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airspeed sensors often need to be on longer cables due to having to be outside the prop wash.
408 lines
9.6 KiB
C++
408 lines
9.6 KiB
C++
/****************************************************************************
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*
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* Copyright (c) 2013, 2014 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 ets_airspeed.cpp
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* @author Simon Wilks
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*
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* Driver for the Eagle Tree Airspeed V3 connected via I2C.
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*/
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#include <nuttx/config.h>
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#include <drivers/device/i2c.h>
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#include <sys/types.h>
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#include <stdint.h>
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#include <stdlib.h>
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#include <stdbool.h>
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#include <semaphore.h>
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#include <string.h>
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#include <fcntl.h>
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#include <poll.h>
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#include <errno.h>
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#include <stdio.h>
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#include <math.h>
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#include <unistd.h>
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#include <nuttx/arch.h>
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#include <nuttx/wqueue.h>
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#include <nuttx/clock.h>
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#include <arch/board/board.h>
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#include <systemlib/airspeed.h>
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#include <systemlib/err.h>
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#include <systemlib/param/param.h>
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#include <systemlib/perf_counter.h>
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#include <drivers/drv_airspeed.h>
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#include <drivers/drv_hrt.h>
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#include <drivers/device/ringbuffer.h>
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#include <uORB/uORB.h>
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#include <uORB/topics/differential_pressure.h>
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#include <uORB/topics/subsystem_info.h>
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#include <drivers/airspeed/airspeed.h>
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Airspeed::Airspeed(int bus, int address, unsigned conversion_interval, const char* path) :
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I2C("Airspeed", path, bus, address, 100000),
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_reports(nullptr),
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_buffer_overflows(perf_alloc(PC_COUNT, "airspeed_buffer_overflows")),
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_max_differential_pressure_pa(0),
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_sensor_ok(false),
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_last_published_sensor_ok(true), /* initialize differently to force publication */
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_measure_ticks(0),
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_collect_phase(false),
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_diff_pres_offset(0.0f),
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_airspeed_pub(-1),
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_subsys_pub(-1),
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_class_instance(-1),
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_conversion_interval(conversion_interval),
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_sample_perf(perf_alloc(PC_ELAPSED, "airspeed_read")),
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_comms_errors(perf_alloc(PC_COUNT, "airspeed_comms_errors"))
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{
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// enable debug() calls
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_debug_enabled = false;
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// work_cancel in the dtor will explode if we don't do this...
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memset(&_work, 0, sizeof(_work));
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}
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Airspeed::~Airspeed()
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{
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/* make sure we are truly inactive */
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stop();
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if (_class_instance != -1)
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unregister_class_devname(AIRSPEED_DEVICE_PATH, _class_instance);
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/* free any existing reports */
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if (_reports != nullptr)
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delete _reports;
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// free perf counters
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perf_free(_sample_perf);
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perf_free(_comms_errors);
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perf_free(_buffer_overflows);
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}
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int
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Airspeed::init()
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{
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int ret = ERROR;
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/* do I2C init (and probe) first */
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if (I2C::init() != OK)
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goto out;
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/* allocate basic report buffers */
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_reports = new RingBuffer(2, sizeof(differential_pressure_s));
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if (_reports == nullptr)
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goto out;
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/* register alternate interfaces if we have to */
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_class_instance = register_class_devname(AIRSPEED_DEVICE_PATH);
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/* publication init */
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if (_class_instance == CLASS_DEVICE_PRIMARY) {
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/* advertise sensor topic, measure manually to initialize valid report */
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struct differential_pressure_s arp;
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measure();
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_reports->get(&arp);
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/* measurement will have generated a report, publish */
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_airspeed_pub = orb_advertise(ORB_ID(differential_pressure), &arp);
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if (_airspeed_pub < 0)
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warnx("uORB started?");
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}
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ret = OK;
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out:
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return ret;
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}
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int
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Airspeed::probe()
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{
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/* on initial power up the device may need more than one retry
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for detection. Once it is running the number of retries can
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be reduced
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*/
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_retries = 4;
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int ret = measure();
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// drop back to 2 retries once initialised
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_retries = 2;
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return ret;
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}
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int
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Airspeed::ioctl(struct file *filp, int cmd, unsigned long arg)
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{
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switch (cmd) {
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case SENSORIOCSPOLLRATE: {
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switch (arg) {
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/* switching to manual polling */
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case SENSOR_POLLRATE_MANUAL:
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stop();
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_measure_ticks = 0;
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return OK;
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/* external signalling (DRDY) not supported */
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case SENSOR_POLLRATE_EXTERNAL:
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/* zero would be bad */
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case 0:
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return -EINVAL;
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/* set default/max polling rate */
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case SENSOR_POLLRATE_MAX:
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case SENSOR_POLLRATE_DEFAULT: {
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/* do we need to start internal polling? */
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bool want_start = (_measure_ticks == 0);
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/* set interval for next measurement to minimum legal value */
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_measure_ticks = USEC2TICK(_conversion_interval);
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/* if we need to start the poll state machine, do it */
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if (want_start)
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start();
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return OK;
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}
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/* adjust to a legal polling interval in Hz */
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default: {
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/* do we need to start internal polling? */
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bool want_start = (_measure_ticks == 0);
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/* convert hz to tick interval via microseconds */
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unsigned ticks = USEC2TICK(1000000 / arg);
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/* check against maximum rate */
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if (ticks < USEC2TICK(_conversion_interval))
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return -EINVAL;
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/* update interval for next measurement */
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_measure_ticks = ticks;
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/* if we need to start the poll state machine, do it */
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if (want_start)
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start();
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return OK;
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}
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}
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}
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case SENSORIOCGPOLLRATE:
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if (_measure_ticks == 0)
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return SENSOR_POLLRATE_MANUAL;
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return (1000 / _measure_ticks);
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case SENSORIOCSQUEUEDEPTH: {
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/* lower bound is mandatory, upper bound is a sanity check */
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if ((arg < 1) || (arg > 100))
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return -EINVAL;
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irqstate_t flags = irqsave();
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if (!_reports->resize(arg)) {
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irqrestore(flags);
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return -ENOMEM;
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}
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irqrestore(flags);
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return OK;
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}
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case SENSORIOCGQUEUEDEPTH:
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return _reports->size();
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case SENSORIOCRESET:
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/* XXX implement this */
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return -EINVAL;
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case AIRSPEEDIOCSSCALE: {
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struct airspeed_scale *s = (struct airspeed_scale*)arg;
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_diff_pres_offset = s->offset_pa;
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return OK;
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}
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case AIRSPEEDIOCGSCALE: {
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struct airspeed_scale *s = (struct airspeed_scale*)arg;
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s->offset_pa = _diff_pres_offset;
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s->scale = 1.0f;
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return OK;
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}
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default:
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/* give it to the superclass */
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return I2C::ioctl(filp, cmd, arg);
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}
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}
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ssize_t
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Airspeed::read(struct file *filp, char *buffer, size_t buflen)
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{
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unsigned count = buflen / sizeof(differential_pressure_s);
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differential_pressure_s *abuf = reinterpret_cast<differential_pressure_s *>(buffer);
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int ret = 0;
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/* buffer must be large enough */
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if (count < 1)
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return -ENOSPC;
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/* if automatic measurement is enabled */
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if (_measure_ticks > 0) {
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/*
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* While there is space in the caller's buffer, and reports, copy them.
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* Note that we may be pre-empted by the workq thread while we are doing this;
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* we are careful to avoid racing with them.
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*/
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while (count--) {
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if (_reports->get(abuf)) {
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ret += sizeof(*abuf);
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abuf++;
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}
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}
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/* if there was no data, warn the caller */
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return ret ? ret : -EAGAIN;
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}
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/* manual measurement - run one conversion */
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do {
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_reports->flush();
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/* trigger a measurement */
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if (OK != measure()) {
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ret = -EIO;
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break;
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}
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/* wait for it to complete */
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usleep(_conversion_interval);
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/* run the collection phase */
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if (OK != collect()) {
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ret = -EIO;
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break;
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}
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/* state machine will have generated a report, copy it out */
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if (_reports->get(abuf)) {
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ret = sizeof(*abuf);
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}
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} while (0);
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return ret;
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}
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void
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Airspeed::start()
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{
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/* reset the report ring and state machine */
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_collect_phase = false;
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_reports->flush();
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/* schedule a cycle to start things */
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work_queue(HPWORK, &_work, (worker_t)&Airspeed::cycle_trampoline, this, 1);
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}
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void
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Airspeed::stop()
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{
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work_cancel(HPWORK, &_work);
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}
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void
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Airspeed::update_status()
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{
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if (_sensor_ok != _last_published_sensor_ok) {
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/* notify about state change */
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struct subsystem_info_s info = {
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true,
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true,
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_sensor_ok,
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SUBSYSTEM_TYPE_DIFFPRESSURE
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};
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if (_subsys_pub > 0) {
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orb_publish(ORB_ID(subsystem_info), _subsys_pub, &info);
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} else {
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_subsys_pub = orb_advertise(ORB_ID(subsystem_info), &info);
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}
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_last_published_sensor_ok = _sensor_ok;
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}
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}
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void
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Airspeed::cycle_trampoline(void *arg)
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{
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Airspeed *dev = (Airspeed *)arg;
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dev->cycle();
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// XXX we do not know if this is
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// really helping - do not update the
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// subsys state right now
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//dev->update_status();
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}
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void
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Airspeed::print_info()
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{
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perf_print_counter(_sample_perf);
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perf_print_counter(_comms_errors);
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perf_print_counter(_buffer_overflows);
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warnx("poll interval: %u ticks", _measure_ticks);
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_reports->print_info("report queue");
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}
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void
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Airspeed::new_report(const differential_pressure_s &report)
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{
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if (!_reports->force(&report))
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perf_count(_buffer_overflows);
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}
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