FIELD: aviation; weapons.
SUBSTANCE: invention relates to ballistic support of aircraft bombs and can be used in development of new and modernization of existing aircraft target systems of aircraft. To account for wind when using aviation bombs, wind velocity is measured at discharge height, average wind velocity is calculated and impact parameters of application are determined with its use. In addition, the type of bomb is determined, and if an aerial bomb with a braking device is used, an individual wind function is calculated, on the basis of which the aiming parameters of the bombing are specified taking into account the individual characteristics of the used aerial bomb with the braking device.
EFFECT: higher accuracy of using an aircraft bomb with a braking device by determining an individual wind function and specifying on its basis the impact parameters of use - the position of the aiming mark.
1 cl, 1 dwg
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