flymaple::_accumulate(void)
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// Read accelerometer
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// ADXL345 is in the default FIFO bypass mode, so the FIFO is not used
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uint8_t buffer[6];
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uint64_t now = hal.scheduler->micros();
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uint32_t now = hal.scheduler->micros();
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// This takes about 250us at 400kHz I2C speed
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if ((now - _last_accel_timestamp) >= raw_sample_interval_us
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&& hal.i2c->readRegisters(FLYMAPLE_ACCELEROMETER_ADDRESS, FLYMAPLE_ACCELEROMETER_ADXLREG_DATAX0, 6, buffer) == 0)
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@ -300,7 +259,7 @@ void AP_InertialSensor_Flymaple::_accumulate(void)
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_accel_filtered = Vector3f(_accel_filter_x.apply(x),
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_accel_filter_y.apply(y),
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_accel_filter_z.apply(z));
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_accel_samples++;
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_have_accel_sample = true;
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_last_accel_timestamp = now;
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}
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@ -317,7 +276,7 @@ void AP_InertialSensor_Flymaple::_accumulate(void)
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_gyro_filtered = Vector3f(_gyro_filter_x.apply(x),
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_gyro_filter_y.apply(y),
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_gyro_filter_z.apply(z));
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_gyro_samples++;
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_have_gyro_sample = true;
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_last_gyro_timestamp = now;
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}
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@ -325,26 +284,4 @@ void AP_InertialSensor_Flymaple::_accumulate(void)
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i2c_sem->give();
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}
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bool AP_InertialSensor_Flymaple::_sample_available(void)
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{
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_accumulate();
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return min(_accel_samples, _gyro_samples) / _sample_divider > 0;
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}
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bool AP_InertialSensor_Flymaple::wait_for_sample(uint16_t timeout_ms)
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{
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if (_sample_available()) {
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return true;
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}
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uint32_t start = hal.scheduler->millis();
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while ((hal.scheduler->millis() - start) < timeout_ms) {
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hal.scheduler->delay_microseconds(100);
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if (_sample_available()) {
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return true;
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}
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}
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return false;
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}
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#endif // CONFIG_HAL_BOARD
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@ -6,39 +6,32 @@
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#include <AP_HAL.h>
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#if CONFIG_HAL_BOARD == HAL_BOARD_FLYMAPLE
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#include <AP_Progmem.h>
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#include "AP_InertialSensor.h"
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#include <Filter.h>
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#include <LowPassFilter2p.h>
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class AP_InertialSensor_Flymaple : public AP_InertialSensor
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class AP_InertialSensor_Flymaple : public AP_InertialSensor_Backend
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{
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public:
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AP_InertialSensor_Flymaple(AP_InertialSensor &imu);
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AP_InertialSensor_Flymaple() : AP_InertialSensor() {}
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/* update accel and gyro state */
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bool update();
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/* Concrete implementation of AP_InertialSensor functions: */
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bool update();
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float get_delta_time() const;
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float get_gyro_drift_rate();
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bool wait_for_sample(uint16_t timeout_ms);
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bool get_gyro_health(void) const;
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bool get_accel_health(void) const;
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bool healthy(void) const { return get_gyro_health() && get_accel_health(); }
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bool gyro_sample_available(void) { _accumulate(); return _have_gyro_sample; }
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bool accel_sample_available(void) { _accumulate(); return _have_accel_sample; }
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// detect the sensor
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static AP_InertialSensor_Backend *detect(AP_InertialSensor &imu,
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AP_InertialSensor::Sample_rate sample_rate);
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private:
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uint16_t _init_sensor( Sample_rate sample_rate );
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static void _accumulate(void);
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bool _sample_available();
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uint64_t _last_update_usec;
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float _delta_time;
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static Vector3f _accel_filtered;
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static uint32_t _accel_samples;
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static Vector3f _gyro_filtered;
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static uint32_t _gyro_samples;
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static uint64_t _last_accel_timestamp;
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static uint64_t _last_gyro_timestamp;
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uint8_t _sample_divider;
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bool _init_sensor(AP_InertialSensor::Sample_rate sample_rate);
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void _accumulate(void);
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Vector3f _accel_filtered;
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Vector3f _gyro_filtered;
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bool _have_gyro_sample;
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bool _have_accel_sample;
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// support for updating filter at runtime
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uint8_t _last_filter_hz;
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void _set_filter_frequency(uint8_t filter_hz);
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// Low Pass filters for gyro and accel
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static LowPassFilter2p _accel_filter_x;
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static LowPassFilter2p _accel_filter_y;
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static LowPassFilter2p _accel_filter_z;
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static LowPassFilter2p _gyro_filter_x;
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static LowPassFilter2p _gyro_filter_y;
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static LowPassFilter2p _gyro_filter_z;
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LowPassFilter2p _accel_filter_x;
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LowPassFilter2p _accel_filter_y;
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LowPassFilter2p _accel_filter_z;
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LowPassFilter2p _gyro_filter_x;
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LowPassFilter2p _gyro_filter_y;
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LowPassFilter2p _gyro_filter_z;
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uint8_t _gyro_instance;
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uint8_t _accel_instance;
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uint32_t _last_gyro_timestamp;
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uint32_t _last_accel_timestamp;
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};
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#endif
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#endif // __AP_INERTIAL_SENSOR_FLYMAPLE_H__
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