FIELD: aircraft engineering.
SUBSTANCE: claimed invention is meant for control over manned aircraft or drones in low-altitude flight with flyby over the set of obstacles in vertical plane. The flight is path is set with selected pitch angles. Selected path is corrected at approach to said set of obstacles to be approximated by semi-ellipse. Pitch angle increment is computed by a definite rule. Pitch angle is corrected in a definite way starting from the moment when the distance from controlled drone to the centre of approximating ellipse is smaller than preset magnitude.
EFFECT: higher survivability in low-altitude flight.
3 dwg
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