CN115930675A - Individual rocket tube simulation terminal and individual harness combined with same - Google Patents

Individual rocket tube simulation terminal and individual harness combined with same Download PDF

Info

Publication number
CN115930675A
CN115930675A CN202211460032.0A CN202211460032A CN115930675A CN 115930675 A CN115930675 A CN 115930675A CN 202211460032 A CN202211460032 A CN 202211460032A CN 115930675 A CN115930675 A CN 115930675A
Authority
CN
China
Prior art keywords
laser
individual
striking
simulation terminal
rocket launcher
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.)
Pending
Application number
CN202211460032.0A
Other languages
Chinese (zh)
Inventor
张勤辉
胡宇耕
尤利宁
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.)
Shaanxi Aorun Laser Technology Co ltd
Original Assignee
Shaanxi Aorun Laser Technology Co ltd
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 Shaanxi Aorun Laser Technology Co ltd filed Critical Shaanxi Aorun Laser Technology Co ltd
Priority to CN202211460032.0A priority Critical patent/CN115930675A/en
Publication of CN115930675A publication Critical patent/CN115930675A/en
Pending legal-status Critical Current

Links

Images

Classifications

    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T90/00Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation

Abstract

The invention relates to an individual rocket launcher simulation terminal and an individual harness used in combination with the same, wherein the individual rocket launcher simulation terminal comprises: the device comprises a gun barrel, a laser transmitter integrated on the gun barrel and used for transmitting attack laser to a striking target, a posture measuring module used for collecting posture information of the gun barrel, and an effect simulation device used for simulating exposure signs. The laser comprises pre-striking laser and data striking laser, the pre-striking laser comprises a pre-striking laser number, the pre-striking laser number comprises pre-striking laser emission information, and the pre-striking laser emission information comprises emission time, longitude and latitude elevation coordinates during emission and an emission angle during emission. The invention effectively solves the outstanding problem that the shooting hit rate is in direct proportion to the target distance due to the distance of laser spots.

Description

Individual rocket tube simulation terminal and individual harness combined with same
Technical Field
The invention relates to the field of weapon equipment for exercise training, in particular to an individual rocket tube simulation terminal and an individual harness combined with the same.
Background
Since the 90 s, in consideration of saving cost and improving exercise fidelity, major military countries in the world are developing laser simulation countermeasure systems, which can simulate the operation performance of weapons of both enemy and my parties, embody various operation actions and operation relations, realize point killing, surface killing, soft killing and comprehensive damage to targets, and enable actual combat to be closer to actual combat.
A simulation terminal used in traditional military simulation training only emits one laser beam, and the outstanding problem that the shooting hit rate is in direct proportion to the target distance due to the fact that the laser spot is far and near is solved.
Disclosure of Invention
In order to solve the technical problems, the invention provides an individual rocket launcher simulation terminal and an individual harness used in combination with the same.
In order to achieve the above object, the present application proposes a first technical solution:
an individual rocket launcher simulation terminal for military exercises, the simulation terminal comprising: the device comprises a gun barrel, a laser transmitter integrated on the gun barrel and used for transmitting attack laser to a striking target, a posture measuring module used for collecting posture information of the gun barrel, and an effect simulation device used for simulating exposure symptoms.
In one embodiment of the present invention, the laser includes a pre-percussion laser including a pre-percussion laser number including pre-percussion laser emission information.
In one embodiment of the invention, the pre-strike laser emission information comprises emission time, longitude and latitude elevation coordinates during emission and an emission angle during emission.
In one embodiment of the invention, the laser transmitter comprises a plurality of laser modules for simulating weapon types.
In one embodiment of the invention, the effect simulator comprises a sonotrode and a photoelastic detection trigger device for activating the sonotrode by the sonotrode detection trigger device so as to simulate the exposure sign.
In one embodiment of the invention, the simulation terminal further comprises an indication module, and the indication module is used for displaying the configuration parameters of the rocket launcher.
In one embodiment of the invention, the indication module comprises an indication panel and an indicator light, the configuration parameters of the rocket launcher are marked on the indication panel, and the indicator light is used for displaying the configuration parameters of the rocket launcher.
In an embodiment of the present invention, the analog terminal further includes a short-range infrared module, configured to collect configuration information.
In one embodiment of the invention, the analog terminal further comprises a key and a trigger, wherein the key is used for function selection, and the trigger is used for triggering the laser transmitter.
In order to achieve the above object, the present application further provides a second technical solution:
the individual soldier outfit is in data interaction with the individual rocket launcher simulation terminal.
Compared with the prior art, the technical scheme of the invention has the following advantages:
the single rocket launcher simulation terminal and the single rocket launcher harness used in combination with the same adopt a hitting mode of fusing laser and data and a multi-light-path laser transmitting and receiving processing technology, and effectively solve the outstanding problem that the shooting hit rate is in direct proportion to the target distance due to the distance of laser spots.
According to the individual rocket tube simulation terminal and the individual harness combined with the same, the individual rocket tube simulation terminal can receive control information sent by the individual harness, day and night mode switching is achieved, and the brightness of the state indicator lamp can be automatically reduced in a night mode.
The individual rocket launcher simulation terminal and the individual harness used in combination with the same can receive ammunition setting instructions sent by the individual harness, and realize simulated loading; the information such as weapon firing, ammunition consumption residual capacity and the like can be uploaded to the individual soldier outfit in a wireless mode.
According to the individual rocket tube simulation terminal and the individual harness used in combination with the same, the launching function is automatically locked or unlocked according to the current projectile amount, the launching function is locked when the projectile amount is 0, and the launching function is unlocked when the projectile amount is not 0.
The individual rocket tube simulation terminal and the individual harness combined with the same can simulate exposure symptoms of weapons during shooting through the bidirectional acoustic-optical bombs.
Drawings
In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings needed to be used in the description of the embodiments will be briefly introduced below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art to obtain other drawings based on these drawings without creative efforts.
FIG. 1 is a functional block diagram of the present invention;
fig. 2 is a schematic block diagram of the individual rocket launcher simulating terminal of the invention.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more apparent, the technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 2, an individual rocket launcher simulation terminal includes: the device comprises a gun barrel, a laser transmitter integrated on the gun barrel and used for transmitting attack laser to a striking target, a posture measuring module used for collecting posture information of the gun barrel, and an effect simulation device used for simulating exposure signs. The laser comprises pre-striking laser and data striking laser, the pre-striking laser comprises a pre-striking laser number, the pre-striking laser number comprises pre-striking laser emission information, and the pre-striking laser emission information comprises emission time, longitude and latitude elevation coordinates during emission and an emission angle during emission. The simulation terminal further comprises a key, a trigger and a short-distance infrared module, wherein the key is used for function selection, the trigger is used for triggering the laser transmitter, and the short-distance infrared module is used for collecting configuration information such as ammunition parameter information and the like of a loading collector.
In actual military exercises, in order to facilitate data exchange between the individual rocket launcher simulation terminal and the striking target, a background system is arranged, the individual rocket launcher simulation terminal is further provided with a communication module, and the individual rocket launcher simulation terminal performs data interaction with the background system in a wireless communication (4G and the like) mode.
When the rocket launcher simulation terminal is used, the shooting process of the single rocket launcher simulation terminal is as follows:
aiming the pre-striking target through the aiming system and emitting pre-striking laser.
The pre-strike laser number contains the following information:
a transmission time (T1);
longitude and latitude elevation coordinates (X1, Y1, Z1) during transmission;
the emission angle (α 1, β 1, γ 1) of the emission.
The hit target receives the laser coding information for decoding and uploads hit data to a background system, wherein the hit data mainly comprises the following information:
an attack time (T2);
longitude and latitude elevation coordinates (X2, Y2, Z2) when attacked;
coded information (identity information ID 1) of the attacker;
time when the attack started (T1);
longitude and latitude elevations (X1, Y1, Z1) during transmission;
the emission angle (α 1, β 1, γ 1) of the emission.
The background system processes the data to be hit according to the uploaded data, and mainly processes the following information: relative coordinates between the attacker and the attacked and the shooting angles (T1, delta alpha 1, delta beta 1, delta gamma 1) relative to the coordinate system at the shooting moment are transmitted to the attacker through the 4G network: an attacker receives corrected shooting angle information (T1, delta alpha 1, delta beta 1 and delta gamma 1) issued by a background system, corrects the shooting angle information during first transmission, and calculates the shooting angle information at the current moment; and controlling a laser transmitter to continuously transmit data striking laser, wherein the data striking laser comprises ammunition information, fuze information and the like, uploading the information of the attack event to a background system, and simultaneously triggering an effect simulation device to expose the symptom. And the background system calculates whether the final impact point information of the rocket launcher effectively attacks the pre-hit target or related facilities according to the uploaded attack information, and guides the related equipment facilities to be effectively attacked.
The single-soldier rocket launcher can generate exposure symptoms such as sound, light and smoke when being launched, therefore, in order to simulate the exposure symptoms while the single-soldier rocket launcher is launched, the effect simulation device comprises an acoustic-optic bomb and an acoustic-optic bomb detection trigger device, the acoustic-optic bomb is started by the acoustic-optic bomb detection trigger device while the laser launcher is launched, so that the exposure symptoms are simulated, and the exposure symptoms comprise the sound and the light emitted by a flashing bomb.
In order to facilitate the configuration parameter of instructing individual soldier's rocket launcher, simulation terminal still includes indicating module, indicating module includes indicating panel and pilot lamp, the last sign of indicating panel has the configuration parameter of rocket launcher, the pilot lamp is used for showing the configuration parameter of rocket launcher, configuration parameter can be the bullet kind, bullet volume, the location condition that rocket launcher carried and the connection condition etc. with individual soldier's outfit.
In one embodiment, the laser transmitter comprises a plurality of laser modules, different weapon types are simulated through the laser modules, further, the laser transmitter uses different laser modules on far, middle and near lasers, different weapon types are simulated through controlling laser emission power switching, and the weapon types can be shells with different functions and launched by an antitank rocket launcher. Three beams of laser are emitted in a time-sharing manner, the three beams of laser are emitted in a near-middle-far sequence, and the emission time interval is obtained through test; the laser decoding also performs the superimposition judgment in this order. The laser receiver comprises four laser emission drivers: the laser driving system comprises a far laser emission driver, a middle laser emission driver and a near laser emission driver and a calibration laser driver. Preferably, 980nm-1W is used for simulating weapon emission laser, and 520nm-120mW is used for initial laser calibration.
In this embodiment, an individual soldier rocket launcher simulation terminal, individual rocket launcher can be 11 formulas 93mm individual rocket launcher, 66mm individual rocket launcher etc. and the preferred 93mm individual rocket launcher of individual rocket launcher in this embodiment. For the advantages of easy modulation, high reliability, and all weather, the laser transmitter and the laser receiver in this embodiment preferably use the 980nm wavelength band.
The individual soldier outfit is in data interaction with the individual rocket launcher simulation terminal.
The control information sent by the individual soldier harness controls the brightness, the brightness time and other parameters of the indication module, the individual soldier harness sends an ammunition setting instruction to control the indication module to realize simulated loading, and the individual rocket launcher simulation terminal can upload information such as weapon emission, ammunition consumption and residual electric quantity to the individual soldier harness in a wireless communication mode.
In actual military exercises, in order to facilitate data exchange among the individual rocket launcher simulation terminal, the individual harness and the striking target, the individual harness is provided with a communication module, the individual harness performs data interaction with the individual rocket launcher simulation terminal in a wireless communication mode, and the wireless communication mode of the individual harness and the individual rocket launcher simulation terminal is preferably Zigbee communication.
Embodiments of the present invention are described with reference to flowchart illustrations and/or block diagrams of methods, apparatus (systems) and computer program products according to embodiments of the invention. It will be understood that each flow and/or block of the flow diagrams and/or block diagrams, and combinations of flows and/or blocks in the flow diagrams and/or block diagrams, can be implemented by computer program instructions. These computer program instructions may be provided to a processor of a general purpose computer, special purpose computer, embedded processor, or other programmable data processing apparatus to produce a machine, such that the instructions, which execute via the processor of the computer or other programmable data processing apparatus, create means for implementing the functions specified in the flowchart flow or flows and/or block diagram block or blocks.
These computer program instructions may also be stored in a computer-readable memory that can direct a computer or other programmable data processing apparatus to function in a particular manner, such that the instructions stored in the computer-readable memory produce an article of manufacture including instruction means which implement the function specified in the flowchart flow or flows and/or block diagram block or blocks.
These computer program instructions may also be loaded onto a computer or other programmable data processing apparatus to cause a series of operational steps to be performed on the computer or other programmable apparatus to produce a computer implemented process such that the instructions which execute on the computer or other programmable apparatus provide steps for implementing the functions specified in the flowchart flow or flows and/or block diagram block or blocks.
It is to be noted that the foregoing is only illustrative of the preferred embodiments of the present invention and the technical principles employed. It will be understood by those skilled in the art that the present invention is not limited to the particular embodiments described herein, but is capable of various obvious changes, rearrangements and substitutions as will now become apparent to those skilled in the art without departing from the scope of the invention. Therefore, although the present invention has been described in greater detail by the above embodiments, the present invention is not limited to the above embodiments, and may include other equivalent embodiments without departing from the spirit of the present invention, and the scope of the present invention is determined by the scope of the appended claims.

Claims (10)

1. An individual rocket tube simulation terminal for military exercises, the simulation terminal comprising: the device comprises a gun barrel, a laser transmitter integrated on the gun barrel and used for transmitting attack laser to a striking target, a posture measuring module used for collecting posture information of the gun barrel, and an effect simulation device used for simulating exposure signs.
2. The individual rocket launcher simulation terminal according to claim 1, wherein: the laser comprises pre-striking laser, the pre-striking laser comprises pre-striking laser numbers, and the pre-striking laser numbers comprise pre-striking laser emission information.
3. The individual rocket launcher simulation terminal according to claim 2, wherein: the pre-strike laser emission information comprises emission time, longitude and latitude elevation coordinates during emission and an emitting angle during emission.
4. The individual rocket launcher simulation terminal according to claim 1, wherein: the laser transmitter comprises a plurality of laser modules, and the laser modules are used for simulating weapon types.
5. The individual rocket launcher simulation terminal according to claim 1, wherein: the effect simulation device comprises a sound-light bullet and a sound-light bullet detection trigger device and is used for starting the sound-light bullet through the sound-light bullet detection trigger device so as to simulate the exposure symptom.
6. The individual rocket launcher simulation terminal according to claim 1, wherein: the simulation terminal further comprises an indication module, and the indication module is used for displaying the configuration parameters of the rocket tube.
7. The individual rocket launcher simulation terminal according to claim 4, wherein: the indicating module comprises an indicating panel and an indicating lamp, the indicating panel is marked with the configuration parameters of the rocket tube, and the indicating lamp is used for displaying the configuration parameters of the rocket tube.
8. The individual rocket launcher simulation terminal according to claim 1, wherein: the analog terminal also comprises a short-distance infrared module used for collecting configuration information.
9. The individual rocket launcher simulation terminal according to claim 1, wherein: the simulation terminal further comprises a key and a trigger, wherein the key is used for function selection, and the trigger is used for triggering the laser transmitter.
10. An individual soldier harness, characterized in that: the individual harness performs data interaction with the individual rocket launcher simulation terminal of claims 1-9.
CN202211460032.0A 2022-11-17 2022-11-17 Individual rocket tube simulation terminal and individual harness combined with same Pending CN115930675A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202211460032.0A CN115930675A (en) 2022-11-17 2022-11-17 Individual rocket tube simulation terminal and individual harness combined with same

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202211460032.0A CN115930675A (en) 2022-11-17 2022-11-17 Individual rocket tube simulation terminal and individual harness combined with same

Publications (1)

Publication Number Publication Date
CN115930675A true CN115930675A (en) 2023-04-07

Family

ID=86696799

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202211460032.0A Pending CN115930675A (en) 2022-11-17 2022-11-17 Individual rocket tube simulation terminal and individual harness combined with same

Country Status (1)

Country Link
CN (1) CN115930675A (en)

Similar Documents

Publication Publication Date Title
US4682953A (en) Combined arms effectiveness simulation system
KR100833162B1 (en) Apparatus and system for simulating of shooting a grenade launcher
US6386879B1 (en) Precision gunnery simulator system and method
US8312814B2 (en) Simulated hand grenade having a multiple integrated laser engagement system
KR100914274B1 (en) Training simulation system for indirect fire weapon systems
RU2379614C2 (en) Method to control artillery piece fire
US7052276B2 (en) System and method for combat simulation
US5690491A (en) Method and apparatus for simulating the effects of precision-guided munitions
JP3905440B2 (en) Shooting simulation device
CN115930675A (en) Individual rocket tube simulation terminal and individual harness combined with same
CN207635940U (en) A kind of nachinegun fire dot laser simulator
CN109357567A (en) A kind of method that control directly takes aim at weapon effective range in laser countermeasure (s)
JP7197443B2 (en) combat training system
CN115790261A (en) Antitank rocket launcher simulation terminal and base station
CN105135937A (en) Actual combat shooting training system
KR101229872B1 (en) Claymore simulator using LED light and a mock battle system using the claymore simulator
RU2287189C1 (en) System for imitating air combat
CN210268352U (en) Mortar confrontation simulator
CN117558182A (en) Individual portable antitank missile simulation equipment and simulation method thereof
CN105004217A (en) Laser simulation shooting CS (Counter-Strike) counter-training system
CN105066774A (en) Laser simulated shooting confronting training system
CN115798286A (en) Tank simulation terminal
CN105066772A (en) CS practical shooting training system
CN105403100A (en) Laser simulated shooting counter-training system
IL284634B (en) System and method of impact detection in training

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination