What does the F-16 (perhaps other fighters as well) use to decide when to deploy leading edge flaps? I would assume angle of attack, airspeed, stick deflection, or some combination of the three, are the main factors.
Technically, F-16 and "similar fighters" have leading edge flaps (LEF) (or droop flaps), rather than slats. The difference is that they don't form a gap between themselves and the main surface when deflected. This makes them usable at high speeds, whereas slats are typically used for low-speed takeoff/landing.
For fighters, the most important use for them is to extend the range of usable angles of attack (AoA), which is important for manoeuvring as well as for takeoff/landing.
For F-16, @Mr R posted some details. I have some info for Soviet fighters of the same generation.
LEFs have two positions, up and down (20°). They are deployed:
- When landing gear is down (including takeoff and landing).
- Automatically in flight when AoA > 9° and M < 0.8 (Mach number).
- On manual override by the pilot.
LEF on Su-27 don't have fixed positions and constantly track AoA in flight. Maximum deflection 30°.
They are automatically deployed to 3/4 of travel when landing gear is down for takeoff or landing.
The pilot has a manual override (down-auto-up selector).
For both aircraft, if LEF fail, the allowed AoA is limited to 10°, which is roughly half the normal (depending on speed).
According to a F16 forum..
Those are the LEF's (leading edge flaps). They are there to produce extra lift to the wings during high AOA and low airspeeds. The reason they are up on the ground is they are wired to the left and right main WOW (weight on wheels) switches. They are schedule to -2 degrees on the ground. The only time they move on the ground is during FLCS self test or during LEF ops checks. In flight they are scheduled as a function of AOA and airspeed.
OR AoA and Mach Number (rather than airspeed).
For the F-16 only talk, the wings must be at an angle of attack more than 9 degrees slower speed or more if you are making a turn but no more than Mach 0. 95 above this value is upward 2 degrees and locked. For the F 16 with TO /Landing gains(landing gear and trailing flaps _flaperons _at 20 degrees down, the Leading Edge Flaps are 15 degrees down - on speed - if not will vary depending on the AOA or weight on wheels = upward 2 degrees ).