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@ -241,7 +241,14 @@ PARAM_DEFINE_FLOAT(MT_FPA_MAX, 30.0f);
@@ -241,7 +241,14 @@ PARAM_DEFINE_FLOAT(MT_FPA_MAX, 30.0f);
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* |
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* @group mTECS |
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*/ |
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PARAM_DEFINE_FLOAT(MT_A_LP, 1.0f); |
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PARAM_DEFINE_FLOAT(MT_A_LP, 0.5f); |
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/**
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* Airspeed derivative calculation lowpass |
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* |
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* @group mTECS |
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*/ |
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PARAM_DEFINE_FLOAT(MT_AD_LP, 0.5f); |
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/**
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* P gain for the airspeed control |
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@ -268,7 +275,7 @@ PARAM_DEFINE_FLOAT(MT_ACC_D, 0.0f);
@@ -268,7 +275,7 @@ PARAM_DEFINE_FLOAT(MT_ACC_D, 0.0f);
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* |
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* @group mTECS |
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*/ |
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PARAM_DEFINE_FLOAT(MT_ACC_D_LP, 1.0f); |
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PARAM_DEFINE_FLOAT(MT_ACC_D_LP, 0.5f); |
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/**
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* Minimal acceleration (air) |
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@ -286,13 +293,6 @@ PARAM_DEFINE_FLOAT(MT_ACC_MIN, -40.0f);
@@ -286,13 +293,6 @@ PARAM_DEFINE_FLOAT(MT_ACC_MIN, -40.0f);
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*/ |
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PARAM_DEFINE_FLOAT(MT_ACC_MAX, 40.0f); |
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/**
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* Airspeed derivative calculation lowpass |
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* |
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* @group mTECS |
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*/ |
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PARAM_DEFINE_FLOAT(MT_AD_LP, 1.0f); |
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/**
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* Minimal throttle during takeoff |
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* |
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