mirror of
https://github.com/PX4/PX4-Autopilot.git
synced 2026-06-09 20:04:05 +08:00
File diff suppressed because it is too large
Load Diff
@@ -29,6 +29,10 @@ public:
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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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float dAngBiasSigma;
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@@ -55,6 +59,9 @@ public:
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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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EAS2TAS = 1.0f;
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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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yawVarScale = 1.0f;
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windVelSigma = 0.1f;
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@@ -115,6 +122,7 @@ 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 statesAtOptFlowTime[n_states]; // States at the effective optical flow 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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@@ -147,9 +155,13 @@ public:
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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 losData[2]; // optical flow LOS rate measurements (rad/sec)
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float innovVtas; // innovation output
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float innovRng; ///< Range finder innovation
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float innovOptFlow[2]; // optical flow LOS innovations (rad/sec)
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float varInnovOptFlow[2]; // optical flow innovations variances (rad/sec)^2
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float varInnovVtas; // innovation variance output
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float varInnovRng; // range finder innovation variance
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float VtasMeas; // true airspeed measurement (m/s)
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float magDeclination; ///< magnetic declination
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double latRef; // WGS-84 latitude of reference point (rad)
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@@ -178,12 +190,18 @@ 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 fuseOptFlowData; // true when optical flow data is fused
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bool inhibitWindStates; // true when wind states and covariances are to remain constant
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bool inhibitMagStates; // true when magnetic field states and covariances are to remain constant
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bool inhibitGndHgtState; // true when the terrain ground height offset state and covariances are to remain constant
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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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bool ekfDiverged;
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uint64_t lastReset;
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@@ -208,7 +226,7 @@ void FuseAirspeed();
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void FuseRangeFinder();
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void FuseOpticalFlow();
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void FuseOptFlow();
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void zeroRows(float (&covMat)[n_states][n_states], uint8_t first, uint8_t last);
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@@ -8,6 +8,7 @@
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#ifdef EKF_DEBUG
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#include <stdio.h>
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#include <stdarg.h>
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static void
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ekf_debug_print(const char *fmt, va_list args)
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@@ -101,6 +102,25 @@ Vector3f operator*( Mat3f matIn, Vector3f vecIn)
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return vecOut;
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}
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// overload * operator to provide a matrix product
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Mat3f operator*( Mat3f matIn1, Mat3f matIn2)
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{
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Mat3f matOut;
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matOut.x.x = matIn1.x.x*matIn2.x.x + matIn1.x.y*matIn2.y.x + matIn1.x.z*matIn2.z.x;
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matOut.x.y = matIn1.x.x*matIn2.x.y + matIn1.x.y*matIn2.y.y + matIn1.x.z*matIn2.z.y;
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matOut.x.z = matIn1.x.x*matIn2.x.z + matIn1.x.y*matIn2.y.z + matIn1.x.z*matIn2.z.z;
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matOut.y.x = matIn1.y.x*matIn2.x.x + matIn1.y.y*matIn2.y.x + matIn1.y.z*matIn2.z.x;
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matOut.y.y = matIn1.y.x*matIn2.x.y + matIn1.y.y*matIn2.y.y + matIn1.y.z*matIn2.z.y;
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matOut.y.z = matIn1.y.x*matIn2.x.z + matIn1.y.y*matIn2.y.z + matIn1.y.z*matIn2.z.z;
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matOut.z.x = matIn1.z.x*matIn2.x.x + matIn1.z.y*matIn2.y.x + matIn1.z.z*matIn2.z.x;
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matOut.z.y = matIn1.z.x*matIn2.x.y + matIn1.z.y*matIn2.y.y + matIn1.z.z*matIn2.z.y;
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matOut.z.z = matIn1.z.x*matIn2.x.z + matIn1.z.y*matIn2.y.z + matIn1.z.z*matIn2.z.z;
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return matOut;
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}
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// overload % operator to provide a vector cross product
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Vector3f operator%( Vector3f vecIn1, Vector3f vecIn2)
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{
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@@ -41,6 +41,7 @@ Vector3f operator*(float sclIn1, Vector3f vecIn1);
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Vector3f operator+( Vector3f vecIn1, Vector3f vecIn2);
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Vector3f operator-( Vector3f vecIn1, Vector3f vecIn2);
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Vector3f operator*( Mat3f matIn, Vector3f vecIn);
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Mat3f operator*( Mat3f matIn1, Mat3f matIn2);
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Vector3f operator%( Vector3f vecIn1, Vector3f vecIn2);
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Vector3f operator*(Vector3f vecIn1, float sclIn1);
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@@ -79,4 +80,4 @@ struct ekf_status_report {
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bool velOffsetExcessive;
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};
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void ekf_debug(const char *fmt, ...);
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void ekf_debug(const char *fmt, ...);
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