/**************************************************************************** * * Copyright (c) 2013, 2014 PX4 Development Team. All rights reserved. * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions * are met: * * 1. Redistributions of source code must retain the above copyright * notice, this list of conditions and the following disclaimer. * 2. Redistributions in binary form must reproduce the above copyright * notice, this list of conditions and the following disclaimer in * the documentation and/or other materials provided with the * distribution. * 3. Neither the name PX4 nor the names of its contributors may be * used to endorse or promote products derived from this software * without specific prior written permission. * * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE * POSSIBILITY OF SUCH DAMAGE. * ****************************************************************************/ /** * @file ets_airspeed.cpp * @author Simon Wilks * * Driver for the Eagle Tree Airspeed V3 connected via I2C. */ #include #include #include #include #include #include #include #include #include #include #include #include #include #include #include #include #include #include #include #include #include #include #include #include #include #include #include #include #include Airspeed::Airspeed(int bus, int address, unsigned conversion_interval, const char* path) : I2C("Airspeed", path, bus, address, 100000), _reports(nullptr), _buffer_overflows(perf_alloc(PC_COUNT, "airspeed_buffer_overflows")), _max_differential_pressure_pa(0), _sensor_ok(false), _last_published_sensor_ok(true), /* initialize differently to force publication */ _measure_ticks(0), _collect_phase(false), _diff_pres_offset(0.0f), _airspeed_pub(-1), _subsys_pub(-1), _class_instance(-1), _conversion_interval(conversion_interval), _sample_perf(perf_alloc(PC_ELAPSED, "airspeed_read")), _comms_errors(perf_alloc(PC_COUNT, "airspeed_comms_errors")) { // enable debug() calls _debug_enabled = false; // work_cancel in the dtor will explode if we don't do this... memset(&_work, 0, sizeof(_work)); } Airspeed::~Airspeed() { /* make sure we are truly inactive */ stop(); if (_class_instance != -1) unregister_class_devname(AIRSPEED_DEVICE_PATH, _class_instance); /* free any existing reports */ if (_reports != nullptr) delete _reports; // free perf counters perf_free(_sample_perf); perf_free(_comms_errors); perf_free(_buffer_overflows); } int Airspeed::init() { int ret = ERROR; /* do I2C init (and probe) first */ if (I2C::init() != OK) goto out; /* allocate basic report buffers */ _reports = new RingBuffer(2, sizeof(differential_pressure_s)); if (_reports == nullptr) goto out; /* register alternate interfaces if we have to */ _class_instance = register_class_devname(AIRSPEED_DEVICE_PATH); /* publication init */ if (_class_instance == CLASS_DEVICE_PRIMARY) { /* advertise sensor topic, measure manually to initialize valid report */ struct differential_pressure_s arp; measure(); _reports->get(&arp); /* measurement will have generated a report, publish */ _airspeed_pub = orb_advertise(ORB_ID(differential_pressure), &arp); if (_airspeed_pub < 0) warnx("failed to create airspeed sensor object. uORB started?"); } ret = OK; out: return ret; } int Airspeed::probe() { /* on initial power up the device needs more than one retry for detection. Once it is running then retries aren't needed */ _retries = 4; int ret = measure(); _retries = 2; return ret; } int Airspeed::ioctl(struct file *filp, int cmd, unsigned long arg) { switch (cmd) { case SENSORIOCSPOLLRATE: { switch (arg) { /* switching to manual polling */ case SENSOR_POLLRATE_MANUAL: stop(); _measure_ticks = 0; return OK; /* external signalling (DRDY) not supported */ case SENSOR_POLLRATE_EXTERNAL: /* zero would be bad */ case 0: return -EINVAL; /* set default/max polling rate */ case SENSOR_POLLRATE_MAX: case SENSOR_POLLRATE_DEFAULT: { /* do we need to start internal polling? */ bool want_start = (_measure_ticks == 0); /* set interval for next measurement to minimum legal value */ _measure_ticks = USEC2TICK(_conversion_interval); /* if we need to start the poll state machine, do it */ if (want_start) start(); return OK; } /* adjust to a legal polling interval in Hz */ default: { /* do we need to start internal polling? */ bool want_start = (_measure_ticks == 0); /* convert hz to tick interval via microseconds */ unsigned ticks = USEC2TICK(1000000 / arg); /* check against maximum rate */ if (ticks < USEC2TICK(_conversion_interval)) return -EINVAL; /* update interval for next measurement */ _measure_ticks = ticks; /* if we need to start the poll state machine, do it */ if (want_start) start(); return OK; } } } case SENSORIOCGPOLLRATE: if (_measure_ticks == 0) return SENSOR_POLLRATE_MANUAL; return (1000 / _measure_ticks); case SENSORIOCSQUEUEDEPTH: { /* lower bound is mandatory, upper bound is a sanity check */ if ((arg < 1) || (arg > 100)) return -EINVAL; irqstate_t flags = irqsave(); if (!_reports->resize(arg)) { irqrestore(flags); return -ENOMEM; } irqrestore(flags); return OK; } case SENSORIOCGQUEUEDEPTH: return _reports->size(); case SENSORIOCRESET: /* XXX implement this */ return -EINVAL; case AIRSPEEDIOCSSCALE: { struct airspeed_scale *s = (struct airspeed_scale*)arg; _diff_pres_offset = s->offset_pa; return OK; } case AIRSPEEDIOCGSCALE: { struct airspeed_scale *s = (struct airspeed_scale*)arg; s->offset_pa = _diff_pres_offset; s->scale = 1.0f; return OK; } default: /* give it to the superclass */ return I2C::ioctl(filp, cmd, arg); } } ssize_t Airspeed::read(struct file *filp, char *buffer, size_t buflen) { unsigned count = buflen / sizeof(differential_pressure_s); differential_pressure_s *abuf = reinterpret_cast(buffer); int ret = 0; /* buffer must be large enough */ if (count < 1) return -ENOSPC; /* if automatic measurement is enabled */ if (_measure_ticks > 0) { /* * While there is space in the caller's buffer, and reports, copy them. * Note that we may be pre-empted by the workq thread while we are doing this; * we are careful to avoid racing with them. */ while (count--) { if (_reports->get(abuf)) { ret += sizeof(*abuf); abuf++; } } /* if there was no data, warn the caller */ return ret ? ret : -EAGAIN; } /* manual measurement - run one conversion */ do { _reports->flush(); /* trigger a measurement */ if (OK != measure()) { ret = -EIO; break; } /* wait for it to complete */ usleep(_conversion_interval); /* run the collection phase */ if (OK != collect()) { ret = -EIO; break; } /* state machine will have generated a report, copy it out */ if (_reports->get(abuf)) { ret = sizeof(*abuf); } } while (0); return ret; } void Airspeed::start() { /* reset the report ring and state machine */ _collect_phase = false; _reports->flush(); /* schedule a cycle to start things */ work_queue(HPWORK, &_work, (worker_t)&Airspeed::cycle_trampoline, this, 1); } void Airspeed::stop() { work_cancel(HPWORK, &_work); } void Airspeed::update_status() { if (_sensor_ok != _last_published_sensor_ok) { /* notify about state change */ struct subsystem_info_s info = { true, true, _sensor_ok, SUBSYSTEM_TYPE_DIFFPRESSURE }; if (_subsys_pub > 0) { orb_publish(ORB_ID(subsystem_info), _subsys_pub, &info); } else { _subsys_pub = orb_advertise(ORB_ID(subsystem_info), &info); } _last_published_sensor_ok = _sensor_ok; } } void Airspeed::cycle_trampoline(void *arg) { Airspeed *dev = (Airspeed *)arg; dev->cycle(); dev->update_status(); } void Airspeed::print_info() { perf_print_counter(_sample_perf); perf_print_counter(_comms_errors); perf_print_counter(_buffer_overflows); warnx("poll interval: %u ticks", _measure_ticks); _reports->print_info("report queue"); } void Airspeed::new_report(const differential_pressure_s &report) { if (!_reports->force(&report)) perf_count(_buffer_overflows); }