METHOD OF CORRECTION OF SHOOTING FROM ARTILLERY-TYPE WEAPON Russian patent published in 2018 - IPC F41G3/00 F41G7/00 

Abstract RU 2669690 C1

FIELD: weapons and ammunition.

SUBSTANCE: invention relates to methods and means of artillery reconnaissance based on obtaining and analyzing photo images of the terrain with objects from the aiming area. Method for correcting firing from artillery guns is based on the preliminary determination of the parameters of firing with combat shells. According to these parameters, the gun is aimed and a cluster reconnaissance missile with ballistic characteristics identical to the service projectile is fired. With the help of a knockout device installed in the head of the projectile, clusters are thrown out of the shell of the projectile. Image of the terrain in the impact zone is photographed by one of the clusters. Image is transferred to the shooting unit. Based on the analysis of images, correction of the shooting is performed. Body of the reconnaissance shell is covered with a radio-absorbing coating. Clusters of the reconnaissance missile are made in the form of transceiver modules with in-flight stabilization devices. Modules are placed in the body of the projectile in series so that their stabilization devices are located on the side of the knockout device. First module (1) is left in the body of the shell after the knockout device is activated. Video information is formed about the position of the module (1) in the space before it falls onto the terrain. Second module (2) with the photodetector is oriented with the photodetector part in the module (1) falling direction. Series of consecutive digital photo images of the terrain is obtained. Marking is formed in the center of each image. Height of the module above the terrain is continuously measured. This information is transmitted to the third module (3). Third module is caused to fall at a rate of less than the speed of falling of the second module. It illuminates the terrain in the zone of falling of modules (1) and (2). Information is received from the second module and transmitted to the remote receiver. Information from the remote receiver is analyzed. On each frame of the terrain image, the height of the second module above the terrain, the position of the marking in the center of the frame, and the display of the marking corresponding to the position of the first module, are determined. According to information from several images, these markings are graphically tied to the terrain. Shooting direction is a line between these markings on different images. Point of detonation of a service projectile, when firing conventional ammunition, is the point of the position of the first module on the last frame of the terrain image. Distance from the marking in the center of the frame to the aiming point and other objects is determined by calculation.

EFFECT: it is possible to obtain photo information from a reconnaissance projectile, with the possibility of tying the graphic data obtained in this way to objects on the ground, and determine the direction of shooting and the point of detonation.

1 cl, 3 dwg

Similar patents RU2669690C1

Title Year Author Number
METHOD OF ARTILLERY SHELL CORRECTION 2017
  • Kuznetsov Nikolaj Sergeevich
RU2667167C1
FIRING METHOD OF GUIDED MISSILE WITH LASER HALF-ACTIVE HOMING HEAD AND DEVICE REALIZING THEREOF 2019
  • Umerenkov Sergej Aleksandrovich
  • Shadrin Sergej Vladimirovich
  • Levitskij Mikhail Vitalevich
  • Mukhametshin Alfat Talgatovich
  • Lavrentev Aleksandr Petrovich
  • Khokhlov Vladimir Aleksandrovich
  • Akatev Sergej Anatolevich
RU2737634C2
METHOD OF HIGH-SPEED AERIAL RECONNAISSANCE 2009
  • Abramkin Semen Grigor'Evich
  • Abramkin Maksim Semenovich
RU2395782C1
FIRING METHOD WITH GUIDED MISSILES WITH LASER SEMI-ACTIVE SELF-GUIDANCE HEAD 2019
  • Khokhlov Nikolaj Ivanovich
  • Podchufarov Yurij Borisovich
  • Shigin Aleksandr Viktorovich
  • Larin Dmitrij Viktorovich
  • Larin Andrej Viktorovich
  • Moiseev Anton Stanislavovich
RU2716462C1
METHOD OF TARGET TRACKING USING SPECIAL MISSILE 2019
  • Kozlov Vyacheslav Vladimirovich
  • Chuprin Andrej Igorevich
  • Zontova Tatyana Vladimirovna
  • Evtushenko Evgenij Valerevich
RU2715466C1
METHOD FOR AERIAL SURVEILLANCE OF GROUND (SURFACE) OBJECTS FOR THE PURPOSE OF SURVEYING, METEOROLOGICAL AND OTHER TYPES OF SUPPORT OF LAUNCHES (RELEASES) OF CONTROLLED AIR WEAPONS USING OPTOELECTRONIC HOMING HEADS 2020
  • Moor Aleksej Nikolaevich
  • Egorov Pavel Sergeevich
  • Balanyan Sergej Tovmasovich
  • Al Saftli Fadi Khajdar
RU2771965C1
WEAPON AIMING SYSTEM 2021
  • Malov Yurij Ivanovich
RU2784528C1
METHOD OF INDICATING TRAJECTORY OF MISSILE FLIGHT 2019
  • Kuznetsov Nikolaj Sergeevich
RU2698884C1
METHOD OF FIRE WITH LASER SEMIACTIVE HOMING SHELL ON MOBILE TARGET (VERSIONS) 2007
  • Babichev Viktor Il'Ich
  • Rabinovich Vladimir Isaakovich
  • Larin Andrej Viktorovich
  • Larin Dmitrij Viktorovich
  • Shamin Mikhail Stepanovich
RU2347999C2
METHOD FOR ARTILLERY FIRE 2021
  • Solovev Vladimir Aleksandrovich
  • Yaroshchuk Stepan Stepanovich
  • Taras Roman Borisovich
  • Pafikov Evgenij Anatolevich
RU2772681C1

RU 2 669 690 C1

Authors

Kuznetsov Nikolaj Sergeevich

Dates

2018-10-12Published

2017-08-29Filed