FIELD: transport.
SUBSTANCE: invention relates to application of drones and can be used for continuous control over conditions of oil- and gas-lines, storages, high-voltage lines and similar long structures. Proposed method comprises measurement of flight altitude H, horizontal distance to design distance to touch-down point D, deviation from vertical plane extending through runway axis ΔZ, definition of three velocity components and acceleration at touch-down point, generation of pilot path of lower flight H0(D,D0) and Z0(D,D0) from the point of landing start at the distance D0 reference tough-down point, definition of drone deviation from reference landing part Δh=H-H0(D,D0) and ΔZ=Z-Z0(D,D0), generation of control signals proceeding from measurement results and feeding them to drone control surfaces. Drone landing path cross-section is set as a circle located on the plane perpendicular to reference part and with centre at landing reference line. In case the drone flies out from reference cross-section a new landing part is generated.
EFFECT: higher reliability and safety.
3 cl, 2 dwg
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Authors
Dates
2014-01-10—Published
2012-02-02—Filed