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Merge remote-tracking branch 'upstream/master' into new_state_machine

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Conflicts:
	apps/commander/commander.c
	apps/uORB/topics/vehicle_status.h
This commit is contained in:
Julian Oes
2013-03-11 11:01:49 -07:00
parent 0fe5aeb02c 1d444f80a3
commit 591cc0ac4d
55 changed files with 2019 additions and 683 deletions
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apps/sensors/sensors.cpp
+52 -57
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@@ -187,6 +187,7 @@ private:
float mag_scale[3];
float accel_offset[3];
float accel_scale[3];
float airspeed_offset;
int rc_type;
@@ -233,6 +234,7 @@ private:
param_t accel_scale[3];
param_t mag_offset[3];
param_t mag_scale[3];
param_t airspeed_offset;
param_t rc_map_roll;
param_t rc_map_pitch;
@@ -475,6 +477,9 @@ Sensors::Sensors() :
_parameter_handles.mag_scale[1] = param_find("SENS_MAG_YSCALE");
_parameter_handles.mag_scale[2] = param_find("SENS_MAG_ZSCALE");
/*Airspeed offset */
_parameter_handles.airspeed_offset = param_find("SENS_VAIR_OFF");
_parameter_handles.battery_voltage_scaling = param_find("BAT_V_SCALING");
/* fetch initial parameter values */
@@ -672,6 +677,9 @@ Sensors::parameters_update()
param_get(_parameter_handles.mag_scale[1], &(_parameters.mag_scale[1]));
param_get(_parameter_handles.mag_scale[2], &(_parameters.mag_scale[2]));
/* Airspeed offset */
param_get(_parameter_handles.airspeed_offset, &(_parameters.airspeed_offset));
/* scaling of ADC ticks to battery voltage */
if (param_get(_parameter_handles.battery_voltage_scaling, &(_parameters.battery_voltage_scaling)) != OK) {
warnx("Failed updating voltage scaling param");
@@ -975,12 +983,16 @@ Sensors::adc_poll(struct sensor_combined_s &raw)
/* read all channels available */
int ret = read(_fd_adc, &buf_adc, sizeof(buf_adc));
/* look for battery channel */
for (unsigned i = 0; i < sizeof(buf_adc) / sizeof(buf_adc[0]); i++) {
if (ret >= (int)sizeof(buf_adc[0])) {
/* Save raw voltage values */
if (i < (sizeof(raw.adc_voltage_v)) / sizeof(raw.adc_voltage_v[0])) {
raw.adc_voltage_v[i] = buf_adc[i].am_data / (4096.0f / 3.3f);
}
/* look for specific channels and process the raw voltage to measurement data */
if (ADC_BATTERY_VOLTAGE_CHANNEL == buf_adc[i].am_channel) {
/* Voltage in volts */
float voltage = (buf_adc[i].am_data * _parameters.battery_voltage_scaling);
@@ -1010,8 +1022,7 @@ Sensors::adc_poll(struct sensor_combined_s &raw)
} else if (ADC_AIRSPEED_VOLTAGE_CHANNEL == buf_adc[i].am_channel) {
/* calculate airspeed, raw is the difference from */
float voltage = buf_adc[i].am_data / 4096.0f;
float voltage = (float)(buf_adc[i].am_data ) * 3.3f / 4096.0f * 2.0f; //V_ref/4096 * (voltage divider factor)
/**
* The voltage divider pulls the signal down, only act on
@@ -1019,24 +1030,24 @@ Sensors::adc_poll(struct sensor_combined_s &raw)
*/
if (voltage > 0.4f) {
float pres_raw = fabsf(voltage - (3.3f / 2.0f));
float pres_mbar = pres_raw * (3.3f / 5.0f) * 10.0f;
float diff_pres_pa = (voltage - _parameters.airspeed_offset) * 1000.0f; //for MPXV7002DP sensor
float airspeed_true = calc_true_airspeed(pres_mbar + _barometer.pressure,
_barometer.pressure, _barometer.temperature - 5.0f);
float airspeed_true = calc_true_airspeed(diff_pres_pa + _barometer.pressure*1e2f,
_barometer.pressure*1e2f, _barometer.temperature - 5.0f); //factor 1e2 for conversion from mBar to Pa
// XXX HACK - true temperature is much less than indicated temperature in baro,
// subtract 5 degrees in an attempt to account for the electrical upheating of the PCB
float airspeed_indicated = calc_indicated_airspeed(pres_mbar + _barometer.pressure,
_barometer.pressure, _barometer.temperature - 5.0f);
// XXX HACK
float airspeed_indicated = calc_indicated_airspeed(diff_pres_pa);
//printf("voltage: %.4f, diff_pres_pa %.4f, baro press %.4f Pa, v_ind %.4f, v_true %.4f\n", (double)voltage, (double)diff_pres_pa, (double)_barometer.pressure*1e2f, (double)airspeed_indicated, (double)airspeed_true);
_differential_pressure.timestamp = hrt_absolute_time();
_differential_pressure.static_pressure_mbar = _barometer.pressure;
_differential_pressure.differential_pressure_mbar = pres_mbar;
_differential_pressure.differential_pressure_mbar = diff_pres_pa*1e-2f;
_differential_pressure.temperature_celcius = _barometer.temperature;
_differential_pressure.indicated_airspeed_m_s = airspeed_indicated;
_differential_pressure.true_airspeed_m_s = airspeed_true;
_differential_pressure.voltage = voltage;
/* announce the airspeed if needed, just publish else */
if (_airspeed_pub > 0) {
@@ -1058,36 +1069,6 @@ Sensors::adc_poll(struct sensor_combined_s &raw)
void
Sensors::ppm_poll()
{
/* fake low-level driver, directly pulling from driver variables */
static orb_advert_t rc_input_pub = -1;
struct rc_input_values raw;
raw.timestamp = ppm_last_valid_decode;
/* we are accepting this message */
_ppm_last_valid = ppm_last_valid_decode;
/*
* relying on two decoded channels is very noise-prone,
* in particular if nothing is connected to the pins.
* requiring a minimum of four channels
*/
if (ppm_decoded_channels > 4 && hrt_absolute_time() - _ppm_last_valid < PPM_INPUT_TIMEOUT_INTERVAL) {
for (unsigned i = 0; i < ppm_decoded_channels; i++) {
raw.values[i] = ppm_buffer[i];
}
raw.channel_count = ppm_decoded_channels;
/* publish to object request broker */
if (rc_input_pub <= 0) {
rc_input_pub = orb_advertise(ORB_ID(input_rc), &raw);
} else {
orb_publish(ORB_ID(input_rc), rc_input_pub, &raw);
}
}
/* read low-level values from FMU or IO RC inputs (PPM, Spektrum, S.Bus) */
bool rc_updated;
@@ -1133,31 +1114,45 @@ Sensors::ppm_poll()
/* Read out values from raw message */
for (unsigned int i = 0; i < channel_limit; i++) {
/* scale around the mid point differently for lower and upper range */
/*
* 1) Constrain to min/max values, as later processing depends on bounds.
*/
if (rc_input.values[i] < _parameters.min[i])
rc_input.values[i] = _parameters.min[i];
if (rc_input.values[i] > _parameters.max[i])
rc_input.values[i] = _parameters.max[i];
/*
* 2) Scale around the mid point differently for lower and upper range.
*
* This is necessary as they don't share the same endpoints and slope.
*
* First normalize to 0..1 range with correct sign (below or above center),
* the total range is 2 (-1..1).
* If center (trim) == min, scale to 0..1, if center (trim) == max,
* scale to -1..0.
*
* As the min and max bounds were enforced in step 1), division by zero
* cannot occur, as for the case of center == min or center == max the if
* statement is mutually exclusive with the arithmetic NaN case.
*
* DO NOT REMOVE OR ALTER STEP 1!
*/
if (rc_input.values[i] > (_parameters.trim[i] + _parameters.dz[i])) {
_rc.chan[i].scaled = (rc_input.values[i] - _parameters.trim[i]) / (float)(_parameters.max[i] - _parameters.trim[i]);
_rc.chan[i].scaled = (rc_input.values[i] - _parameters.trim[i] - _parameters.dz[i]) / (float)(_parameters.max[i] - _parameters.trim[i] - _parameters.dz[i]);
} else if (rc_input.values[i] < (_parameters.trim[i] - _parameters.dz[i])) {
/* division by zero impossible for trim == min (as for throttle), as this falls in the above if clause */
_rc.chan[i].scaled = -((_parameters.trim[i] - rc_input.values[i]) / (float)(_parameters.trim[i] - _parameters.min[i]));
_rc.chan[i].scaled = (rc_input.values[i] - _parameters.trim[i] - _parameters.dz[i]) / (float)(_parameters.trim[i] - _parameters.min[i] - _parameters.dz[i]);
} else {
/* in the configured dead zone, output zero */
_rc.chan[i].scaled = 0.0f;
}
/* reverse channel if required */
if (i == (int)_rc.function[THROTTLE]) {
if ((int)_parameters.rev[i] == -1) {
_rc.chan[i].scaled = 1.0f + -1.0f * _rc.chan[i].scaled;
}
} else {
_rc.chan[i].scaled *= _parameters.rev[i];
}
_rc.chan[i].scaled *= _parameters.rev[i];
/* handle any parameter-induced blowups */
if (isnan(_rc.chan[i].scaled) || isinf(_rc.chan[i].scaled))
if (!isfinite(_rc.chan[i].scaled))
_rc.chan[i].scaled = 0.0f;
}