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@ -65,7 +65,7 @@ PARAM_DEFINE_INT32(MT_ENABLED, 1);
@@ -65,7 +65,7 @@ PARAM_DEFINE_INT32(MT_ENABLED, 1);
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* @max 10.0 |
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* @group mTECS |
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*/ |
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PARAM_DEFINE_FLOAT(MT_THR_FF, 0.2f); |
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PARAM_DEFINE_FLOAT(MT_THR_FF, 0.7f); |
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/**
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* Total Energy Rate Control P |
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@ -75,7 +75,7 @@ PARAM_DEFINE_FLOAT(MT_THR_FF, 0.2f);
@@ -75,7 +75,7 @@ PARAM_DEFINE_FLOAT(MT_THR_FF, 0.2f);
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* @max 10.0 |
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* @group mTECS |
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*/ |
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PARAM_DEFINE_FLOAT(MT_THR_P, 0.03f); |
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PARAM_DEFINE_FLOAT(MT_THR_P, 0.1f); |
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/**
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* Total Energy Rate Control I |
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@ -85,7 +85,7 @@ PARAM_DEFINE_FLOAT(MT_THR_P, 0.03f);
@@ -85,7 +85,7 @@ PARAM_DEFINE_FLOAT(MT_THR_P, 0.03f);
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* @max 10.0 |
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* @group mTECS |
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*/ |
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PARAM_DEFINE_FLOAT(MT_THR_I, 0.1f); |
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PARAM_DEFINE_FLOAT(MT_THR_I, 0.25f); |
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/**
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* Total Energy Rate Control Offset (Cruise throttle sp) |
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@ -104,7 +104,7 @@ PARAM_DEFINE_FLOAT(MT_THR_OFF, 0.7f);
@@ -104,7 +104,7 @@ PARAM_DEFINE_FLOAT(MT_THR_OFF, 0.7f);
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* @max 10.0 |
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* @group mTECS |
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*/ |
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PARAM_DEFINE_FLOAT(MT_PIT_FF, 0.1f); |
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PARAM_DEFINE_FLOAT(MT_PIT_FF, 0.4f); |
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/**
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* Energy Distribution Rate Control P |
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@ -182,7 +182,7 @@ PARAM_DEFINE_FLOAT(MT_PIT_MAX, 20.0f);
@@ -182,7 +182,7 @@ PARAM_DEFINE_FLOAT(MT_PIT_MAX, 20.0f);
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* @max 10.0f |
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* @group mTECS |
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*/ |
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PARAM_DEFINE_FLOAT(MT_FPA_P, 0.2f); |
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PARAM_DEFINE_FLOAT(MT_FPA_P, 0.3f); |
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/**
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* D gain for the altitude control |
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@ -210,7 +210,7 @@ PARAM_DEFINE_FLOAT(MT_FPA_D_LP, 1.0f);
@@ -210,7 +210,7 @@ PARAM_DEFINE_FLOAT(MT_FPA_D_LP, 1.0f);
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* @unit deg |
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* @group mTECS |
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*/ |
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PARAM_DEFINE_FLOAT(MT_FPA_MIN, -10.0f); |
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PARAM_DEFINE_FLOAT(MT_FPA_MIN, -20.0f); |
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/**
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* Maximal flight path angle setpoint |
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@ -237,7 +237,7 @@ PARAM_DEFINE_FLOAT(MT_A_LP, 1.0f);
@@ -237,7 +237,7 @@ PARAM_DEFINE_FLOAT(MT_A_LP, 1.0f);
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* @max 10.0f |
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* @group mTECS |
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*/ |
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PARAM_DEFINE_FLOAT(MT_ACC_P, 1.5f); |
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PARAM_DEFINE_FLOAT(MT_ACC_P, 0.3f); |
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/**
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* D gain for the airspeed control |
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