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authorLorenz Meier <lm@inf.ethz.ch>2014-02-09 16:04:32 +0100
committerLorenz Meier <lm@inf.ethz.ch>2014-02-09 16:04:32 +0100
commit773f70a9df376745523bf78f29d6747c8878c01d (patch)
treef63d9f6c2d4bb3bb3018b230ae9f42f89ff85c7a /src/drivers/meas_airspeed/meas_airspeed.cpp
parentac326beaaae7b38d65ad6d7d13f00dfeaa6ae520 (diff)
parentf52f15c7914983ea1569e584e516d53d21cdde56 (diff)
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Merged origin/master into pubsub_cleanup
Diffstat (limited to 'src/drivers/meas_airspeed/meas_airspeed.cpp')
-rw-r--r--src/drivers/meas_airspeed/meas_airspeed.cpp22
1 files changed, 7 insertions, 15 deletions
diff --git a/src/drivers/meas_airspeed/meas_airspeed.cpp b/src/drivers/meas_airspeed/meas_airspeed.cpp
index 51a059e39..05ae21c1f 100644
--- a/src/drivers/meas_airspeed/meas_airspeed.cpp
+++ b/src/drivers/meas_airspeed/meas_airspeed.cpp
@@ -77,7 +77,6 @@
#include <systemlib/err.h>
#include <systemlib/param/param.h>
#include <systemlib/perf_counter.h>
-#include <mathlib/mathlib.h>
#include <drivers/drv_airspeed.h>
#include <drivers/drv_hrt.h>
@@ -178,24 +177,17 @@ MEASAirspeed::collect()
return ret;
}
- //uint16_t diff_pres_pa = (val[1]) | ((val[0] & ~(0xC0)) << 8);
- uint16_t temp = (val[3] & 0xE0) << 8 | val[2];
-
- // XXX leaving this in until new calculation method has been cross-checked
- //diff_pres_pa = abs(diff_pres_pa - (16384 / 2.0f));
- //diff_pres_pa -= _diff_pres_offset;
int16_t dp_raw = 0, dT_raw = 0;
dp_raw = (val[0] << 8) + val[1];
- dp_raw = 0x3FFF & dp_raw; //mask the used bits
+ /* mask the used bits */
+ dp_raw = 0x3FFF & dp_raw;
dT_raw = (val[2] << 8) + val[3];
dT_raw = (0xFFE0 & dT_raw) >> 5;
float temperature = ((200 * dT_raw) / 2047) - 50;
- // XXX we may want to smooth out the readings to remove noise.
-
- // Calculate differential pressure. As its centered around 8000
- // and can go positive or negative, enforce absolute value
-// uint16_t diff_press_pa = abs(dp_raw - (16384 / 2.0f));
+ /* calculate differential pressure. As its centered around 8000
+ * and can go positive or negative, enforce absolute value
+ */
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;
@@ -204,7 +196,7 @@ MEASAirspeed::collect()
struct differential_pressure_s report;
- // Track maximum differential pressure measured (so we can work out top speed).
+ /* 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;
}
@@ -394,7 +386,7 @@ test()
err(1, "immediate read failed");
warnx("single read");
- warnx("diff pressure: %d pa", report.differential_pressure_pa);
+ warnx("diff pressure: %d pa", (double)report.differential_pressure_pa);
/* start the sensor polling at 2Hz */
if (OK != ioctl(fd, SENSORIOCSPOLLRATE, 2))