forked from Archive/PX4-Autopilot
Fixed MS4525 error flag handling
This commit is contained in:
parent
7be1c400f9
commit
c5a1f4617c
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@ -104,7 +104,7 @@
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class MEASAirspeed : public Airspeed
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{
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public:
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MEASAirspeed(int bus, int address = I2C_ADDRESS_MS4525DO, const char* path = PATH_MS4525);
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MEASAirspeed(int bus, int address = I2C_ADDRESS_MS4525DO, const char *path = PATH_MS4525);
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protected:
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@ -123,7 +123,7 @@ protected:
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*/
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extern "C" __EXPORT int meas_airspeed_main(int argc, char *argv[]);
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MEASAirspeed::MEASAirspeed(int bus, int address, const char* path) : Airspeed(bus, address,
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MEASAirspeed::MEASAirspeed(int bus, int address, const char *path) : Airspeed(bus, address,
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CONVERSION_INTERVAL, path)
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{
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@ -161,23 +161,30 @@ MEASAirspeed::collect()
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ret = transfer(nullptr, 0, &val[0], 4);
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if (ret < 0) {
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perf_count(_comms_errors);
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perf_end(_sample_perf);
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perf_count(_comms_errors);
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perf_end(_sample_perf);
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return ret;
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}
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uint8_t status = val[0] & 0xC0;
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uint8_t status = (val[0] & 0xC0) >> 6;
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if (status == 2) {
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log("err: stale data");
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perf_count(_comms_errors);
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perf_end(_sample_perf);
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return ret;
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} else if (status == 3) {
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log("err: fault");
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perf_count(_comms_errors);
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perf_end(_sample_perf);
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return ret;
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switch (status) {
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case 0: break;
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case 1:
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perf_count(_comms_errors);
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perf_end(_sample_perf);
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return -EAGAIN;
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case 2:
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perf_count(_comms_errors);
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perf_end(_sample_perf);
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return -EAGAIN;
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case 3:
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perf_count(_comms_errors);
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perf_end(_sample_perf);
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return -EAGAIN;
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}
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int16_t dp_raw = 0, dT_raw = 0;
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@ -193,19 +200,21 @@ MEASAirspeed::collect()
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*/
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const float P_min = -1.0f;
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const float P_max = 1.0f;
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float diff_press_pa = fabsf( ( ((float)dp_raw - 0.1f*16383.0f) * (P_max-P_min)/(0.8f*16383.0f) + P_min) * 6894.8f) - _diff_pres_offset;
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if (diff_press_pa < 0.0f)
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diff_press_pa = 0.0f;
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float diff_press_pa = fabsf((((float)dp_raw - 0.1f * 16383.0f) * (P_max - P_min) / (0.8f * 16383.0f) + P_min) * 6894.8f) - _diff_pres_offset;
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if (diff_press_pa < 0.0f) {
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diff_press_pa = 0.0f;
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}
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struct differential_pressure_s report;
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/* track maximum differential pressure measured (so we can work out top speed). */
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if (diff_press_pa > _max_differential_pressure_pa) {
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_max_differential_pressure_pa = diff_press_pa;
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_max_differential_pressure_pa = diff_press_pa;
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}
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report.timestamp = hrt_absolute_time();
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report.error_count = perf_event_count(_comms_errors);
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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_pa = diff_press_pa;
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report.voltage = 0;
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@ -261,8 +270,9 @@ MEASAirspeed::cycle()
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}
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/* measurement phase */
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if (OK != measure())
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if (OK != measure()) {
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log("measure error");
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}
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/* next phase is collection */
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_collect_phase = true;
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@ -303,15 +313,17 @@ start(int i2c_bus)
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{
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int fd;
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if (g_dev != nullptr)
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if (g_dev != nullptr) {
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errx(1, "already started");
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}
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/* create the driver, try the MS4525DO first */
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g_dev = new MEASAirspeed(i2c_bus, I2C_ADDRESS_MS4525DO, PATH_MS4525);
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/* check if the MS4525DO was instantiated */
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if (g_dev == nullptr)
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if (g_dev == nullptr) {
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goto fail;
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}
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/* try the MS5525DSO next if init fails */
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if (OK != g_dev->Airspeed::init()) {
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@ -319,22 +331,26 @@ start(int i2c_bus)
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g_dev = new MEASAirspeed(i2c_bus, I2C_ADDRESS_MS5525DSO, PATH_MS5525);
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/* check if the MS5525DSO was instantiated */
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if (g_dev == nullptr)
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if (g_dev == nullptr) {
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goto fail;
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}
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/* both versions failed if the init for the MS5525DSO fails, give up */
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if (OK != g_dev->Airspeed::init())
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if (OK != g_dev->Airspeed::init()) {
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goto fail;
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}
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}
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/* set the poll rate to default, starts automatic data collection */
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fd = open(AIRSPEED_DEVICE_PATH, O_RDONLY);
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if (fd < 0)
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if (fd < 0) {
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goto fail;
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}
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if (ioctl(fd, SENSORIOCSPOLLRATE, SENSOR_POLLRATE_DEFAULT) < 0)
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if (ioctl(fd, SENSORIOCSPOLLRATE, SENSOR_POLLRATE_DEFAULT) < 0) {
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goto fail;
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}
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exit(0);
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@ -379,21 +395,24 @@ test()
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int fd = open(AIRSPEED_DEVICE_PATH, O_RDONLY);
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if (fd < 0)
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if (fd < 0) {
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err(1, "%s open failed (try 'meas_airspeed start' if the driver is not running", AIRSPEED_DEVICE_PATH);
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}
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/* do a simple demand read */
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sz = read(fd, &report, sizeof(report));
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if (sz != sizeof(report))
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if (sz != sizeof(report)) {
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err(1, "immediate read failed");
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}
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warnx("single read");
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warnx("diff pressure: %8.4f pa", (double)report.differential_pressure_pa);
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/* start the sensor polling at 2Hz */
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if (OK != ioctl(fd, SENSORIOCSPOLLRATE, 2))
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if (OK != ioctl(fd, SENSORIOCSPOLLRATE, 2)) {
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errx(1, "failed to set 2Hz poll rate");
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}
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/* read the sensor 5x and report each value */
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for (unsigned i = 0; i < 5; i++) {
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@ -404,14 +423,16 @@ test()
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fds.events = POLLIN;
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ret = poll(&fds, 1, 2000);
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if (ret != 1)
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if (ret != 1) {
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errx(1, "timed out waiting for sensor data");
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}
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/* now go get it */
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sz = read(fd, &report, sizeof(report));
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if (sz != sizeof(report))
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if (sz != sizeof(report)) {
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err(1, "periodic read failed");
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}
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warnx("periodic read %u", i);
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warnx("diff pressure: %8.4f pa", (double)report.differential_pressure_pa);
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@ -419,8 +440,9 @@ test()
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}
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/* reset the sensor polling to its default rate */
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if (OK != ioctl(fd, SENSORIOCSPOLLRATE, SENSOR_POLLRATE_DEFAULT))
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if (OK != ioctl(fd, SENSORIOCSPOLLRATE, SENSOR_POLLRATE_DEFAULT)) {
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errx(1, "failed to set default rate");
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}
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errx(0, "PASS");
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}
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@ -433,14 +455,17 @@ reset()
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{
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int fd = open(AIRSPEED_DEVICE_PATH, O_RDONLY);
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if (fd < 0)
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if (fd < 0) {
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err(1, "failed ");
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}
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if (ioctl(fd, SENSORIOCRESET, 0) < 0)
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if (ioctl(fd, SENSORIOCRESET, 0) < 0) {
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err(1, "driver reset failed");
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}
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if (ioctl(fd, SENSORIOCSPOLLRATE, SENSOR_POLLRATE_DEFAULT) < 0)
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if (ioctl(fd, SENSORIOCSPOLLRATE, SENSOR_POLLRATE_DEFAULT) < 0) {
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err(1, "driver poll restart failed");
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}
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exit(0);
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}
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@ -451,8 +476,9 @@ reset()
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void
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info()
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{
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if (g_dev == nullptr)
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if (g_dev == nullptr) {
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errx(1, "driver not running");
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}
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printf("state @ %p\n", g_dev);
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g_dev->print_info();
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@ -491,32 +517,37 @@ meas_airspeed_main(int argc, char *argv[])
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/*
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* Start/load the driver.
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*/
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if (!strcmp(argv[1], "start"))
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if (!strcmp(argv[1], "start")) {
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meas_airspeed::start(i2c_bus);
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}
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/*
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* Stop the driver
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*/
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if (!strcmp(argv[1], "stop"))
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if (!strcmp(argv[1], "stop")) {
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meas_airspeed::stop();
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}
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/*
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* Test the driver/device.
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*/
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if (!strcmp(argv[1], "test"))
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if (!strcmp(argv[1], "test")) {
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meas_airspeed::test();
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}
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/*
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* Reset the driver.
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*/
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if (!strcmp(argv[1], "reset"))
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if (!strcmp(argv[1], "reset")) {
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meas_airspeed::reset();
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}
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/*
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* Print driver information.
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*/
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if (!strcmp(argv[1], "info") || !strcmp(argv[1], "status"))
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if (!strcmp(argv[1], "info") || !strcmp(argv[1], "status")) {
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meas_airspeed::info();
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}
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meas_airspeed_usage();
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exit(0);
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