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WO2018169446A2 - Canon automoteur - Google Patents

Canon automoteur Download PDF

Info

Publication number
WO2018169446A2
WO2018169446A2 PCT/RU2018/000053 RU2018000053W WO2018169446A2 WO 2018169446 A2 WO2018169446 A2 WO 2018169446A2 RU 2018000053 W RU2018000053 W RU 2018000053W WO 2018169446 A2 WO2018169446 A2 WO 2018169446A2
Authority
WO
WIPO (PCT)
Prior art keywords
self
propelled
output
angle
input
Prior art date
Legal status (The legal status 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 status listed.)
Ceased
Application number
PCT/RU2018/000053
Other languages
English (en)
Russian (ru)
Other versions
WO2018169446A3 (fr
Inventor
Вячеслав Викторович ЛАПИН
Владимир Алексеевич ВОРОНЦОВ
Евгений Сергеевич ЛЯДОВ
Станислав Алексеевич БАСАЛОВ
Вячеслав Петрович КУЗНЕЦОВ
Владимир Михайлович ГОРНОСТАЕВ
Юрий Иванович БЕЛЫЙ
Станислав Владимирович ФЁДОРОВ
Александр Евгеньевич МОНИН
Анатолий Фёдорович ВАСИЛЬЕВ
Юрий Петрович ЛИРИОНОВ
Владимир Сергеевич ШАРОВ
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Joint Stock Co "air And Space Defence Corp "almaz-Antey"
Joint Stock Co "ulyanovsk Mechanical Plant"
Original Assignee
Joint Stock Co "air And Space Defence Corp "almaz-Antey"
Joint Stock Co "ulyanovsk Mechanical Plant"
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 Joint Stock Co "air And Space Defence Corp "almaz-Antey", Joint Stock Co "ulyanovsk Mechanical Plant" filed Critical Joint Stock Co "air And Space Defence Corp "almaz-Antey"
Publication of WO2018169446A2 publication Critical patent/WO2018169446A2/fr
Publication of WO2018169446A3 publication Critical patent/WO2018169446A3/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G3/00—Aiming or laying means
    • F41G3/04—Aiming or laying means for dispersing fire from a battery ; for controlling spread of shots; for coordinating fire from spaced weapons

Definitions

  • the utility model relates to the field of military equipment and can be used as part of medium-range anti-aircraft missile systems (SAM) as the main combat weapon.
  • SAM medium-range anti-aircraft missile systems
  • Known self-propelled firing system (patent jNbl43315), containing a self-propelled chassis, a launcher with mounted missiles with semi-active radar homing heads, a radar station, a digital computer system, a gyroscopic system for measuring heading angles, roll, pitch, the input of which is connected to the output of the navigation system, and the output is connected to a digital computing system, the interface device, the input of which is connected to the output of the optoelectronic system, and the output is connected to the input intellectual th system.
  • the applied gyroscopic system uses a manual input mode of input data. The complexity of the known device and manual operations for entering data into the gyroscopic system reduce the reliability of the SDA.
  • SUP self-propelled gun mount
  • the heel and pitch angles are transmitted to the DAC. Errors in measuring coordinates that arise due to the fact that the tracked vehicle is not on an ideally horizontal base are determined and eliminated in the DAC.
  • the heading angle is also transmitted to the CVC, which must be taken into account for interaction in a single coordinate system with the radar stations of the complex, the command post and other air defense systems.
  • the disadvantage of the SDA 9A317 is that the IKV-1 course vertical line used in the gyroscopic system produces angles in the form of sine-cosine voltages, which must be converted to a digital serial code for transmission to the SDS CVS.
  • the use of additional phase-to-code converters complicates the equipment and reduces reliability.
  • Known closest in technical essence to the claimed self-propelled firing system [patent N ° 91 155], containing a tracked vehicle, a launching device on which anti-aircraft guided missiles, an electro-hydraulic tracking drive, a radar station, a digital computer system, an information system of vertical and course Ts -061K.
  • the Ts-061K information system is intended for installation on aircraft that can perform complex spatial maneuvers, for example, the Nesterov loop.
  • the information complex is equipped with an external roll frame, which complicates its design and reliability. This in turn reduces the reliability of the JMA as a whole.
  • the proposed utility model solves the problem of improving the reliability of the JMA.
  • a self-propelled gun mount containing self-propelled chassis, a launcher that houses anti-aircraft guided missiles, an electro-hydraulic tracking drive, a radar station, a digital computer system, an angle meter with a fiber optic gyroscope and a pairing device are introduced, with the output the angle meter is connected to the input of the interface device, and the input-output of the interface device is connected to the input-output of the DAC.
  • the angle meter is designed to form a heading angle, pitch angle, roll angle in a digital code that is fed to the IUG output.
  • Heading angle - the angle between the projection of the longitudinal axis of the SOU chassis on the horizon plane and the direction to the North.
  • Pitch angle - the angle in the vertical plane between the longitudinal axis of the SOU chassis and its projection onto the horizon plane.
  • the angle of heel is the angle in the plane perpendicular to the longitudinal axis of the chassis of the JMA between the transverse axis of the chassis of the JMA and its projection onto the horizon plane.
  • IUG you can apply, for example, the IBZ-100.12-01 meter, which is produced commercially. This meter uses fiber-optic gyroscopes, the principle of which is based on measuring the phase difference of two counterpropagating waves propagating in an annular fiber interferometer, which occurs when it is rotated due to the Sagnac effect.
  • the interface device is designed to transmit measurement information to the DAC at its request according to the exchange protocol.
  • the interface device can be implemented using the DAC program.
  • Self-propelled chassis with respect to the horizontal plane of which the heights of the heel and pitch are measured, is designed to transport the JMA to the guarded object, all the JMA systems and devices are placed on the chassis.
  • a self-propelled chassis you can use the GM 969B-01 tracked vehicle or the MZKT-69221 wheeled chassis, which are mass-produced.
  • missiles are sent towards the target being followed.
  • SAM commercially available 9MZ 17 anti-aircraft guided missiles.
  • the SDA radar is activated, which surveys the space in its sector of responsibility, and then accompanies those detected and identified as dangerous air targets.
  • the tracking data that is, the azimuth, elevation angle, speed, range of several targets at the same time, is sent to the DAC, where, taking into account the angle of heel and pitch entered from the angle meter in the DAC, the tasks of pointing the launching device to the anticipated point, the missile meeting tasks with the target are solved, signals are generated pointing missiles at the target in angles and radial velocity.
  • the heading angle measured and entered into the CVS determines the orientation of the JMA in the area relative to the cardinal points, which allows you to distribute the detected dangerous targets between other firing systems for air defense systems for firing.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Gyroscopes (AREA)
  • Navigation (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

Le canon automoteur se rapporte aux équipements militaires et peut s'utiliser dans des systèmes de missiles anti-aériens de moyenne portée utilisé en tant que arme principale. L'invention porte sur un modèle d'utilité qui permet d'obtenir une meilleure fiabilité du canon automoteur. Le canon automoteur comprend un châssis autoporteur, une rampe de lancement sur laquelle sont disposés des missiles guidés anti-aériens, un entraînement de suivi électro-hydraulique, une station radar, un système informatique numérique (SIN), un dispositif de mesure d'angles doté d'un gyroscope à fibre optique et un dispositif d'interface, la sortie du dispositif de mesure d'angles étant reliée à l'entrée du dispositif d'interface, et l'entrée / sortie du dispositif d'interface est reliée à l'entrée / sortie du SIN.
PCT/RU2018/000053 2016-12-27 2018-01-31 Canon automoteur Ceased WO2018169446A2 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
RU2016151902 2016-12-27
RU2016151902 2016-12-27

Publications (2)

Publication Number Publication Date
WO2018169446A2 true WO2018169446A2 (fr) 2018-09-20
WO2018169446A3 WO2018169446A3 (fr) 2018-11-29

Family

ID=63523717

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/RU2018/000053 Ceased WO2018169446A2 (fr) 2016-12-27 2018-01-31 Canon automoteur

Country Status (1)

Country Link
WO (1) WO2018169446A2 (fr)

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5347910A (en) * 1985-10-15 1994-09-20 The Boeing Company Target acquisition system
US6422508B1 (en) * 2000-04-05 2002-07-23 Galileo Group, Inc. System for robotic control of imaging data having a steerable gimbal mounted spectral sensor and methods
RU91155U1 (ru) * 2009-10-07 2010-01-27 Открытое акционерное общество "Ульяновский механический завод" (ОАО "УМЗ") Самоходная огневая установка
RU143315U1 (ru) * 2014-02-25 2014-07-20 Открытое акционерное общество "Научно-исследовательский институт приборостроения имени В.В. Тихомирова" Самоходная огневая установка обнаружения, сопровождения и подсвета целей, наведения и пуска ракет зенитного ракетного комплекса средней дальности

Also Published As

Publication number Publication date
WO2018169446A3 (fr) 2018-11-29

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