mirror of https://github.com/ArduPilot/ardupilot
AP_NavEKF: Modifed Vel Pos fusion to fuse height data whenever baro reading has changed
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@ -71,6 +71,8 @@ NavEKF::NavEKF(const AP_AHRS *ahrs, AP_Baro &baro) :
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hgtRate = 0.0f;
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mag_state.q0 = 1;
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mag_state.DCM.identity();
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hgtMeaPrev = 0.0f;
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hgtMea = 0.0f;
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}
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bool NavEKF::healthy(void) const
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@ -262,31 +264,12 @@ void NavEKF::SelectVelPosFusion()
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{
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fuseVelData = true;
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fusePosData = true;
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fuseHgtData = true;
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}
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// Don't wait longer than HGTmsecMax msec between height updates
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// if no GPS
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else if ((IMUmsec - HGTmsecPrev) >= HGTmsecMax)
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if (newDataHgt)
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{
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// Static mode is used for pre-arm and bench testing and allows operation
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// without GPS
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if (staticMode) {
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fuseVelData = true;
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fusePosData = true;
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fuseHgtData = true;
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}
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else {
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fuseVelData = false;
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fusePosData = false;
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fuseHgtData = true;
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}
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HGTmsecPrev = IMUmsec;
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}
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else
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{
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fuseVelData = false;
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fusePosData = false;
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fuseHgtData = false;
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fuseHgtData = true;
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}
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// set flag to let other processes know that GPS and/or height fusion has
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// ocurred in this frame
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@ -294,6 +277,7 @@ void NavEKF::SelectVelPosFusion()
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{
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FuseVelPosNED();
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newDataGps = false;
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newDataHgt = false;
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posVelFuseStep = true;
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}
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else
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@ -1958,14 +1942,16 @@ void NavEKF::readGpsData()
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void NavEKF::readHgtData()
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{
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// ToDo do we check for new height data or grab a height measurement?
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// ToDo - better check for new height data
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// Best to do this at the same time as GPS measurement fusion for efficiency
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hgtMea = _baro.get_altitude();
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#if 0
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Vector3f pos;
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getPosNED(pos);
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//::printf("BARO.Alt=%.2f REL.z=%.2f\n", hgtMea, -pos.z);
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#endif
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if (hgtMeaPrev != hgtMea) {
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newDataHgt == true;
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hgtMeaPrev = hgtMea;
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}
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else {
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newDataHgt == false;
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}
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// recall states from compass measurement time
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RecallStates(statesAtHgtTime, (IMUmsec - msecHgtDelay));
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}
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@ -201,7 +201,7 @@ private:
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ftype _windStateNoise; // rate of change of wind : m/s^2
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ftype _wndVarHgtRateScale; // scale factor applied to wind process noise from height rate
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ftype _gyrNoise; // gyro process noise : rad/s
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ftype _accNoise; // accelerometer process noise : m/s^2
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ftype _accNoise; // accelerometer process noise : m/s^2hgtHealth = (sq(hgtInnov) < maxf((100.0f * varInnovVelPos[5])) , 5.0f);
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ftype _dAngBiasNoise; // gyro bias state noise : rad/s^2
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ftype _magEarthNoise; // earth magnetic field process noise : gauss/sec
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ftype _magBodyNoise; // earth magnetic field process noise : gauss/sec
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@ -297,6 +297,10 @@ private:
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// TAS input variables
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bool newDataTas;
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// HGT input variables
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float hgtMeaPrev;
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bool newDataHgt;
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// Time stamp when vel, pos or height measurements last failed checks
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uint32_t velFailTime;
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uint32_t posFailTime;
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