TL Elektronic Integra Efis TL-6560, Руководство по настройке

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Page 35
Autopilot Section
Pitch Axis Setup
Mode-Longitudinal Angle
If you select this mode, the AP will control the aircraft according to parameter Max. Longitudinal Angle(described below).
Max. Longitudinal Angle
The parameter determines angle between longitudinal axis of the aircraft in horizontal flight and longitudinal axis of the aircraft when the AP
pitches the aircraft up or down during controlled altitude change. If Mode-Longitudinal Angle is set, parameter Max. Longitudinal Angle is
activated.
Max. Climb Speed/Max. Descent Speed
If Mode-Vertical Speed is selected, Max. Climb Speed and Max. Descent Speed will be used for reduction of Vertical Speed during climb or
descent of the aircraft.
Min. Air Speed
Min. Air Speed is minimum airspeed at which you can activated the AP.
If actual airspeed is lower than set Min. Air Speed , the AP will pitch the aircraft down to increase actual airspeed.
If aircraft’s altitude is lower than altitude determined by Altitude Bug or Navigation source(VOR or GPS) and the AP can’t pitch the aircraft up
without dropping below Min. Air. Speed , the Integra will display message “ADD POWER”.
The Min. Air Speed must be set to (at least) 30% above Vs. This is default setting of Min. Air Speed value.
Max. Air Speed
Max. Air Speed is maximum airspeed at which you can activated the AP.
If actual airspeed is higher than set Max. Air Speed , the AP will pitch the aircraft up to decrease actual airspeed.
If aircraft’s altitude is higher than altitude determined by Altitude Bug or Navigation source(VOR or GPS) and the AP can’t pitch the aircraft
down without Max. Air. Speed get exceed , the Integra will display message “REDUCE POWER”.
The Max. Air Speed must be set to (at most) 95% of Vne. This is default setting of Max. Air Speed value.