FIELD: aircrafts.
SUBSTANCE: inventions group relates to a method and device for controlling the flight of a group of aircraft. For flight control, set the true geometric height, the desired value of the track angle and the maximum allowable deviation from it, set the minimum allowable distance between aircraft and the minimum allowable distance to the terrain, set the aircraft identifiers and the distance that determines the radius of the area centered at the location of the aircraft device, measure the current value of the track angle and the rate of its change, determine the coordinates of the aircraft and transmit them to other aircraft, receive coordinates from other aircraft, together with their identifiers, determine the difference in slant ranges from the left and right sides of the wing and the rate of its change , form and transmit a control signal to the rudder, taking into account the trajectories and motion parameters of other aircraft. The device contains three slant range meters, an adder, a differentiator, a block for setting control parameters, a module for generating a control signal to the rudder, a rudder, a device for receiving/transmitting information about the aircraft, an inertial navigation system, a module for calculating sectors of permitted directions of movement, a module for implementing the correlation extreme method, connected in a certain way.
EFFECT: increased flight safety while minimizing the flight altitude.
2 cl, 2 dwg
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Authors
Dates
2022-12-19—Published
2022-05-23—Filed