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@ -1014,23 +1014,21 @@ PARAM_DEFINE_FLOAT(WEIGHT_GROSS, -1.0f);
@@ -1014,23 +1014,21 @@ PARAM_DEFINE_FLOAT(WEIGHT_GROSS, -1.0f);
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* This is used for limiting the roll setpoint near the ground. (if multiple wings, take the longest span) |
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* |
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* @unit m |
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* @min 1.0 |
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* @max 15.0 |
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* @min 0.1 |
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* @decimal 1 |
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* @increment 0.1 |
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* @group FW Geometry |
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*/ |
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PARAM_DEFINE_FLOAT(FW_WING_SPAN, 6.0); |
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PARAM_DEFINE_FLOAT(FW_WING_SPAN, 3.0); |
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/**
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* Height (AGL) of the wings when the aircraft is on the ground. |
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* |
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* This is used to constrain a minimum altitude below which we keep wings level to avoid wing tip strike. It's prudent |
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* This is used to constrain a minimum altitude below which we keep wings level to avoid wing tip strike. It's safer |
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* to give a slight margin here (> 0m) |
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* |
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* @unit m |
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* @min 0.0 |
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* @max 5.0 |
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* @decimal 1 |
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* @increment 1 |
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* @group FW Geometry |
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