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@ -418,9 +418,9 @@ PARAM_DEFINE_FLOAT(FW_LND_THRTC_SC, 1.0f);
@@ -418,9 +418,9 @@ PARAM_DEFINE_FLOAT(FW_LND_THRTC_SC, 1.0f);
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/**
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* Minimum Airspeed |
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* Minimum Airspeed (CAS) |
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* |
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* If the airspeed falls below this value, the TECS controller will try to |
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* If the CAS (calibrated airspeed) falls below this value, the TECS controller will try to |
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* increase airspeed more aggressively. |
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* |
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* @unit m/s |
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@ -433,9 +433,9 @@ PARAM_DEFINE_FLOAT(FW_LND_THRTC_SC, 1.0f);
@@ -433,9 +433,9 @@ PARAM_DEFINE_FLOAT(FW_LND_THRTC_SC, 1.0f);
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PARAM_DEFINE_FLOAT(FW_AIRSPD_MIN, 10.0f); |
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/**
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* Maximum Airspeed |
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* Maximum Airspeed (CAS) |
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* |
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* If the airspeed is above this value, the TECS controller will try to decrease |
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* If the CAS (calibrated airspeed) is above this value, the TECS controller will try to decrease |
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* airspeed more aggressively. |
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* |
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* @unit m/s |
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@ -448,9 +448,11 @@ PARAM_DEFINE_FLOAT(FW_AIRSPD_MIN, 10.0f);
@@ -448,9 +448,11 @@ PARAM_DEFINE_FLOAT(FW_AIRSPD_MIN, 10.0f);
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PARAM_DEFINE_FLOAT(FW_AIRSPD_MAX, 20.0f); |
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/**
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* Cruise Airspeed |
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* Cruise Airspeed (CAS) |
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* |
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* The fixed wing controller tries to fly at this airspeed. |
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* The trim CAS (calibrated airspeed) of the vehicle. If an airspeed controller is active, |
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* this is the default airspeed setpoint that the controller will try to achieve if |
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* no other airspeed setpoint sources are present (e.g. through non-centered RC sticks). |
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* |
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* @unit m/s |
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* @min 0.0 |
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