RU2792141C1 - Reconnaissance and scouting relay complex - Google Patents

Abstract

FIELD: surveillance.

SUBSTANCE: invention is intended for remote reconnaissance of hard-to-reach and dangerous terrain. System comprises a weapon 1, a first projectile 2 with containers 3 and 14 equipped with sensors 4, configured to eject said containers on the trajectory. The sensor is equipped with a meter 10 and an energy source 12 with the outputs connected to the input of the meter and the emitter 11 of the sensor. The input of the energy source is connected to the output of the activator 13, the outputs of the computing apparatus 15 are connected to the inputs of containers 3 and 14. The system also comprises a first receiver 5 located in the firing area, a second projectile 6 equipped with a second receiver 7, a transmitter 8, and an inertial current source 9 configured to relay a signal on the flight trajectory from the sensor to the first receiver, a space vehicle 16, and an analyser 17. The input of the space vehicle is connected to the output of the first receiver, and the output of the space vehicle is connected to the input of the analyser. The sensor, the second receiver, and the transmitter are configured to operate during the flight of the second projectile.

EFFECT: improved characteristics of the reconnaissance and scouting relay complex.

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Description

The invention relates to equipment designed for remote reconnaissance of hard-to-reach and dangerous terrain.

Known search and signal system containing a gun, the first projectile with search, reconnaissance and signaling sensors, made with the possibility of their ejection on the trajectory, and the first receiver placed in the area of the shot, the second projectile, equipped with a second receiver and transmitter, made with the ability to relay on flight path signal from the sensors to the first receiver (RF patent for utility model No. 89896 according to application No. 2009102002/22).

This system makes it possible to obtain information about the parameters of objects in hard-to-reach and dangerous terrain from the gun placement zone, but does not have sufficient technical characteristics.

Also known is a search and signal system containing a tool, the first projectile with a sensor, made with the possibility of ejection on the trajectory, the sensor is equipped with a meter and an energy source, the outputs of which are connected to the input of the meter and the emitter of the sensor, the input of the energy source is connected to the output of the activator, the first receiver, placed in the firing zone, the second projectile, equipped with a second receiver, a transmitter and an inertial current source, configured to relay the signal from the sensor to the first receiver on the flight path, the sensor contains an activator configured to be triggered from the transmitter signal, and the output of the activator is connected to the input The emitter, sensor, receiver and transmitter are configured to be actuated by inertial current sources (RF patent No. 2413251 according to application No. 2010103156/28 - prototype).

This solution improves the reliability and survivability of the search and signal system in hard-to-reach and dangerous areas. However, this system does not allow generalizing and using data for additional reconnaissance of objects through sensor control.

The purpose of the invention is to improve the technical characteristics of the reconnaissance and search complex.

The technical result is achieved by the fact that the reconnaissance and search relay complex contains a weapon, the first projectile with sensors, made with the possibility of their ejection on the trajectory, the sensor is equipped with a meter and an energy source, the outputs of which are connected to the input of the meter and the sensor emitter, the input of the energy source is connected to the output activator, the first receiver placed in the shot zone, the second projectile equipped with the second receiver, transmitter and inertial current source, configured to relay the signal from the sensor to the first receiver on the flight path, the sensor, the second receiver and transmitter are configured to operate during the flight of the second projectile, the first projectile contains a calculating device for ejecting sensors in trajectory sections, the complex additionally contains a spacecraft and an analyzer, the apparatus input is connected to the output of the first receiver, the apparatus output is connected to the analyzer input.

The invention is illustrated in Fig.1-2, where it is indicated: 1 - tool; 2 - the first projectile; 3 - the first container; 4 - sensor; 5 - the first receiver; 6 - the second projectile; 7 - second receiver; 8 - transmitter; 9 - inertial current source; 10 - meter; 11 - emitter; 12 - energy source; 13 - activator; 14 - second container; 15 - counting device; 16 - spacecraft; 17 - analyzer.

The operation of the complex is as follows. In the initial position, containers 3 and 14 with sensors 4 are mounted on the first projectile 2, which is configured to eject the sensors on the flight path.

The sensor is equipped with a meter 10, an emitter 11, an energy source 12 and an activator 13 for switching on and off the energy source of the meter and the emitter. The outputs of the calculating device are connected to the inputs of the containers 3 and 14. The outputs of the meter and the energy source are connected to the input of the emitter, configured to transmit a signal to the second receiver. The activator is configured to be triggered by a transmitter signal.

The second projectile 6 is equipped with a second receiver 7, a transmitter 8 and an inertial current source 9 for relaying the signal from the sensors to the first receiver on the flight path. The sensors, the second receiver and the transmitter are configured to operate from a current source during the flight of the second projectile.

The complex additionally contains a spacecraft 16 and an analyzer 17, the input of the apparatus is connected to the output of the first receiver, the output of the apparatus is connected to the input of the analyzer.

Gun 1, receiver 5 and analyzer 17 are installed outside the hard-to-reach and dangerous terrain.

For remote reconnaissance in a remote area, the first projectile 2 is fired from the gun 1, when the projectile is flying along the trajectory, the calculating device 15 is launched, at the signal of which containers 3 and 14 with sensors 4 are sequentially ejected on sections of the projectile flight trajectory onto hard-to-reach and dangerous terrain, where the energy sources of the sensors are in standby mode.

After that, a second projectile 6 is fired, during the flight of which the inertial current source operates, the transmitter activates the activator, energy sources and sensor emitters for the duration of the inertial current source, and the signal from the sensor emitters through the second receiver 7 and transmitter 8 is relayed to the first receiver from which the signal is transmitted to the spacecraft and analyzer.

EFFECT: invention allows searching and reconnaissance of objects in various parts of the projectile flight path, transmitting reconnaissance results via a spacecraft to an analyzer for summarizing information from various sources. It has high stealth and low vulnerability due to the high speed of the projectile. Allows you to improve the technical characteristics of the reconnaissance and search relay complex.

Claims (1)

Reconnaissance and search relay complex containing a weapon, the first projectile with sensors placed in two containers, made with the possibility of their ejection on the trajectory, each sensor is equipped with a meter, an emitter and an energy source, the outputs of which are connected to the input of the meter and the emitter of the sensor, and the output of the meter is also connected to the input of the emitter, and the input of the energy source is connected to the output of the activator, the first receiver located in the firing zone, the second projectile, equipped with a second receiver, transmitter and inertial current source, configured to relay the signal from the sensors on the flight path to the first receiver, moreover, the sensors, the second receiver and the transmitter are configured to operate during the flight of the second projectile, while the first projectile additionally contains a calculating device for ejecting sensors in sections of the trajectory, the outputs of which are connected to the inputs of containers with sensors, and the complex is equipped with spacecraft and analyzer, the input of the spacecraft is connected to the output of the first receiver, and the output of the spacecraft is connected to the input of the analyzer.

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