TCAS: pressure vs radio altimeter
Altert altitudes refer to AGL/radar alt - not sea-level/pressure alt. Avoids false alerts, i.e. while taxiing.
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2a4657c609
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2 changed files with 42 additions and 19 deletions
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@ -501,7 +501,7 @@ TCAS::AdvisoryCoordinator::update(int mode)
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}
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/* [TCASII]: "Aural annunciations are inhibited below 500+/-100 feet AGL." */
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if ((tcas->threatDetector.getAlt() > 500)&&
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if ((tcas->threatDetector.getRadarAlt() > 500)&&
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(mode >= SwitchTaOnly))
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tcas->annunciator.trigger(current, revertedRA);
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else
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@ -525,8 +525,10 @@ TCAS::AdvisoryCoordinator::update(int mode)
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TCAS::ThreatDetector::ThreatDetector(TCAS* _tcas) :
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tcas(_tcas),
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checkCount(0),
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pAlarmThresholds(&sensitivityLevels[0])
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{
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self.radarAltFt = 0.0;
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unitTest();
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}
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@ -535,7 +537,8 @@ TCAS::ThreatDetector::init(void)
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{
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nodeLat = fgGetNode("/position/latitude-deg", true);
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nodeLon = fgGetNode("/position/longitude-deg", true);
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nodeAlt = fgGetNode("/position/altitude-ft", true);
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nodePressureAlt = fgGetNode("/position/altitude-ft", true);
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nodeRadarAlt = fgGetNode("/position/altitude-agl-ft", true);
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nodeHeading = fgGetNode("/orientation/heading-deg", true);
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nodeVelocity = fgGetNode("/velocities/airspeed-kt", true);
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nodeVerticalFps = fgGetNode("/velocities/vertical-speed-fps", true);
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@ -548,18 +551,30 @@ void
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TCAS::ThreatDetector::update(void)
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{
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// update local position
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self.lat = nodeLat->getDoubleValue();
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self.lon = nodeLon->getDoubleValue();
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self.altFt = nodeAlt->getDoubleValue();
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self.heading = nodeHeading->getDoubleValue();
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self.velocityKt = nodeVelocity->getDoubleValue();
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self.verticalFps = nodeVerticalFps->getDoubleValue();
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self.lat = nodeLat->getDoubleValue();
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self.lon = nodeLon->getDoubleValue();
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self.pressureAltFt = nodePressureAlt->getDoubleValue();
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self.heading = nodeHeading->getDoubleValue();
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self.velocityKt = nodeVelocity->getDoubleValue();
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self.verticalFps = nodeVerticalFps->getDoubleValue();
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/* radar altimeter provides a lot of spikes due to uneven terrain
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* MK-VIII GPWS-spec requires smoothing the radar altitude with a
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* 10second moving average. Likely the TCAS spec requires the same.
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* => We use a cheap 10 second exponential average method.
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*/
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const double SmoothingFactor = 0.3;
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self.radarAltFt = nodeRadarAlt->getDoubleValue()*SmoothingFactor +
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(1-SmoothingFactor)*self.radarAltFt;
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#ifdef FEATURE_TCAS_DEBUG_THREAT_DETECTOR
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printf("TCAS::ThreatDetector::update: radarAlt = %f\n",self.radarAltFt);
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checkCount = 0;
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#endif
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// determine current altitude's "Sensitivity Level Definition and Alarm Thresholds"
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int sl=0;
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for (sl=0;((self.altFt > sensitivityLevels[sl].maxAltitude)&&
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for (sl=0;((self.radarAltFt > sensitivityLevels[sl].maxAltitude)&&
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(sensitivityLevels[sl].maxAltitude));sl++);
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pAlarmThresholds = &sensitivityLevels[sl];
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tcas->advisoryGenerator.setAlarmThresholds(pAlarmThresholds);
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@ -597,7 +612,9 @@ TCAS::ThreatDetector::checkTransponder(const SGPropertyNode* pModel, float veloc
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int
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TCAS::ThreatDetector::checkThreat(int mode, const SGPropertyNode* pModel)
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{
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#ifdef FEATURE_TCAS_DEBUG_THREAT_DETECTOR
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checkCount++;
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#endif
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float velocityKt = pModel->getDoubleValue("velocities/true-airspeed-kt");
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@ -606,7 +623,7 @@ TCAS::ThreatDetector::checkThreat(int mode, const SGPropertyNode* pModel)
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int threatLevel = ThreatNone;
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float altFt = pModel->getDoubleValue("position/altitude-ft");
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currentThreat.relativeAltitudeFt = altFt - self.altFt;
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currentThreat.relativeAltitudeFt = altFt - self.pressureAltFt;
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// save computation time: don't care when relative altitude is excessive
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if (fabs(currentThreat.relativeAltitudeFt) > 10000)
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@ -638,7 +655,7 @@ TCAS::ThreatDetector::checkThreat(int mode, const SGPropertyNode* pModel)
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/* do not detect any threats when in standby or on ground and taxiing */
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if ((mode <= SwitchStandby)||
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((self.altFt < 360)&&(self.velocityKt < 40)))
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((self.radarAltFt < 360)&&(self.velocityKt < 40)))
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{
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return threatLevel;
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}
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@ -1032,7 +1049,7 @@ TCAS::AdvisoryGenerator::resolution(int mode, int threatLevel, float rangeNm, fl
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/* [EUROACAS]: "Certain RAs are inhibited at altitudes based on inputs from the radio altimeter:
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* [..] (c)1000ft (+/- 100ft) and below, all RAs are inhibited;" */
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if (pSelf->altFt < 1000)
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if (pSelf->radarAltFt < 1000)
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threatLevel = ThreatTA;
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// RAs only issued in mode "Auto" (= "TA/RA" mode)
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@ -1100,7 +1117,7 @@ TCAS::AdvisoryGenerator::resolution(int mode, int threatLevel, float rangeNm, fl
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/* [TCASII]: "TCAS is designed to inhibit Increase Descent RAs below 1450 feet AGL; */
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/* [TCASII]: "Descend RAs below 1100 feet AGL;" (inhibited) */
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if (pSelf->altFt < 1100)
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if (pSelf->radarAltFt < 1100)
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{
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RA &= ~AdvisoryDescend;
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//TODO Support "Do not descend" RA
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@ -1291,8 +1308,8 @@ TCAS::selfTest(void)
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newAdvisory.threatLevel = ThreatRA;
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newAdvisory.RA = AdvisoryClear;
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newAdvisory.RAOption = OptionNone;
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// TCAS audio is disabled below 500ft
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threatDetector.setAlt(501);
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// TCAS audio is disabled below 500ft AGL
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threatDetector.setRadarAlt(501);
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// trigger various advisories
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switch(selfTestStep)
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@ -140,7 +140,8 @@ class TCAS : public SGSubsystem
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{
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double lat;
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double lon;
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float altFt;
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float pressureAltFt;
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float radarAltFt;
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float heading;
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float velocityKt;
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float verticalFps;
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@ -324,8 +325,12 @@ class TCAS : public SGSubsystem
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void horizontalThreat (float bearing, float distanceNm, float heading,
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float velocityKt);
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void setAlt (float altFt) { self.altFt = altFt;}
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float getAlt (void) { return self.altFt;}
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void setPressureAlt (float altFt) { self.pressureAltFt = altFt;}
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float getPressureAlt (void) { return self.pressureAltFt;}
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void setRadarAlt (float altFt) { self.radarAltFt = altFt;}
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float getRadarAlt (void) { return self.radarAltFt;}
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float getVelocityKt (void) { return self.velocityKt;}
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int getRASense (void) { return currentThreat.RASense;}
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@ -340,7 +345,8 @@ class TCAS : public SGSubsystem
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SGPropertyNode_ptr nodeLat;
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SGPropertyNode_ptr nodeLon;
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SGPropertyNode_ptr nodeAlt;
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SGPropertyNode_ptr nodePressureAlt;
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SGPropertyNode_ptr nodeRadarAlt;
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SGPropertyNode_ptr nodeHeading;
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SGPropertyNode_ptr nodeVelocity;
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SGPropertyNode_ptr nodeVerticalFps;
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