mirror of https://github.com/ArduPilot/ardupilot
APM: update for new barometer interface
the barometer can now calibrate and return altitude values. A 0.3 low pass filter is used on altitude to match the previous code
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@ -46,6 +46,7 @@ version 2.1 of the License, or (at your option) any later version.
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#include <AP_RangeFinder.h> // Range finder library
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#include <Filter.h> // Filter library
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#include <ModeFilter.h> // Mode Filter from Filter library
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#include <LowPassFilter.h> // LowPassFilter class (inherits from Filter class)
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#include <AP_Relay.h> // APM relay
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#include <AP_Camera.h> // Photo or video camera
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#include <memcheck.h>
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@ -469,8 +470,6 @@ static float airspeed_pressure;
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////////////////////////////////////////////////////////////////////////////////
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// Altitude Sensor variables
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////////////////////////////////////////////////////////////////////////////////
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// Raw absolute pressure measurement (filtered). ADC units
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static unsigned long abs_pressure;
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// Altitude from the sonar sensor. Meters. Not yet implemented.
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static int sonar_alt;
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@ -7,66 +7,23 @@ void ReadSCP1000(void) {}
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static void init_barometer(void)
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{
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int flashcount = 0;
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long ground_pressure = 0;
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int ground_temperature;
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while (ground_pressure == 0 || !barometer.healthy) {
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barometer.read(); // Get initial data from absolute pressure sensor
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ground_pressure = barometer.get_pressure();
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ground_temperature = barometer.get_temperature();
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mavlink_delay(20);
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//Serial.printf("barometer.Press %ld\n", barometer.get_pressure());
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}
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for(int i = 0; i < 30; i++){ // We take some readings...
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#if HIL_MODE == HIL_MODE_SENSORS
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gcs_update(); // look for inbound hil packets
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#endif
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do {
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barometer.read(); // Get pressure sensor
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} while (!barometer.healthy);
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ground_pressure = (ground_pressure * 9l + barometer.get_pressure()) / 10l;
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ground_temperature = (ground_temperature * 9 + barometer.get_temperature()) / 10;
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mavlink_delay(20);
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if(flashcount == 5) {
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digitalWrite(C_LED_PIN, LED_OFF);
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digitalWrite(A_LED_PIN, LED_ON);
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digitalWrite(B_LED_PIN, LED_OFF);
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}
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if(flashcount >= 10) {
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flashcount = 0;
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digitalWrite(C_LED_PIN, LED_ON);
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digitalWrite(A_LED_PIN, LED_OFF);
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digitalWrite(B_LED_PIN, LED_ON);
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}
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flashcount++;
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}
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g.ground_pressure.set_and_save(ground_pressure);
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g.ground_temperature.set_and_save(ground_temperature / 10.0f);
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abs_pressure = ground_pressure;
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Serial.printf_P(PSTR("abs_pressure %ld\n"), abs_pressure);
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gcs_send_text_P(SEVERITY_MEDIUM, PSTR("barometer calibration complete."));
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barometer.calibrate(mavlink_delay);
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g.ground_pressure.set_and_save(barometer.get_ground_pressure());
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g.ground_temperature.set_and_save(barometer.get_ground_temperature() / 10.0f);
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ahrs.set_barometer(&barometer);
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gcs_send_text_P(SEVERITY_LOW, PSTR("barometer calibration complete"));
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}
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static long read_barometer(void)
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// filter altitude from the barometer with a 0.3 low pass
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// filter
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static LowPassFilterInt32 altitude_filter(0.3);
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// read the barometer and return the updated altitude in centimeters
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// above the calibration altitude
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static int32_t read_barometer(void)
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{
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float x, scaling, temp;
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barometer.read(); // Get new data from absolute pressure sensor
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//abs_pressure = (abs_pressure + barometer.get_pressure()) >> 1; // Small filtering
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abs_pressure = ((float)abs_pressure * .7) + ((float)barometer.get_pressure() * .3); // large filtering
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scaling = (float)g.ground_pressure / (float)abs_pressure;
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temp = ((float)g.ground_temperature) + 273.15f;
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x = log(scaling) * temp * 29271.267f;
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return (x / 10);
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barometer.read();
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return altitude_filter.apply(((int32_t)barometer.get_altitude() * 100.0));
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}
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// in M/S * 100
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@ -695,7 +695,7 @@ test_pressure(uint8_t argc, const Menu::arg *argv)
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} else {
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Serial.printf_P(PSTR("Alt: %0.2fm, Raw: %ld Temperature: %.1f\n"),
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current_loc.alt / 100.0,
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abs_pressure, 0.1*barometer.get_temperature());
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barometer.get_pressure(), 0.1*barometer.get_temperature());
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}
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if(Serial.available() > 0){
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