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@ -359,12 +359,12 @@ PARAM_DEFINE_INT32(VT_MC_ON_FMU, 0);
@@ -359,12 +359,12 @@ PARAM_DEFINE_INT32(VT_MC_ON_FMU, 0);
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* @max 45.0 |
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* @group VTOL Attitude Control |
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*/ |
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PARAM_DEFINE_FLOAT(VT_PTCH_MIN, -5.0f); |
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PARAM_DEFINE_FLOAT(VT_PITCH_MIN, -5.0f); |
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/**
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* Minimum pitch angle during hover landing. |
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* |
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* Overrides VT_PTCH_MIN when the vehicle is in LAND mode (hovering). |
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* Overrides VT_PITCH_MIN when the vehicle is in LAND mode (hovering). |
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* During landing it can be beneficial to allow lower minimum pitch angles as it can avoid the wings |
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* generating too much lift and preventing the vehicle from sinking at the desired rate. |
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* |
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@ -372,7 +372,7 @@ PARAM_DEFINE_FLOAT(VT_PTCH_MIN, -5.0f);
@@ -372,7 +372,7 @@ PARAM_DEFINE_FLOAT(VT_PTCH_MIN, -5.0f);
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* @max 45.0 |
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* @group VTOL Attitude Control |
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*/ |
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PARAM_DEFINE_FLOAT(VT_LND_PTCH_MIN, -5.0f); |
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PARAM_DEFINE_FLOAT(VT_LND_PITCH_MIN, -5.0f); |
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/**
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* Spoiler setting while landing (hover) |
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