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Apply small suggestions from code review
Further param description improvements. Co-authored-by: Matthias Grob <maetugr@gmail.com>
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co-authored by
Matthias Grob
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@@ -43,8 +43,8 @@
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/**
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* Use fixed-wing actuation in hover to accelerate forward
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*
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* This feature can be used to avoid the plane having to pitch down in order to move forward.
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* Prevents large, negative lift from pitching down into wind.
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* This feature can be used to avoid the plane having to pitch nose down in order to move forward.
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* Prevents large, negative lift from pitching nose down into wind.
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* Fixed-wing forward actuators refers to puller/pusher (standard VTOL), or forward-tilt (tiltrotor VTOL).
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* Only active if demanded down pitch is below VT_PITCH_MIN.
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* Use VT_FWD_THRUST_SC to tune it.
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@@ -278,7 +278,7 @@ PARAM_DEFINE_INT32(VT_FW_QC_R, 0);
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*
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* Maximum height above the ground (if available, otherwhise above
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* home if available, otherwise above the local origin) where triggering a quadchute is possible.
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* At high altitudes there is a big risk to deplete the battery and therefore crash if in quad-chuting there.
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* At high altitudes there is a big risk to deplete the battery and therefore crash if quad-chuting there.
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*
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* @unit m
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* @min 0
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