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updated calculation
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@@ -73,7 +73,7 @@ void Ekf::fuseAirspeed()
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if (v_tas_pred > 3.0f) {
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// Calculate the observation jacobian
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// intermediate variable from algebraic optimisation
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SH_TAS[0] = 1 / (sqrt(sq(ve - vwe) + sq(vn - vwn) + sq(vd)));
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SH_TAS[0] = 1 / v_tas_pred;
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SH_TAS[1] = (SH_TAS[0] * (2 * ve - 2 * vwe)) / 2.0f;
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SH_TAS[2] = (SH_TAS[0] * (2 * vn - 2 * vwn)) / 2.0f;
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