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https://gitee.com/mirrors_PX4/PX4-Autopilot.git
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apply differential pressure calibration (SENS_DPRES_OFF) centrally
- remove drv_airspeed.h and ioctls
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@@ -150,9 +150,6 @@ ETSAirspeed::collect()
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diff_pres_pa_raw = 0.001f * (report.timestamp & 0x01);
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}
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// The raw value still should be compensated for the known offset
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diff_pres_pa_raw -= _diff_pres_offset;
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report.error_count = perf_event_count(_comms_errors);
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// XXX we may want to smooth out the readings to remove noise.
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@@ -212,8 +212,8 @@ MEASAirspeed::collect()
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report.error_count = perf_event_count(_comms_errors);
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report.temperature = temperature;
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report.differential_pressure_filtered_pa = _filter.apply(diff_press_pa_raw) - _diff_pres_offset;
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report.differential_pressure_raw_pa = diff_press_pa_raw - _diff_pres_offset;
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report.differential_pressure_filtered_pa = _filter.apply(diff_press_pa_raw);
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report.differential_pressure_raw_pa = diff_press_pa_raw;
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report.device_id = _device_id.devid;
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report.timestamp = hrt_absolute_time();
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@@ -265,8 +265,8 @@ MS5525::collect()
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differential_pressure_s diff_pressure{};
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diff_pressure.error_count = perf_event_count(_comms_errors);
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diff_pressure.differential_pressure_raw_pa = diff_press_pa_raw - _diff_pres_offset;
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diff_pressure.differential_pressure_filtered_pa = _filter.apply(diff_press_pa_raw) - _diff_pres_offset;
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diff_pressure.differential_pressure_raw_pa = diff_press_pa_raw;
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diff_pressure.differential_pressure_filtered_pa = _filter.apply(diff_press_pa_raw);
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diff_pressure.temperature = temperature_c;
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diff_pressure.device_id = _device_id.devid;
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diff_pressure.timestamp = hrt_absolute_time();
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@@ -172,8 +172,8 @@ SDP3X::collect()
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report.error_count = perf_event_count(_comms_errors);
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report.temperature = temperature_c;
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report.differential_pressure_filtered_pa = _filter.apply(diff_press_pa_raw) - _diff_pres_offset;
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report.differential_pressure_raw_pa = diff_press_pa_raw - _diff_pres_offset;
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report.differential_pressure_filtered_pa = _filter.apply(diff_press_pa_raw);
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report.differential_pressure_raw_pa = diff_press_pa_raw;
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report.device_id = _device_id.devid;
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report.timestamp = hrt_absolute_time();
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@@ -1,72 +0,0 @@
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/****************************************************************************
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*
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* Copyright (C) 2013 PX4 Development Team. All rights reserved.
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*
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* Redistribution and use in source and binary forms, with or without
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* modification, are permitted provided that the following conditions
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* are met:
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*
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* 1. Redistributions of source code must retain the above copyright
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* notice, this list of conditions and the following disclaimer.
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* 2. Redistributions in binary form must reproduce the above copyright
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* notice, this list of conditions and the following disclaimer in
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* the documentation and/or other materials provided with the
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* distribution.
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* 3. Neither the name PX4 nor the names of its contributors may be
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* used to endorse or promote products derived from this software
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* without specific prior written permission.
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*
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* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
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* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
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* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
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* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
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* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
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* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
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* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
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* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
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* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
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* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
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* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
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* POSSIBILITY OF SUCH DAMAGE.
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*
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****************************************************************************/
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/**
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* @file drv_airspeed.h
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*
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* Airspeed driver interface.
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*
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* @author Simon Wilks
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*/
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#ifndef _DRV_AIRSPEED_H
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#define _DRV_AIRSPEED_H
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#include <stdint.h>
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#include <sys/ioctl.h>
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#include "drv_sensor.h"
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#include "drv_orb_dev.h"
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#define AIRSPEED_BASE_DEVICE_PATH "/dev/airspeed"
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#define AIRSPEED0_DEVICE_PATH "/dev/airspeed0"
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/*
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* ioctl() definitions
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*
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* Airspeed drivers also implement the generic sensor driver
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* interfaces from drv_sensor.h
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*/
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#define _AIRSPEEDIOCBASE (0x7700)
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#define __AIRSPEEDIOC(_n) (_PX4_IOC(_AIRSPEEDIOCBASE, _n))
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#define AIRSPEEDIOCSSCALE __AIRSPEEDIOC(0)
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/** airspeed scaling factors; out = (in * Vscale) + offset */
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struct airspeed_scale {
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float offset_pa;
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float scale;
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};
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#endif /* _DRV_AIRSPEED_H */
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@@ -38,7 +38,6 @@
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#pragma once
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#include "sensor_bridge.hpp"
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#include <drivers/drv_airspeed.h>
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#include <uORB/topics/airspeed.h>
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#include <uavcan/equipment/air_data/IndicatedAirspeed.hpp>
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@@ -37,7 +37,6 @@
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#include "differential_pressure.hpp"
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#include <drivers/drv_airspeed.h>
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#include <drivers/drv_hrt.h>
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#include <lib/geo/geo.h>
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#include <parameters/param.h>
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@@ -53,9 +52,6 @@ UavcanDifferentialPressureBridge::UavcanDifferentialPressureBridge(uavcan::INode
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int UavcanDifferentialPressureBridge::init()
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{
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// Initialize the calibration offset
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param_get(param_find("SENS_DPRES_OFF"), &_diff_pres_offset);
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int res = _sub_air.start(AirCbBinder(this, &UavcanDifferentialPressureBridge::air_sub_cb));
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if (res < 0) {
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@@ -78,8 +74,8 @@ void UavcanDifferentialPressureBridge::air_sub_cb(const
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if (PX4_ISFINITE(diff_press_pa)) {
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differential_pressure_s report{};
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report.differential_pressure_raw_pa = diff_press_pa - _diff_pres_offset;
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report.differential_pressure_filtered_pa = _filter.apply(diff_press_pa) - _diff_pres_offset;
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report.differential_pressure_raw_pa = diff_press_pa;
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report.differential_pressure_filtered_pa = _filter.apply(diff_press_pa);
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report.temperature = temperature_c;
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report.device_id = _device_id.devid;
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report.timestamp = hrt_absolute_time();
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@@ -37,9 +37,8 @@
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#pragma once
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#include <uORB/uORB.h>
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#include <uORB/topics/differential_pressure.h>
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#include <mathlib/math/filter/LowPassFilter2p.hpp>
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#include <uORB/topics/differential_pressure.h>
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#include "sensor_bridge.hpp"
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@@ -57,8 +56,6 @@ public:
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int init() override;
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private:
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float _diff_pres_offset{0.f};
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math::LowPassFilter2p<float> _filter{10.f, 1.1f}; /// Adapted from MS5525 driver
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void air_sub_cb(const uavcan::ReceivedDataStructure<uavcan::equipment::air_data::RawAirData> &msg);
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