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change name to true_airspeed
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@@ -132,7 +132,7 @@ void Ekf::fuseAirspeed()
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// calculate measurement innovation
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_airspeed_innov = v_tas_pred - _airspeed_sample_delayed.airspeed; // This is TAS, maybe we should indicate that in some way
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_airspeed_innov = v_tas_pred - _airspeed_sample_delayed.true_airspeed;
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// Calculate the innovation variance
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_airspeed_innov_var = 1.0f / SK_TAS[0];
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