Multi-aircraft coordinated combat simulation control apparatus

A control device and simulation technology, applied in general control systems, control/regulation systems, instruments, etc., can solve the problems of inability to multi-machine cooperative combat ground simulation launch command control, the quantity cannot meet the demand, and the simulation progress is affected. The effect of the urgent need for the test, the reduction of the difficulty of equipment operation and personnel coordination, and the reduction of preparation time

Active Publication Date: 2016-11-09
JIANGXI HONGDU AVIATION IND GRP
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  • Summary
  • Abstract
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] 1) Multi-machine cooperative power supply control requires multiple sets of simulation control devices to supply power to the aircraft, and the number of existing simulation control devices cannot meet the demand;
[0004] 2) The software loading device must be used when loading the software of the aircraft. For the loading of multiple sets of aircraft during multi-aircraft co-simulation, repeated disassembly of the loading test cable is required, which affects the simulation process;
[0005] 3) Since the multi-machine collaborative simulation power supply control bypasses the electrical integrated control combination to directly supply power to the aircraft, the launch command control principle is different from the past. The existing simulation control device cannot perform the launch command control of the multi-machine cooperative combat ground simulation;
[0006] 4) If existing resources are used for multi-machine cooperative combat ground simulation, it is necessary to deploy multiple simulation control devices and software loading devices. At the same time, multiple operators also need to cooperate during the simulation process, which is likely to be caused by personnel operating errors. Simulation interruption is time-consuming and labor-intensive and affects the simulation progress

Method used

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  • Multi-aircraft coordinated combat simulation control apparatus
  • Multi-aircraft coordinated combat simulation control apparatus
  • Multi-aircraft coordinated combat simulation control apparatus

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Embodiment Construction

[0021] The present invention will be further described below in conjunction with the accompanying drawings and specific embodiments. The following examples are only used to illustrate the present invention, and are not intended to limit the protection scope of the present invention.

[0022] Such as figure 1 As shown, a multi-machine cooperative combat simulation control device of the present invention includes a power supply control module 1, a launch control module 2, a software loading control module 3 and an address bit control module 4,

[0023] refer to figure 2 , power supply control module 1 includes 3-way DC power input, high-power load switch S1~S5, co-effort XL5315V series voltmeter A1~A3 and ammeter V1~V5, shunt FL1~FL5, fuse FU1~FU5, diode indicator light L1 ~L5 and reference voltage divider resistors R1~R5.

[0024] The second and third input negatives of the DC power supply are connected in parallel with the negative input of the first DC power supply. When ...

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Abstract

The invention discloses a multi-aircraft coordinated combat simulation control apparatus. The apparatus comprises a power supply control module, an emission control module, a software loading control module and an address bit control module, wherein the power supply control module provides power supply control for aircrafts; the emission control module obtains discrete magnitude signals from a power supply input end and emits control instruction signals through a delay relay and switches to realize emission control of the aircrafts; the software loading control module performing software loading on simulation systems I, II and III; and the address bit control module is connected with the corresponding switches and carries out address bit control thorough controlling whether the switches are connected with an address loop. The apparatus substantially reduce preparation time before a test, the workload, operation personnel and simulation time, and ensures what is urgently needed for the test.

Description

technical field [0001] The invention relates to a simulation test control device, in particular to a multi-machine cooperative combat simulation control device. It is used to complete related test tasks such as power supply control, launch command control, software loading control and address bit control during ground simulation of multiple aircraft cooperative operations. Background technique [0002] A series of control processes such as ground power supply, software loading and launch control need to be completed during ground simulation of multi-machine cooperative combat. Traditional test methods have the following disadvantages: [0003] 1) Multi-machine cooperative power supply control requires multiple sets of simulation control devices to supply power to the aircraft, and the number of existing simulation control devices cannot meet the demand; [0004] 2) The software loading device must be used when loading the software of the aircraft. For the loading of multip...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B17/02
CPCG05B17/02
Inventor 邹小霞李维彭江军黄桂明冯晓艳孙锐袁丹郑宏海衷莉莎王锦菲巩三莉郭娟
Owner JIANGXI HONGDU AVIATION IND GRP
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