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Airspeed selector: remove ASPD_STALL and replace by FW_AIRSPD_STALL
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
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@@ -433,7 +433,8 @@ PARAM_DEFINE_FLOAT(FW_LND_THRTC_SC, 1.0f);
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/**
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* Minimum Airspeed (CAS)
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*
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* If the CAS (calibrated airspeed) falls below this value, the TECS controller will try to
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* The minimal airspeed (calibrated airspeed) the user is able to command.
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* Further, if the 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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@@ -476,6 +477,22 @@ PARAM_DEFINE_FLOAT(FW_AIRSPD_MAX, 20.0f);
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*/
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PARAM_DEFINE_FLOAT(FW_AIRSPD_TRIM, 15.0f);
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/**
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* Stall Airspeed (CAS)
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*
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* The stall airspeed (calibrated airspeed) of the vehicle.
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* It is used for airspeed sensor failure detection and for the control
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* surface scaling airspeed limits.
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*
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* @unit m/s
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* @min 0.5
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* @max 40
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* @decimal 1
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* @increment 0.5
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* @group FW TECS
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*/
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PARAM_DEFINE_FLOAT(FW_AIRSPD_STALL, 7.0f);
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/**
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* Maximum climb rate
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*
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