AP_NavEKF3: move tasHealth to be a stack variable
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@ -32,9 +32,6 @@ void NavEKF3_core::FuseAirspeed()
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Vector24 H_TAS = {};
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float VtasPred;
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// health is set bad until test passed
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tasHealth = false;
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// copy required states to local variable names
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vn = stateStruct.velocity.x;
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ve = stateStruct.velocity.y;
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@ -129,7 +126,7 @@ void NavEKF3_core::FuseAirspeed()
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tasTestRatio = sq(innovVtas) / (sq(MAX(0.01f * (float)frontend->_tasInnovGate, 1.0f)) * varInnovVtas);
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// fail if the ratio is > 1, but don't fail if bad IMU data
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tasHealth = ((tasTestRatio < 1.0f) || badIMUdata);
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bool tasHealth = ((tasTestRatio < 1.0f) || badIMUdata);
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tasTimeout = (imuSampleTime_ms - lastTasPassTime_ms) > frontend->tasRetryTime_ms;
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// test the ratio before fusing data, forcing fusion if airspeed and position are timed out as we have no choice but to try and use airspeed to constrain error growth
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@ -938,7 +938,6 @@ private:
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// Variables
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bool statesInitialised; // boolean true when filter states have been initialised
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bool magHealth; // boolean true if magnetometer has passed innovation consistency check
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bool tasHealth; // boolean true if true airspeed has passed innovation consistency check
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bool velTimeout; // boolean true if velocity measurements have failed innovation consistency check and timed out
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bool posTimeout; // boolean true if position measurements have failed innovation consistency check and timed out
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bool hgtTimeout; // boolean true if height measurements have failed innovation consistency check and timed out
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