FIELD: aviation.
SUBSTANCE: invention relates to a method of controlling low-altitude flight of an aircraft in a vertical plane. To control low-altitude flight, parameters of aircraft proper state vector and environment are determined, probability of death of ergatic system "operator-aircraft", generating control actions on actuating systems of aircraft, lower and upper hazard limits are determined, a reference trajectory is determined and a low-altitude flight safety corridor is formed, determining the current and predicted normalized error of maintaining the reference trajectory and adaptive boundaries of special flight situations, calculating the current and predicted value of the quantitative assessment of the probability of the destruction of the system and comparing them with the values at the boundaries of special situations for the formed safety corridor, information is output to the indicator of the safety corridor, control actions are generated on the actuating systems of the aircraft for return to the reference trajectory and elimination of special situations.
EFFECT: increasing aircraft flight safety when performing low-altitude flights.
1 cl, 2 dwg
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Authors
Dates
2024-07-15—Published
2023-11-20—Filed