CN210466264U - Helicopter actual combat system data processing unit - Google Patents

Helicopter actual combat system data processing unit Download PDF

Info

Publication number
CN210466264U
CN210466264U CN201921921905.7U CN201921921905U CN210466264U CN 210466264 U CN210466264 U CN 210466264U CN 201921921905 U CN201921921905 U CN 201921921905U CN 210466264 U CN210466264 U CN 210466264U
Authority
CN
China
Prior art keywords
module
processing unit
data processing
helicopter
power supply
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.)
Active
Application number
CN201921921905.7U
Other languages
Chinese (zh)
Inventor
穆俊光
王震
刘小猛
王耀祥
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.)
Beijing Andawell Aviation Equipment Co Ltd
Original Assignee
Beijing Andawell Aviation Equipment 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 Beijing Andawell Aviation Equipment Co Ltd filed Critical Beijing Andawell Aviation Equipment Co Ltd
Priority to CN201921921905.7U priority Critical patent/CN210466264U/en
Application granted granted Critical
Publication of CN210466264U publication Critical patent/CN210466264U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

A helicopter actual combat system data processing unit is characterized in that a main processor module, an interface module and a power supply module are connected with a motherboard; the interface module is connected with the power module connector; the interface module is connected with the weapon nacelle, the communication nacelle and the onboard equipment through the connector; the power supply module is connected with a power supply through a connector; helicopter real soldier combat system data processing unit, can accomplish collection, analog simulation, analysis processes and the storage of helicopter signal, coordinate and accomplish data real-time transmission and control, the main tactics technical performance and the real equipment performance of the weapon that makes the system simulation are unanimous, and the helicopter pilot uses the operating procedure when weapon system carries out the combat training unanimous with the real equipment, the system adjudication result is accurate, the hit rate is high, has effectively improved pilot's technical and tactics level.

Description

Helicopter actual combat system data processing unit
Technical Field
The utility model relates to a data analysis field especially relates to a helicopter real soldier combat system data processing unit.
Background
The system on the market at present can not be crosslinked with an airborne system, so that the perception of the aerial combat process is difficult, the fire fighting process of both sides of the combat can not be accurately perceived and controlled, the response to the combat process can not be accurately and real-timely, and a unified guiding and adjusting controller is not available, so that the situation of both sides can not be easily judged, the control deviation is easily caused, the tactical technical performance and the actual installation performance of the helicopter actual combat system are inconsistent, and the operation program of a weapon system is inconsistent with the actual installation.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a helicopter real soldier's combat system data processing unit to solve the aforementioned problem that exists among the prior art.
In order to realize the purpose, the utility model discloses a technical scheme as follows:
a helicopter actual combat system data processing unit comprises a main processor module, an interface module, a power module, a mother board, a case, a connector and a mounting bracket; the host processor module, the interface module and the power supply module are all connected with the motherboard; the interface module and the power supply module are both connected with the connectors; the interface module connects the ordnance pod, the communications pod and the onboard equipment through the connector using a connection cable; the power supply module is connected with a power supply through a connector; the motherboard, the host processor module, the interface module, the power module and the connector are arranged inside the case, the case is provided with an extending hole of the connector, and the host processor module, the power module and the interface module are arranged on the mounting bracket side by side.
Preferably, the power module is connected with a helicopter power supply and provides a working power supply for the data processing unit.
Preferably, the interface module comprises 2 discrete quantity interfaces and 3 data bus interfaces.
Preferably, the data processing unit can interconnect and analyze the data information of the ordnance pod, the communication pod and the onboard equipment in real time and send control information to the equipment.
The utility model has the advantages that: helicopter actual soldier combat system data processing unit, through being connected with weapon nacelle, communication nacelle and onboard equipment, can accomplish the collection, simulation, analysis and processing and the storage of helicopter signal, coordinate and accomplish data real-time transmission and control, make the main tactics technical performance of the weapon of system simulation unanimous with the actual equipment performance, and the helicopter pilot uses operating procedure when weapon system carries out the combat training unanimously with the actual equipment, the system adjudication result is accurate, the hit rate is high, pilot's technical and tactics level has effectively been improved.
Drawings
FIG. 1 is a schematic view of a data processing unit installation;
FIG. 2 is a system cross-link diagram of a data processing unit;
FIG. 3 is a diagram of the internal connections of a data processing unit;
in the figure, 1 is a power supply module, 2 is a main processor module, 3 is an interface module, 4 is a connector, 5 is a mounting bracket, and 6 is a case.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more clearly understood, the present invention is further described in detail below with reference to the accompanying drawings. It should be understood that the detailed description and specific examples, while indicating the invention, are given by way of illustration only.
A helicopter actual combat system data processing unit is shown in figure 1 in a mounting position relation and comprises a main processor module 2, an interface module 3, a power module 1, a motherboard, a case 6, a connector 4 and a mounting bracket 5; the connection relationship among the above components is shown in fig. 2, and the host processor module 2, the interface module 3 and the power module 1 are all connected with the motherboard; the interface module 3 and the power module 1 are connected through a connector 4; the interface module 3 is connected with the weapon nacelle, the communication nacelle and the onboard equipment through the connector 4 by using a connecting cable; the power supply module 1 is connected with a power supply through a connector 4; the motherboard, the host processor module 2, the interface module 3, the power module 1 and the connector 4 are mounted inside the case 6, the case 6 is provided with an extending hole of the connector 4, and the host processor module 2, the power module 1 and the interface module 3 are mounted on the mounting bracket 5 side by side.
The power module 1 is connected with an onboard power supply and provides a working power supply for the data processing unit, the interface module 3 comprises 2 discrete quantity interfaces and 3 data bus interfaces and can be used for processing various discrete, analog and digital information acquisition of helicopter states, and the main processor module 2 can be used for processing, analyzing and storing the information acquired by the interface module 3; the motherboard can realize the transmission, processing and analysis of data information of the interface module 3, the power module 1 and the host processor module 2; the interface module 3 is connected with the weapon nacelle, the communication nacelle and the onboard equipment, can receive information transmitted by the equipment, calculates through the motherboard, transmits the information into the main processing module 2 for data processing, and sends a control instruction according to the information, so that real-time transmission and centralized control of data are realized.
The data processing unit receives the control information of the weapon pod, the storage information of the communication pod and the state information of the onboard equipment, and after the data processing and analysis of the main processor module, the data processing unit transmits and coordinates and controls the information in real time, so that the control functions of power supply, laser, self-checking, resetting and the like can be completed, and commands of failure, ammunition, destruction, laser emission and the like can be sent to the weapon pod or the communication pod.
Through adopting the utility model discloses an above-mentioned technical scheme has obtained following profitable effect:
helicopter actual soldier combat system data processing unit, through being connected with weapon nacelle, communication nacelle and onboard equipment, can accomplish the collection, simulation, analysis and processing and the storage of helicopter signal, coordinate and accomplish data real-time transmission and control, make the main tactics technical performance of the weapon of system simulation unanimous with the actual equipment performance, and the helicopter pilot uses operating procedure when weapon system carries out the combat training unanimously with the actual equipment, the system adjudication result is accurate, the hit rate is high, pilot's technical and tactics level has effectively been improved.
The foregoing is only a preferred embodiment of the present invention, and it should be noted that, for those skilled in the art, a plurality of improvements and decorations can be made without departing from the principle of the present invention, and these improvements and decorations should also be viewed as the protection scope of the present invention.

Claims (4)

1. A helicopter actual combat system data processing unit is characterized by comprising a main processor module, an interface module, a power supply module, a mother board, a case, a connector and a mounting bracket; the host processor module, the interface module and the power supply module are all connected with the motherboard; the interface module and the power supply module are both connected with the connectors; the interface module connects the ordnance pod, the communications pod and the onboard equipment through the connector using a connection cable; the power supply module is connected with a power supply through a connector; the motherboard, the host processor module, the interface module, the power module and the connector are arranged inside the case, the case is provided with an extending hole of the connector, and the host processor module, the power module and the interface module are arranged on the mounting bracket side by side.
2. The helicopter actual combat system data processing unit of claim 1 wherein the power module is connected to a helicopter power supply to provide operating power to the data processing unit.
3. A helicopter actual combat system data processing unit as claimed in claim 1 wherein said interface module includes 2 discrete magnitude interfaces and 3 data bus interfaces.
4. A helicopter actual combat system data processing unit as claimed in claim 1 wherein said data processing unit is capable of interconnecting and analyzing data information of said weapons pods, said communications pods and said onboard equipment in real time and sending control information to said equipment.
CN201921921905.7U 2019-11-08 2019-11-08 Helicopter actual combat system data processing unit Active CN210466264U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201921921905.7U CN210466264U (en) 2019-11-08 2019-11-08 Helicopter actual combat system data processing unit

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201921921905.7U CN210466264U (en) 2019-11-08 2019-11-08 Helicopter actual combat system data processing unit

Publications (1)

Publication Number Publication Date
CN210466264U true CN210466264U (en) 2020-05-05

Family

ID=70437270

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201921921905.7U Active CN210466264U (en) 2019-11-08 2019-11-08 Helicopter actual combat system data processing unit

Country Status (1)

Country Link
CN (1) CN210466264U (en)

Similar Documents

Publication Publication Date Title
CN106656683B (en) A kind of UAV Communication link failure detection device and method
CN102221309B (en) Rocket and antiaircraft gun operation control and safety monitoring system and operation monitoring method
KR101445669B1 (en) Combat Interface Analysis System for the interface performance check between command fire control system and ship installed equipments, Signal distribution apparatus and Conversion apparatus adopted thereto
CN109398709B (en) External airborne weapon fire control system and use method
CN107870631A (en) A kind of unmanned helicopter-mounted system and its control method
CN106991861A (en) The embedded tactical training system of distributed modular
KR100808026B1 (en) Simulator apparatus for flight test system and simulation method by the same
CN210466264U (en) Helicopter actual combat system data processing unit
CN109398716B (en) External airborne control system
CN111924103A (en) Intelligent bomb striking system of autorotation gyroplane
CN210039184U (en) Radar interference equipment simulation training system
CN208775020U (en) External fire control system
CN207440280U (en) A kind of autonomous controllable general purpose radar terminal system
CN214620859U (en) Missile launcher outfield diagnostic system
CN207585439U (en) A kind of weapon station equipment for unmanned boat
CN211855066U (en) Weapon nacelle of helicopter actual combat system
CN112256053A (en) Fire control photoelectric system of small-sized scouting and fighting unmanned aerial vehicle
CN114383464A (en) Launching control simulation system and method for micro missile
CN110701959A (en) Weapon nacelle of helicopter actual combat system
CN112286076A (en) Real vehicle fire control trigger data acquisition simulation system
CN107870628A (en) A kind of depopulated helicopter ground control system and its control method
CN215177232U (en) Unmanned system aims and shoots analog system
US8967032B2 (en) Smart-store emulation unit
CN110930797A (en) Distributed modular virtual-real reconfigurable tactical training system
CN106097681A (en) The device and method of Fructus Rubi group, system, sensor network is remotely controlled based on XBee

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant