RU2015125186A - The method of destruction of small aircraft - Google Patents

The method of destruction of small aircraft Download PDF

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Publication number
RU2015125186A
RU2015125186A RU2015125186A RU2015125186A RU2015125186A RU 2015125186 A RU2015125186 A RU 2015125186A RU 2015125186 A RU2015125186 A RU 2015125186A RU 2015125186 A RU2015125186 A RU 2015125186A RU 2015125186 A RU2015125186 A RU 2015125186A
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RU
Russia
Prior art keywords
mgla
zak
elevation
aircraft
zbp
Prior art date
Application number
RU2015125186A
Other languages
Russian (ru)
Other versions
RU2610734C2 (en
Inventor
Владимир Васильевич Бутузов
Юрий Леонтьевич Козирацкий
Павел Евгеньевич Кулешов
Дмитрий Владимирович Прохоров
Андрей Николаевич Шмаров
Роман Геннадьевич Хильченко
Мирослав Валерьевич Халезов
Александр Александрович Донцов
Татьяна Александровна Ершова
Original Assignee
Акционерное общество "Научно-исследовательский институт "Экран" (АО "НИИ "Экран")
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.)
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Application filed by Акционерное общество "Научно-исследовательский институт "Экран" (АО "НИИ "Экран") filed Critical Акционерное общество "Научно-исследовательский институт "Экран" (АО "НИИ "Экран")
Priority to RU2015125186A priority Critical patent/RU2610734C2/en
Publication of RU2015125186A publication Critical patent/RU2015125186A/en
Application granted granted Critical
Publication of RU2610734C2 publication Critical patent/RU2610734C2/en

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/01—Arrangements thereon for guidance or control
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C13/00—Proximity fuzes; Fuzes for remote detonation
    • F42C13/02—Proximity fuzes; Fuzes for remote detonation operated by intensity of light or similar radiation

Landscapes

  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Optical Radar Systems And Details Thereof (AREA)

Claims (1)

Способ поражения малогабаритного летательного аппарата, заключающийся в поиске, обнаружении и сопровождении зенитно-артиллерийским комплексом (ЗАК) малогабаритного летательного аппарата (МГЛА), наведении ЗАК в направление прицеливания с учетом параметров полета МГЛА и характеристик ЗАК, отличающийся тем, что передают параметры полета МГЛА на неконтактный оптический взрыватель зенитного боеприпаса (ЗБП) ЗАК, подсвечивают МГЛА лазерным излучением, осуществляют ЗАК выстрел ЗБП, измеряют неконтактным оптическим взрывателем ЗБП по принимаемому отраженному лазерному излучению угол места и азимут МГЛА и определяют угломестную составляющую скорости сближения ЗБП и МГЛА, по значениям угломестной составляющей скорости сближения ЗБП и МГЛА, параметров полета МГЛА относительно ЗАК и разрывных характеристик ЗБП вычисляют значение оптимального угла места МГЛА подрыва ЗБП, при достижении по мере сближения ЗБП и МГЛА угла места МГЛА значения угла места подрыва ЗБП осуществляют направленный подрыв ЗБП в направлении текущего азимута МГЛА.The method of hitting a small-sized aircraft, which consists in searching, detecting and tracking an anti-aircraft complex (ZAK) of a small-sized aircraft (MGLA), pointing the ZAK in the direction of aiming taking into account the flight parameters of the MGLA and the characteristics of the ZAK, characterized in that they transmit the flight parameters of the MGLA to non-contact optical fuse of anti-aircraft ammunition (ZBP) ZAK, illuminated with MGLA laser radiation, carry out ZAK shot of an ZBP, measured by a non-contact optical fuse of ZBP according to the reflected laser radiation, the elevation angle and azimuth of the MGLA and determine the elevation component of the approach speed of the ACB and the MGLA, from the values of the elevation component of the approach speed of the airborne defense and the MGLA, the flight parameters of the MGLA relative to the ZAK and the discontinuous characteristics of the airborne defense, calculate the value of the optimal elevation angle of the MGLA to undermine the CBP, as the BZP and MGLA approach the elevation angle of the MGLA, the values of the angle of the elevation of the strike of the BZP carry out a directed blasting of the BZP in the direction of the current azimuth of the MGLA.
RU2015125186A 2015-06-25 2015-06-25 Method of destruction of miniature aerial vehicles RU2610734C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2015125186A RU2610734C2 (en) 2015-06-25 2015-06-25 Method of destruction of miniature aerial vehicles

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2015125186A RU2610734C2 (en) 2015-06-25 2015-06-25 Method of destruction of miniature aerial vehicles

Publications (2)

Publication Number Publication Date
RU2015125186A true RU2015125186A (en) 2017-01-10
RU2610734C2 RU2610734C2 (en) 2017-02-15

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Family Applications (1)

Application Number Title Priority Date Filing Date
RU2015125186A RU2610734C2 (en) 2015-06-25 2015-06-25 Method of destruction of miniature aerial vehicles

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RU (1) RU2610734C2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109827478B (en) * 2019-01-29 2020-01-31 北京理工大学 guidance method with falling angle constraint and overload constraint

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH06147800A (en) * 1992-11-04 1994-05-27 Mitsubishi Electric Corp Proximity fuse
RU2111445C1 (en) * 1996-10-11 1998-05-20 Конструкторское бюро машиностроения Individual-use guided anti-aircraft missile
RU2247927C2 (en) * 2002-07-29 2005-03-10 Козлов Вячеслав Владимирович Combat section of guided missile
US8033221B2 (en) * 2007-08-13 2011-10-11 Raytheon Company System and method for sensing proximity
RU2398183C1 (en) * 2009-07-17 2010-08-27 Василий Васильевич Ефанов Method to control rocket high-explosive warhead killability field characteristics and device to this end

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Publication number Publication date
RU2610734C2 (en) 2017-02-15

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MM4A The patent is invalid due to non-payment of fees

Effective date: 20170626