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FW attitude controller: remove unused control_input.scaler
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
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@@ -447,7 +447,6 @@ void FixedwingAttitudeControl::Run()
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control_input.airspeed_min = _param_fw_airspd_stall.get();
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control_input.airspeed_max = _param_fw_airspd_max.get();
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control_input.airspeed = airspeed;
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control_input.scaler = _airspeed_scaling;
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control_input.lock_integrator = lock_integrator;
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if (wheel_control) {
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@@ -67,7 +67,6 @@ struct ECL_ControlData {
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float airspeed_min;
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float airspeed_max;
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float airspeed;
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float scaler;
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float groundspeed;
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float groundspeed_scaler;
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bool lock_integrator;
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