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voted_sensors_update: refactor out matrix:: because of using namespace
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@ -133,10 +133,10 @@ void VotedSensorsUpdate::deinit()
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void VotedSensorsUpdate::parameters_update()
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{
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/* fine tune board offset */
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matrix::Dcmf board_rotation_offset = matrix::Eulerf(
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M_DEG_TO_RAD_F * _parameters.board_offset[0],
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M_DEG_TO_RAD_F * _parameters.board_offset[1],
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M_DEG_TO_RAD_F * _parameters.board_offset[2]);
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Dcmf board_rotation_offset = Eulerf(
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M_DEG_TO_RAD_F * _parameters.board_offset[0],
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M_DEG_TO_RAD_F * _parameters.board_offset[1],
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M_DEG_TO_RAD_F * _parameters.board_offset[2]);
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_board_rotation = board_rotation_offset * get_rot_matrix((enum Rotation)_parameters.board_rotation);
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@ -557,7 +557,7 @@ void VotedSensorsUpdate::accel_poll(struct sensor_combined_s &raw)
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_accel_device_id[uorb_index] = accel_report.device_id;
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matrix::Vector3f accel_data;
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Vector3f accel_data;
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if (accel_report.integral_dt != 0) {
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/*
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@ -569,9 +569,9 @@ void VotedSensorsUpdate::accel_poll(struct sensor_combined_s &raw)
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// convert the delta velocities to an equivalent acceleration before application of corrections
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float dt_inv = 1.e6f / accel_report.integral_dt;
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accel_data = matrix::Vector3f(accel_report.x_integral * dt_inv,
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accel_report.y_integral * dt_inv,
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accel_report.z_integral * dt_inv);
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accel_data = Vector3f(accel_report.x_integral * dt_inv,
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accel_report.y_integral * dt_inv,
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accel_report.z_integral * dt_inv);
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_last_sensor_data[uorb_index].accelerometer_integral_dt = accel_report.integral_dt;
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@ -580,7 +580,7 @@ void VotedSensorsUpdate::accel_poll(struct sensor_combined_s &raw)
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// Correct each sensor for temperature effects
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// Filtering and/or downsampling of temperature should be performed in the driver layer
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accel_data = matrix::Vector3f(accel_report.x, accel_report.y, accel_report.z);
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accel_data = Vector3f(accel_report.x, accel_report.y, accel_report.z);
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// handle the cse where this is our first output
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if (_last_accel_timestamp[uorb_index] == 0) {
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@ -664,7 +664,7 @@ void VotedSensorsUpdate::gyro_poll(struct sensor_combined_s &raw)
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_gyro_device_id[uorb_index] = gyro_report.device_id;
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matrix::Vector3f gyro_rate;
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Vector3f gyro_rate;
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if (gyro_report.integral_dt != 0) {
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/*
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@ -676,9 +676,9 @@ void VotedSensorsUpdate::gyro_poll(struct sensor_combined_s &raw)
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// convert the delta angles to an equivalent angular rate before application of corrections
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float dt_inv = 1.e6f / gyro_report.integral_dt;
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gyro_rate = matrix::Vector3f(gyro_report.x_integral * dt_inv,
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gyro_report.y_integral * dt_inv,
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gyro_report.z_integral * dt_inv);
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gyro_rate = Vector3f(gyro_report.x_integral * dt_inv,
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gyro_report.y_integral * dt_inv,
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gyro_report.z_integral * dt_inv);
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_last_sensor_data[uorb_index].gyro_integral_dt = gyro_report.integral_dt;
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@ -687,7 +687,7 @@ void VotedSensorsUpdate::gyro_poll(struct sensor_combined_s &raw)
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// Correct each sensor for temperature effects
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// Filtering and/or downsampling of temperature should be performed in the driver layer
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gyro_rate = matrix::Vector3f(gyro_report.x, gyro_report.y, gyro_report.z);
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gyro_rate = Vector3f(gyro_report.x, gyro_report.y, gyro_report.z);
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// handle the case where this is our first output
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if (_last_sensor_data[uorb_index].timestamp == 0) {
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@ -770,7 +770,7 @@ void VotedSensorsUpdate::mag_poll(vehicle_magnetometer_s &magnetometer)
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parameters_update();
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}
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matrix::Vector3f vect(mag_report.x, mag_report.y, mag_report.z);
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Vector3f vect(mag_report.x, mag_report.y, mag_report.z);
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vect = _mag_rotation[uorb_index] * vect;
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_last_magnetometer[uorb_index].timestamp = mag_report.timestamp;
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@ -834,7 +834,7 @@ void VotedSensorsUpdate::baro_poll(vehicle_air_data_s &airdata)
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_baro_device_id[uorb_index] = baro_report.device_id;
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got_update = true;
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matrix::Vector3f vect(baro_report.pressure, baro_report.temperature, 0.f);
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Vector3f vect(baro_report.pressure, baro_report.temperature, 0.f);
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_last_airdata[uorb_index].timestamp = baro_report.timestamp;
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_last_airdata[uorb_index].baro_temp_celcius = baro_report.temperature;
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