FIELD: controlling.
SUBSTANCE: invention relates to the field of control of weaponry of tactical aircrafts. Possible missile launch areas in conditions of covert surveillance of the target are determined based on indirect determination of the range to the target and comparison of the current values of the range and angular positions of the aircraft with the preset values determining the boundaries of the missile launch areas. The characteristics of movement of the target are determined based on the analysis of the dynamics of changes in the angular positions of the target in the plane of attack, and if the parameters of accelerated movement of the target are identified, at least five records are made of the angular positions of the target and the base distances flown by the aircraft relative to the reference points of the trajectory of movement thereof. The areas of convergence relative to the reference points, the parameters of the mutual position of the aerial vehicles in the convergence sections: vectors of the ranges to the target, distances, base distances flown by the target and the aircraft, are determined. The range to the target is determined. The weaponry control system additionally comprises a unit for determining the possible missile launch areas in conditions of covert surveillance of the target.
EFFECT: functional capabilities of the weaponry control system are expanded.
3 cl, 7 dwg
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Authors
Dates
2021-10-11—Published
2020-09-15—Filed