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