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fix(fw_att_control): fix comments / docs
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@@ -207,7 +207,6 @@ void FixedwingAttitudeControl::Run()
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dt = math::constrain((att.timestamp_sample - _last_run) * 1e-6f, DT_MIN, DT_MAX);
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_last_run = att.timestamp_sample;
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// get current rotation matrix from control state quaternions
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_R = matrix::Quatf(att.q);
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}
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