Merge branch 'master' of github.com:PX4/Firmware into bottle_drop_friday

This commit is contained in:
Lorenz Meier
2014-08-24 12:05:37 +02:00
6 changed files with 40 additions and 61 deletions
+6 -14
View File
@@ -155,7 +155,6 @@ ETSAirspeed::collect()
}
uint16_t diff_pres_pa_raw = val[1] << 8 | val[0];
uint16_t diff_pres_pa;
if (diff_pres_pa_raw == 0) {
// a zero value means the pressure sensor cannot give us a
// value. We need to return, and not report a value or the
@@ -166,28 +165,21 @@ ETSAirspeed::collect()
return -1;
}
if (diff_pres_pa_raw < _diff_pres_offset + MIN_ACCURATE_DIFF_PRES_PA) {
diff_pres_pa = 0;
} else {
diff_pres_pa = diff_pres_pa_raw - _diff_pres_offset;
}
// The raw value still should be compensated for the known offset
diff_pres_pa_raw -= _diff_pres_offset;
// Track maximum differential pressure measured (so we can work out top speed).
if (diff_pres_pa > _max_differential_pressure_pa) {
_max_differential_pressure_pa = diff_pres_pa;
if (diff_pres_pa_raw > _max_differential_pressure_pa) {
_max_differential_pressure_pa = diff_pres_pa_raw;
}
differential_pressure_s report;
report.timestamp = hrt_absolute_time();
report.error_count = perf_event_count(_comms_errors);
report.differential_pressure_pa = (float)diff_pres_pa;
// XXX we may want to smooth out the readings to remove noise.
report.differential_pressure_filtered_pa = (float)diff_pres_pa;
report.differential_pressure_raw_pa = (float)diff_pres_pa_raw;
report.differential_pressure_filtered_pa = diff_pres_pa_raw;
report.differential_pressure_raw_pa = diff_pres_pa_raw;
report.temperature = -1000.0f;
report.max_differential_pressure_pa = _max_differential_pressure_pa;
@@ -369,7 +361,7 @@ test()
err(1, "immediate read failed");
warnx("single read");
warnx("diff pressure: %f pa", (double)report.differential_pressure_pa);
warnx("diff pressure: %f pa", (double)report.differential_pressure_filtered_pa);
/* start the sensor polling at 2Hz */
if (OK != ioctl(fd, SENSORIOCSPOLLRATE, 2))
@@ -394,7 +386,7 @@ test()
err(1, "periodic read failed");
warnx("periodic read %u", i);
warnx("diff pressure: %f pa", (double)report.differential_pressure_pa);
warnx("diff pressure: %f pa", (double)report.differential_pressure_filtered_pa);
}
/* reset the sensor polling to its default rate */
+8 -29
View File
@@ -228,44 +228,23 @@ MEASAirspeed::collect()
// the raw value still should be compensated for the known offset
diff_press_pa_raw -= _diff_pres_offset;
float diff_press_pa = fabsf(diff_press_pa_raw);
/*
note that we return both the absolute value with offset
applied and a raw value without the offset applied. This
makes it possible for higher level code to detect if the
user has the tubes connected backwards, and also makes it
possible to correctly use offsets calculated by a higher
level airspeed driver.
With the above calculation the MS4525 sensor will produce a
positive number when the top port is used as a dynamic port
and bottom port is used as the static port
Also note that the _diff_pres_offset is applied before the
fabsf() not afterwards. It needs to be done this way to
prevent a bias at low speeds, but this also means that when
setting a offset you must set it based on the raw value, not
the offset value
*/
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;
if (diff_press_pa_raw > _max_differential_pressure_pa) {
_max_differential_pressure_pa = diff_press_pa_raw;
}
report.timestamp = hrt_absolute_time();
report.error_count = perf_event_count(_comms_errors);
report.temperature = temperature;
report.differential_pressure_pa = diff_press_pa;
report.differential_pressure_filtered_pa = _filter.apply(diff_press_pa);
/* the dynamics of the filter can make it overshoot into the negative range */
if (report.differential_pressure_filtered_pa < 0.0f) {
report.differential_pressure_filtered_pa = _filter.reset(diff_press_pa);
}
report.differential_pressure_filtered_pa = _filter.apply(diff_press_pa_raw);
report.differential_pressure_raw_pa = diff_press_pa_raw;
report.max_differential_pressure_pa = _max_differential_pressure_pa;
@@ -345,7 +324,7 @@ MEASAirspeed::cycle()
/**
correct for 5V rail voltage if the system_power ORB topic is
available
See http://uav.tridgell.net/MS4525/MS4525-offset.png for a graph of
offset versus voltage for 3 sensors
*/
@@ -394,7 +373,7 @@ MEASAirspeed::voltage_correction(float &diff_press_pa, float &temperature)
if (voltage_diff < -1.0f) {
voltage_diff = -1.0f;
}
temperature -= voltage_diff * temp_slope;
temperature -= voltage_diff * temp_slope;
#endif // CONFIG_ARCH_BOARD_PX4FMU_V2
}
@@ -523,7 +502,7 @@ test()
}
warnx("single read");
warnx("diff pressure: %d pa", (int)report.differential_pressure_pa);
warnx("diff pressure: %d pa", (int)report.differential_pressure_filtered_pa);
/* start the sensor polling at 2Hz */
if (OK != ioctl(fd, SENSORIOCSPOLLRATE, 2)) {
@@ -551,7 +530,7 @@ test()
}
warnx("periodic read %u", i);
warnx("diff pressure: %d pa", (int)report.differential_pressure_pa);
warnx("diff pressure: %d pa", (int)report.differential_pressure_filtered_pa);
warnx("temperature: %d C (0x%02x)", (int)report.temperature, (unsigned) report.temperature);
}