EA021656B1 - Remotely controlled portable launcher for portable anti-tank missile system - Google Patents

Abstract

The invention relates to weapons and can be used in anti-tank missile systems. In addition to armaments, the proposed device can be used in automatic video recording systems and other systems requiring mobile exercise of azimuth and position angle coordinates. The invention proposes a remotely controlled portable launcher for a portable anti-tank missile system, which includes a support bed with a tripod, an equipment container fixed on the bed, a movable turning platform connected to the equipment contained by means of a swivel joint. A new feature is that the equipment container of the launcher includes an electronic control system containing a processor PCB, a control PCB of power follow-up drives in horizontal and vertical planes, a video capture PCB, an interface converter, a start signal shaper; the processor PCB is connected via a cable with an external network interface to a remote control panel, and with an internal bus interface to the control PCB of power follow-up drives in horizontal and vertical planes, the interface converter, the video capture PCB and the start signal shaper; the control PCB of power follow-up drives has two output channels; the control PCB of power follow-up drives is electrically connected via one channel to a power follow-up drive in a horizontal plane, and via another channel it is connected to the power follow-up drive in a vertical plane; the interface converter is connected via an internal bus interface to the control PCB of power follow-up drives and electrically connected via a separate interface to a television laser guidance instrument installed on the movable turning platform of the launcher; the video capture PCB is electrically connected to a television channel of the television laser guidance instrument; the start signal shaper is electrically connected to a mechanism for missile launching from a transporter-launcher container installed on the movable turning platform of the launcher. Technical result of the invention consists in operational remote control of the portable launcher of the portable anti-tank missile system at searching, detection and recognition of a target, measurement of distance to the target, target pointing by means of a television laser guidance instrument, at provision of missile start from the transporter-launcher container, at guidance of the missile at the target using the television laser guidance instrument. Remote control of the portable launcher at safe distance provides for safety to a gunner at execution of a combat operation by a portable anti-tank missile system.

Description

The invention relates to the field of weapons and can be used in anti-tank missile systems. In addition to military equipment, the proposed device can be used in installations for automatic video filming and other complexes that require mobile mining of coordinates in azimuth and elevation. A remote-controlled portable launcher for a portable anti-tank missile system containing a support machine with a tripod, an instrumental container mounted on the machine, a movable turntable connected to an instrumental container of a rotatable joint has been proposed. New is the fact that an electronic control system is introduced into the equipment container of the launcher. It contains a processor board, a control board for power tracking drives horizontally and vertically, a video capture board, an interface converter, a starting signal driver, and a processor board connected by cable to an external network interface with a remote control control, and the internal bus interface is connected to the control board of power tracking drives horizontally and vertically, with a converter interfaces, a video capture card and a starter driver, the power tracking drive control board has two output channels, the power tracking drive control board is electrically connected to the power tracking drive horizontally through one channel, and the interface converter along the power tracking drive is connected to the other the internal bus interface is connected to the control board of power tracking drives and electrically connected to a television-laser device via a separate interface the boring device mounted on the movable rotary platform of the launcher, the video capture card is electrically connected to the television channel of the television and laser guidance device, the driver of the starting signal is electrically connected to the rocket launch mechanism from the transport-launch container mounted on the movable rotary platform of the launcher. The technical result of the invention is the implementation of operational remote control portable launcher portable anti-tank missile complex when searching for, detecting and recognizing targets, measuring the distance to the target, aiming at the target using a television-laser guidance device, while ensuring the launch of the rocket from the transport and launch container, pointing missiles at a target using a television-laser pointing device. Remote control of a portable launcher from a safe distance ensures the safety of the gunner operator when carrying out combat work with a portable anti-tank missile system.

The invention relates to the field of weapons and can be used in anti-tank missile systems. In addition to military equipment, the proposed device can be used in installations for automatic video filming and other complexes that require mobile mining of coordinates in azimuth and elevation.

A portable anti-tank missile system containing a tripod, a rotating swivel, vertical and horizontal guidance mechanisms, a sight-guidance device, a rocket in a container electrically connected to the launch mechanism [1], chosen for the prototype, as the closest to all essential features, is known.

A disadvantage of the known portable anti-tank missile system is that the control of the launcher by the operator-gunner is carried out using controls located directly on the launcher, the level of automation of the control is not high. When launching a rocket from a container, the operator-gunner is affected by the acoustic and shock impact of the gas jet of the jet propulsion system of the launching rocket. An emergency launch of a missile can lead to the death of the operator-gunner.

The objective of the proposed technical solution is to provide operational and safe remote control of a portable launcher during the launch of a missile with a portable anti-tank missile system.

The task is achieved by the fact that a remotely controlled portable launcher for a portable anti-tank missile complex containing a tripod support machine, an equipment container mounted on the machine, a movable turntable connected to an instrument container of a rotary joint, an electronic system is inserted into the instrument container of the launcher control board containing a processor board, a control board for power tracking drives horizontally and vertically, a video board Akhvata, interface converter, starter driver, processor board is connected via a cable by an external network interface to a remote control, and an internal bus interface is connected to a control card of power tracking drives horizontally and vertically, an interface converter, a video capture card and a starter driver, a control card power servo drives has two output channels, one channel for controlling power servo drives electrically horizontally driven, and alternatively connected vertically to the drive, the interface converter is connected via an internal bus interface to the control board of power tracking drives and electrically connected to a television-laser guidance device mounted on a movable rotary platform of the launcher, via a separate interface the video capture is electrically connected to the television channel of the television-laser pointing device, the driver of the starting signal is electrically connected to the mechanical izm rocket launch from a transport and launch container mounted on the platform of a movable rotary platform launcher. The safety of using the launcher is achieved by the territorial location of the operator-gunner with a remote control at a distance from the launcher, which guarantees its safety during the launch of the rocket, as well as in emergency situations.

The proposed technical solution is illustrated graphic material.

FIG. 1 shows a block diagram of an electronic control system of the proposed device.

The electronic system contains a processor board 1, a control board for power tracking drives horizontally and vertically 2, an interface converter 3, a video capture board 4, a starting signal driver 5.

A remotely controlled portable launcher for a portable anti-tank missile system operates as follows.

The processor board 1 is connected via an external network interface with the remote control, and via the internal bus interface it is connected horizontally and vertically 2 with the control board for power tracking drives, interface converter 3, video capture card 4, driver of the start signal 5.

The drive control board 2 is connected via an internal bus interface to the interface converter 3. One output of the drive control board 2 is connected to the power tracking drive horizontally, the second output is connected to the power tracking drive in the vertical direction. The interface converter 3 is connected via a separate interface with a television-laser pointing device attached to a movable rotary platform of the portable launcher.

Video capture card 4 is electrically connected to a television channel of a television-laser pointing device.

The shaper of the starting signal 5 is electrically connected to the mechanism of launching the rocket from the transport and launch container, placed on a movable turntable of the portable launcher.

Launcher works as follows.

- 1 021656

From the television channel of the pointing device to the video capture card 4, a standard television signal comes in analog form. The video capture card 4 converts the analog television signal to a digital form and, via the internal bus interface, transmits the converted video signal to the processor board 1, which transmits the incoming video signal via the external network interface to the remote control. Upon a command from the remote control that comes in via the external network interface to the processor board 1 and is transmitted further via the internal bus interface via the interface converter 3 to the television-laser guidance device, one of the three video image scales can be installed in it - a wide field of view, a narrow field view, a narrow field of view with double magnification.

The video image displayed on the remote control in a wide field of view is used to detect, recognize and select targets for firing with a portable anti-tank missile system.

Measuring the distance to the target selected for the shelling. The command to measure the distance via the external network interface from the remote control goes to the processor board 1 and then via the internal bus interface via the interface converter 3 goes to the laser range finder of a television-laser guidance device. The results of the measurement of the distance to the target from the television-laser pointing device come to the interface converter 3 and further to the processor board 1 via a separate interface, and then transmitted to the remote control via the external network interface.

When deciding to launch a rocket by a command from a remote control coming through the external network interface to the processor board 1 and further via the internal bus interface to the interface converter 3, and from it via a separate interface to the television laser guidance device, the scale of the video image is set on it narrow field of view or a narrow field with double magnification.

A video image in a narrow field of view (a narrow field of view with double magnification) displayed on the remote control is used to aim at the target selected for the shelling. The commands for targeting the launcher to the selected target from the remote control via the external network interface are sent to the processor board 1 and then via the internal bus interface via the interface converter 3 to the control board of the power tracking drives horizontally and vertically 2.

The control board of the power tracking drives 2 generates control signals corresponding to the control commands received from the remote control and transmits them to the tracking power drives horizontally and vertically. The power tracking drives horizontally and vertically work out 2 control signals received from the control board. The data on the current spatial position of the power servo drives horizontally and vertically come from the drives to the control board 2, from it via the internal bus interface to the interface converter 3 and further to the processor board 1, and then to the remote control via the external network interface. The process of testing control commands by power tracking drives is controlled by means of the display on the remote control.

The launch of the rocket is initiated by the START command from the remote control received via the external network interface to the processor board 1, and then via the internal bus interface to the driver of the starting signal 5. Upon receipt of the command START, the driver of the starting signal 5 generates an analogue IGNITURING control signal and delivers it to the mechanism launch rocket from the transport and launch container. After the delay time the rocket starts from the transport and launch container. Upon the release of the rocket from the container, an analogue command EXPOSURE is generated, which from the transport and launch container enters the starting signal shaper 5 and digitized, then via the internal bus interface via the processor board 1 to the interface converter 3, then through a separate interface to the laser-laser control channel control device, initiating the formation of a laser field control rocket in flight.

During the flight of the missile to the target, the position of the aiming point relative to the target is controlled by means of indications on the remote control. If necessary, control commands are sent from the remote control via the external network interface to the processor board 1, which corrects the current position of the power tracking drives horizontally and vertically. Corrective commands via the internal bus interface are transmitted through the interface converter 3 to the control board for power tracking drives 2. On the control card for power tracking drives 2, corrective control signals are generated that correspond to incoming control commands that are fed to the power tracking drives horizontally and vertically. The process of working out corrective commands by power tracking drives is controlled by means of the display on the remote control.

A typical PC / 1O4-P1 and 8 PCM-3362 format processor board can be used as a processor board 1, and a typical electronic board can be used as a video capture board 4

- 2 021656 module AUS-2000, as an interface converter 3 a typical ί'Λί (SoygoIegea ΝοΙ \\ όγ1 <) converter PCM-36801 can be used, and the standard interface ÑHN ν can be used as an internal local network. 2.0А, featuring high noise immunity due to the use of differential transceivers, as an external local network, a network interface can be used. (proportionally integrating). The shaper of the starting signal is a controlled charge-carrying capacitive drive with an output unit of electronic keys.

The kind of portable launcher is illustrated in FIG. 2, 3. In FIG. 2 shows a general view of a portable launcher in an expanded state. FIG. 3 shows a portable launcher in the folded state, prepared for ramming and carrying.

Signs characterizing the device, allow to increase the effectiveness of the portable anti-tank missile system by entering into its composition a remotely controlled portable launcher.

In comparison with the prototype, the proposed technical solution provides operational and safe remote control of a portable launcher of a portable anti-tank missile complex during a missile launch, thereby achieving a higher efficiency of the portable anti-tank missile complex during its combat operation.

A source of information

1. Portable anti-tank missile system. Patent for invention KI 2125699 P41P 1/00, 3/00 dated 1/27/1999 (prototype).

Claims (2)

CLAIM A remotely controlled portable launcher for a portable anti-tank missile complex containing a supporting machine with a tripod, an instrumental container mounted on the machine, a movable turntable connected to an instrumental container of a rotatable joint, characterized in that the instrumental container of the launcher contains an electronic control system including a processor PC / 104-P1i8 format board, power and servo drives control board horizontally and vertically, representing Digital RGO controller, video capture card, CA. No. Interface Converter, Starting Driver, Processor Board are connected to the cable via an external network interface of the EShetpe type! with a remote control, and the internal tire CAN ν. The 2.0A interface is connected horizontally and vertically to the control board for power tracking drives, the interface converter, the video capture card and the starting signal driver, the control board for power tracking drives has two output channels, electrically connected to the power tracking drive via a single channel horizontally, and differently connected to the power servo drive vertically, the interface converter is connected to the boards via the internal bus interface control of power tracking drives and a separate interface is electrically connected to a television-laser guidance device installed on a movable rotary platform of the launcher, the video capture card is electrically connected to the television channel of a television-laser guidance device, the starter driver is electrically connected to the rocket launch mechanism from the transport - launch canister installed on the platform of the movable launch platform of the launcher.