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https://gitee.com/mirrors_PX4/PX4-Autopilot.git
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Updated estimator, not using optical flow for now until proven on the bench
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File diff suppressed because one or more lines are too long
@@ -20,7 +20,7 @@ public:
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float z;
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float length(void) const;
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Vector3f zero(void) const;
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void zero(void);
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};
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class Mat3f
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@@ -93,9 +93,6 @@ public:
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float covTimeStepMax; // maximum time allowed between covariance predictions
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float covDelAngMax; // maximum delta angle between covariance predictions
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float rngFinderPitch; // pitch angle of laser range finder in radians. Zero is aligned with the Z body axis. Positive is RH rotation about Y body axis.
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float a1; // optical flow sensor misalgnment angle about X axis (rad)
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float a2; // optical flow sensor misalgnment angle about Y axis (rad)
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float a3; // optical flow sensor misalgnment angle about Z axis (rad)
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float yawVarScale;
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float windVelSigma;
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@@ -122,10 +119,6 @@ public:
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covTimeStepMax = 0.07f; // maximum time allowed between covariance predictions
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covDelAngMax = 0.02f; // maximum delta angle between covariance predictions
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rngFinderPitch = 0.0f; // pitch angle of laser range finder in radians. Zero is aligned with the Z body axis. Positive is RH rotation about Y body axis.
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a1 = 0.0f; // optical flow sensor misalgnment angle about X axis (rad)
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a2 = 0.0f; // optical flow sensor misalgnment angle about Y axis (rad)
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a3 = 0.0f; // optical flow sensor misalgnment angle about Z axis (rad)
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EAS2TAS = 1.0f;
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yawVarScale = 1.0f;
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@@ -165,7 +158,6 @@ public:
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float statesAtMagMeasTime[n_states]; // filter satates at the effective measurement time
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float statesAtVtasMeasTime[n_states]; // filter states at the effective measurement time
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float statesAtRngTime[n_states]; // filter states at the effective measurement time
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float statesAtLosMeasTime[n_states]; // filter states at the effective measurement time
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Vector3f correctedDelAng; // delta angles about the xyz body axes corrected for errors (rad)
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Vector3f correctedDelVel; // delta velocities along the XYZ body axes corrected for errors (m/s)
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@@ -192,14 +184,11 @@ public:
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float rngMea; // Ground distance
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float posNED[3]; // North, East Down position (m)
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float innovMag[3]; // innovation output for magnetometer measurements
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float varInnovMag[3]; // innovation variance output for magnetometer measurements
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float varInnovLOS[2]; // innovation variance output for optical flow measurements
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float innovMag[3]; // innovation output
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float varInnovMag[3]; // innovation variance output
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Vector3f magData; // magnetometer flux radings in X,Y,Z body axes
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float innovVtas; // innovation output for true airspeed measurements
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float innovRng; ///< Range finder innovation for rnge finder measurements
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float innovLOS[2]; // Innovations for optical flow LOS rate measurements
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float losData[2]; // Optical flow LOS rate measurements
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float innovVtas; // innovation output
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float innovRng; ///< Range finder innovation
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float varInnovVtas; // innovation variance output
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float VtasMeas; // true airspeed measurement (m/s)
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double latRef; // WGS-84 latitude of reference point (rad)
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@@ -227,14 +216,12 @@ public:
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bool fuseMagData; // boolean true when magnetometer data is to be fused
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bool fuseVtasData; // boolean true when airspeed data is to be fused
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bool fuseRngData; ///< true when range data is fused
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bool fuseOptData; // true when optical flow data is fused
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bool onGround; ///< boolean true when the flight vehicle is on the ground (not flying)
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bool staticMode; ///< boolean true if no position feedback is fused
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bool useAirspeed; ///< boolean true if airspeed data is being used
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bool useCompass; ///< boolean true if magnetometer data is being used
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bool useRangeFinder; ///< true when rangefinder is being used
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bool useOpticalFlow; // true when optical flow data is being used
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struct ekf_status_report current_ekf_state;
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struct ekf_status_report last_ekf_error;
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