RU2017117740A - A method of firing a guided artillery shell - Google Patents

A method of firing a guided artillery shell Download PDF

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Publication number
RU2017117740A
RU2017117740A RU2017117740A RU2017117740A RU2017117740A RU 2017117740 A RU2017117740 A RU 2017117740A RU 2017117740 A RU2017117740 A RU 2017117740A RU 2017117740 A RU2017117740 A RU 2017117740A RU 2017117740 A RU2017117740 A RU 2017117740A
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RU
Russia
Prior art keywords
target
sight
coordinates
projectile
measured
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Application number
RU2017117740A
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Russian (ru)
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RU2674401C2 (en
RU2017117740A3 (en
Inventor
Александр Владимирович Медведев
Александр Васильевич Гринкевич
Борис Сергеевич Касауров
Original Assignee
Публичное акционерное общество "Ростовский оптико-механический завод" (ПАО "РОМЗ")
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Application filed by Публичное акционерное общество "Ростовский оптико-механический завод" (ПАО "РОМЗ") filed Critical Публичное акционерное общество "Ростовский оптико-механический завод" (ПАО "РОМЗ")
Priority to RU2017117740A priority Critical patent/RU2674401C2/en
Publication of RU2017117740A publication Critical patent/RU2017117740A/en
Publication of RU2017117740A3 publication Critical patent/RU2017117740A3/ru
Application granted granted Critical
Publication of RU2674401C2 publication Critical patent/RU2674401C2/en

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G7/00Direction control systems for self-propelled missiles

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Position Fixing By Use Of Radio Waves (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Claims (9)

Способ стрельбы управляемым артиллерийским снарядом, включающий обнаружение цели через прицел с встроенными вычислителем собственных координат и координат цели, Глонасс/GРS модулем, измерителем дальности до цели, измерителем азимута и измерителем угла места цели, отличающийся тем, что передача координат цели от прицела к снаряду осуществляется через проводной или электромагнитный интерфейс связи, а снаряд содержит контроллер вычислителя, встроенный определитель собственных координат с Глонасс/GPS модулем и корректор траектории, управляющий рулевыми или тормозными элементами снаряда по координатам цели, введенным от вычислителя прицела через интерфейс связи, причем контроллер вычислителя снаряда также формирует команду подрыва снаряда по измеренной дальности при отсутствии сигналов от Глонасс/GPS модуля, при этом выполняются следующие соотношения:A method of firing a guided artillery shell, which includes detecting a target through a sight with built-in calculator of its own coordinates and target coordinates, a Glonass / GPS module, a target range meter, an azimuth meter and a target elevation meter, characterized in that the target coordinates are transmitted from the sight to the projectile via a wired or electromagnetic communication interface, and the projectile contains a computer controller, a built-in eigen-coordinate locator with a Glonass / GPS module and a path corrector, yayuschy steering or brake elements of the projectile target coordinates inputted from the calculator sight through the communication interface, wherein the controller also generates calculator projectile projectile firing command from the measured range in the absence of signals from the GLONASS / GPS module, wherein the following relations: Хц0+D⋅sin αX c = X 0 + D⋅sin α Yц=Y0+D⋅cosαY c = Y 0 + D⋅cosα Zц=Z0+D⋅sinβZ c = Z 0 + D⋅sinβ где Хц, Yц, Zц - вычисленные координаты цели в прицеле, передаваемые на снаряд через интерфейс связи;wherein X n, Y n, Z n - calculated target coordinates in the sight transmitted to the projectile via the communication interface; Х0, Y0, Z0 собственные координаты прицела, измеренные определителем координат - Глонасс/GРS модулем;X 0 , Y 0 , Z 0 own coordinates of the sight, measured by the determinant of coordinates - Glonass / GPS module; D - дальность до цели, измеренная встроенным в прицел дальномером;D is the range to the target, measured by the range finder integrated in the sight; α - азимут цели, измеренный встроенным в прицел указателем азимута;α is the target azimuth measured by the azimuth indicator integrated in the sight; β - угол места цели, измеренный встроенным в прицел измерителем, угла места цели.β is the target elevation angle, measured by a built-in sight meter, and the elevation angle of the target.
RU2017117740A 2017-05-22 2017-05-22 Method of firing guided artillery projectile RU2674401C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2017117740A RU2674401C2 (en) 2017-05-22 2017-05-22 Method of firing guided artillery projectile

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Application Number Priority Date Filing Date Title
RU2017117740A RU2674401C2 (en) 2017-05-22 2017-05-22 Method of firing guided artillery projectile

Publications (3)

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RU2017117740A true RU2017117740A (en) 2018-11-22
RU2017117740A3 RU2017117740A3 (en) 2018-11-22
RU2674401C2 RU2674401C2 (en) 2018-12-07

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RU2017117740A RU2674401C2 (en) 2017-05-22 2017-05-22 Method of firing guided artillery projectile

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Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2695592C1 (en) * 2018-12-13 2019-07-24 Акционерное общество "Научно-производственное предприятие "Дельта" Method of correction of hitting trajectory of artillery projectile
CN114608391B (en) * 2022-03-21 2023-09-29 陕西北斗东芯科技有限公司 Cannonball guidance method and system with stealth effect

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2111437C1 (en) * 1995-05-17 1998-05-20 Конструкторское бюро приборостроения Method of gun laying and device for its realization
US7728264B2 (en) * 2005-10-05 2010-06-01 Raytheon Company Precision targeting
RU2527609C1 (en) * 2013-02-13 2014-09-10 Федеральное государственное казённое учреждение "3 Центральный научно-исследовательский институт Министерства обороны Российской Федерации" Guided artillery round
RU2529828C1 (en) * 2013-04-09 2014-09-27 Открытое акционерное общество "Конструкторское бюро приборостроения им. академика А.Г. Шипунова" Firing of guided missile

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Publication number Publication date
RU2674401C2 (en) 2018-12-07
RU2017117740A3 (en) 2018-11-22

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Effective date: 20190523