FIELD: aviation.
SUBSTANCE: invention relates to a method of controlling longitudinal motion of aircraft at landing. For control of longitudinal movement of aircraft during landing, a main control signal is transmitted to drive elevator, target altitude flight is formed and adaptively monitoring by determining and minimising angle between vector of trajectory flight speed and direction to program simulated target, moving in preset path at specified distance from centre of mass of aircraft, auxiliary signal is formed on drive sections of interceptors during capture and stabilisation of glide path, alignment with implementation of approach on second wheel if necessary.
EFFECT: aircraft landing.
1 cl, 7 dwg
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