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@ -225,10 +225,10 @@ PARAM_DEFINE_FLOAT(FW_THR_MIN, 0.0f);
@@ -225,10 +225,10 @@ PARAM_DEFINE_FLOAT(FW_THR_MIN, 0.0f);
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PARAM_DEFINE_FLOAT(FW_THR_IDLE, 0.15f); |
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/**
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* Throttle limit value before flare |
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* Throttle limit during landing below throttle limit altitude |
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* |
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* This throttle value will be set as throttle limit at FW_LND_TLALT, |
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* before aircraft will flare. |
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* During the flare of the autonomous landing process, this value will be set |
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* as throttle limit when the aircraft altitude is below FW_LND_TLALT. |
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* |
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* @unit norm |
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* @min 0.0 |
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@ -332,7 +332,7 @@ PARAM_DEFINE_INT32(FW_LND_USETER, 0);
@@ -332,7 +332,7 @@ PARAM_DEFINE_INT32(FW_LND_USETER, 0);
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* Flare, minimum pitch |
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* |
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* Minimum pitch during flare, a positive sign means nose up |
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* Applied once FW_LND_TLALT is reached |
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* Applied once FW_LND_FLALT is reached |
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* |
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* @unit deg |
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* @min 0 |
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@ -347,7 +347,7 @@ PARAM_DEFINE_FLOAT(FW_LND_FL_PMIN, 2.5f);
@@ -347,7 +347,7 @@ PARAM_DEFINE_FLOAT(FW_LND_FL_PMIN, 2.5f);
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* Flare, maximum pitch |
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* |
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* Maximum pitch during flare, a positive sign means nose up |
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* Applied once FW_LND_TLALT is reached |
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* Applied once FW_LND_FLALT is reached |
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* |
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* @unit deg |
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* @min 0 |
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