RU95101418A - Method of reduction of kill probability of flying vehicle by air defence means - Google Patents

Method of reduction of kill probability of flying vehicle by air defence means

Info

Publication number
RU95101418A
RU95101418A RU95101418/02A RU95101418A RU95101418A RU 95101418 A RU95101418 A RU 95101418A RU 95101418/02 A RU95101418/02 A RU 95101418/02A RU 95101418 A RU95101418 A RU 95101418A RU 95101418 A RU95101418 A RU 95101418A
Authority
RU
Russia
Prior art keywords
reduction
flying vehicle
air defence
kill probability
defence means
Prior art date
Application number
RU95101418/02A
Other languages
Russian (ru)
Other versions
RU2095737C1 (en
Inventor
В.Д. Долин
В.А. Ковальчук
В.Н. Мартынов
И.С. Селезнев
Original Assignee
В.Д. Долин
В.А. Ковальчук
В.Н. Мартынов
И.С. Селезнев
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by В.Д. Долин, В.А. Ковальчук, В.Н. Мартынов, И.С. Селезнев filed Critical В.Д. Долин
Priority to RU95101418A priority Critical patent/RU2095737C1/en
Publication of RU95101418A publication Critical patent/RU95101418A/en
Application granted granted Critical
Publication of RU2095737C1 publication Critical patent/RU2095737C1/en

Links

Abstract

FIELD: aviation; aerobatic aeroplanes. SUBSTANCE: manoeuvre is three dimensional combination of turns of spiral in plane perpendicular to direction of flight in form of intersecting eights. Transfer from one eight to another occurs inadvertently. EFFECT: reduction of till probability due to realization of manoeuvre excluding possibility of extrapolation of parameters of its trajectory.

Claims (1)

Изобретение относится к области авиации, а именно к маневренным летательным аппаратам. Цель изобретения - уменьшение вероятности поражения маневрирующего летательного аппарата средствами ПВО за счет реализации маневра, исключающего возможность экстраполяции параметров его траектории. Маневр представляет собой пространственную комбинацию витков спирали и плоскости, перпендикулярной направлению полета, имеет вид взаимно перемещающихся в своих узлах восьмерок. Переход с одной восьмерки на другую осуществляется случайным образом.The invention relates to the field of aviation, namely to maneuverable aircraft. The purpose of the invention is to reduce the likelihood of hitting a maneuvering aircraft by air defense means by implementing a maneuver that excludes the possibility of extrapolating the parameters of its trajectory. A maneuver is a spatial combination of spiral turns and a plane perpendicular to the direction of flight, looks like eights mutually moving at their nodes. The transition from one eight to another is carried out randomly.
RU95101418A 1995-01-25 1995-01-25 Method of decrease of probability of hitting of aircraft by means of antiaircraft defense RU2095737C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU95101418A RU2095737C1 (en) 1995-01-25 1995-01-25 Method of decrease of probability of hitting of aircraft by means of antiaircraft defense

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU95101418A RU2095737C1 (en) 1995-01-25 1995-01-25 Method of decrease of probability of hitting of aircraft by means of antiaircraft defense

Publications (2)

Publication Number Publication Date
RU95101418A true RU95101418A (en) 1996-12-10
RU2095737C1 RU2095737C1 (en) 1997-11-10

Family

ID=20164439

Family Applications (1)

Application Number Title Priority Date Filing Date
RU95101418A RU2095737C1 (en) 1995-01-25 1995-01-25 Method of decrease of probability of hitting of aircraft by means of antiaircraft defense

Country Status (1)

Country Link
RU (1) RU2095737C1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2634659C1 (en) * 2016-06-03 2017-11-02 Евгений Николаевич Захаров Maneuvering method for high-speed unmanned aerial vehicle in possible coverage area of anti-missile and air defense means
RU2635022C1 (en) * 2016-07-08 2017-11-08 Евгений Николаевич Захаров Maneuvering method for high-speed unmanned aerial vehicle in possible coverage area of anti-missile and air defense means
US10096251B2 (en) * 2016-12-16 2018-10-09 Insitu, Inc. Systems and methods for establishing a flight pattern adjacent to a target for a vehicle to follow

Also Published As

Publication number Publication date
RU2095737C1 (en) 1997-11-10

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