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@ -230,9 +230,9 @@ PARAM_DEFINE_FLOAT(NPFG_SW_DST_MLT, 0.32f);
@@ -230,9 +230,9 @@ PARAM_DEFINE_FLOAT(NPFG_SW_DST_MLT, 0.32f);
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PARAM_DEFINE_FLOAT(NPFG_PERIOD_SF, 1.5f); |
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/**
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* Cruise throttle |
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* Trim throttle |
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* |
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* This is the throttle setting required to achieve the desired cruise speed. Most airframes have a value of 0.5-0.7. |
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* This is the throttle setting required to achieve FW_AIRSPD_TRIM during level flight. Most airframes have a value of 0.5-0.7. |
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* |
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* @unit norm |
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* @min 0.0 |
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@ -241,25 +241,7 @@ PARAM_DEFINE_FLOAT(NPFG_PERIOD_SF, 1.5f);
@@ -241,25 +241,7 @@ PARAM_DEFINE_FLOAT(NPFG_PERIOD_SF, 1.5f);
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* @increment 0.01 |
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* @group FW L1 Control |
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*/ |
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PARAM_DEFINE_FLOAT(FW_THR_CRUISE, 0.6f); |
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/**
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* Scale throttle by pressure change |
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* |
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* Automatically adjust throttle to account for decreased air density at higher altitudes. |
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* Start with a scale factor of 1.0 and adjust for different propulsion systems. |
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* |
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* When flying without airspeed sensor this will help to keep a constant performance over large altitude ranges. |
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* |
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* The default value of 0 will disable scaling. |
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* |
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* @min 0.0 |
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* @max 10.0 |
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* @decimal 1 |
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* @increment 0.1 |
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* @group FW L1 Control |
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*/ |
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PARAM_DEFINE_FLOAT(FW_THR_ALT_SCL, 0.0f); |
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PARAM_DEFINE_FLOAT(FW_THR_TRIM, 0.6f); |
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/**
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* Throttle max slew rate |
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