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Debug mode for pitot meter
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parent
127542c4d3
commit
c12163930d
3 changed files with 8 additions and 1 deletions
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@ -52,5 +52,6 @@ typedef enum {
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DEBUG_FW_CLIMB_RATE_TO_ALTITUDE,
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DEBUG_RANGEFINDER,
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DEBUG_RANGEFINDER_QUALITY,
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DEBUG_PITOT,
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DEBUG_COUNT
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} debugType_e;
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@ -331,7 +331,8 @@ static const char * const lookupTableDebug[DEBUG_COUNT] = {
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"NAV_LANDING",
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"FW_ALTITUDE",
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"RFIND",
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"RFIND_Q"
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"RFIND_Q",
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"PITOT"
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};
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#ifdef TELEMETRY_LTM
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@ -203,9 +203,11 @@ uint32_t pitotUpdate(void)
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case PITOTMETER_NEEDS_CALCULATION:
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pitot.dev.get();
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pitot.dev.calculate(&pitotPressure, &pitotTemperature);
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DEBUG_SET(DEBUG_PITOT, 0, pitotPressure);
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if (pitotmeterConfig()->use_median_filtering) {
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pitotPressure = applyPitotmeterMedianFilter(pitotPressure);
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}
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DEBUG_SET(DEBUG_PITOT, 1, pitotPressure);
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state = PITOTMETER_NEEDS_SAMPLES;
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return pitot.dev.delay;
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break;
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@ -245,6 +247,9 @@ int32_t pitotCalculateAirSpeed(void)
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const float indicatedAirspeed_tmp = pitotmeterConfig()->pitot_scale * sqrtf(2.0f * fabsf(pitotPressure - pitotPressureZero) / AIR_DENSITY_SEA_LEVEL_15C);
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indicatedAirspeed += pitotmeterConfig()->pitot_noise_lpf * (indicatedAirspeed_tmp - indicatedAirspeed);
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DEBUG_SET(DEBUG_PITOT, 2, indicatedAirspeed_tmp);
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DEBUG_SET(DEBUG_PITOT, 3, indicatedAirspeed);
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pitot.airSpeed = indicatedAirspeed * 100;
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} else {
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performPitotCalibrationCycle();
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