Multifunctional electromechanical system simulation method for simulation of airplane power supply control management system

A power supply control and management system technology, applied in the field of computer simulation, can solve the problems of low utilization rate of hardware resources, not easy to carry, large system, etc., and achieve the effect of light weight, high utilization rate and small size

Active Publication Date: 2012-06-20
XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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Problems solved by technology

Such an emulator is actually a LAN emulation system composed of multiple industrial computers, which has the ...

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  • Multifunctional electromechanical system simulation method for simulation of airplane power supply control management system
  • Multifunctional electromechanical system simulation method for simulation of airplane power supply control management system
  • Multifunctional electromechanical system simulation method for simulation of airplane power supply control management system

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Embodiment Construction

[0033] The present invention will be further described below by means of specific embodiments:

[0034] According to the scheme, the implementation of the multifunctional electromechanical system simulator is divided into hardware implementation and software implementation, which are described as follows:

[0035] 8.1 Hardware implementation

[0036] The hardware implementation of the multifunctional electromechanical system simulator consists of the hardware devices in Table 1.

[0037] Table 1 The hardware composition of the multifunctional electromechanical system simulator

[0038]

[0039]

[0040] 8.2 Software implementation

[0041] The software of the multifunctional electromechanical system simulator is composed of fuel subsystem simulator software, hydraulic subsystem simulator software, environmental control subsystem simulator software and electromechanical management subsystem simulator software.

[0042] Fuel subsystem simulator software, hydraulic subsy...

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Abstract

The invention discloses a multifunctional electromechanical system simulation method for simulation of an airplane power supply control management system, belongs to the computer simulation technology, and particularly relates to improvement of a multifunctional electromechanical system simulation method for simulation of an airplane power supply control management system. The multifunctional electromechanical system simulation method is characterized by comprising a hardware system and a software system, wherein the hardware system in a design scheme consists of an industrial control computer, a 64-route discrete variable I/O (input/output) card and a CAN (controller area network) bus communication card, and the software system in the design scheme comprises fuel subsystem simulator software, hydraulic subsystem simulator software, loop control subsystem simulator software and electromechanical management subsystem simulator software. Simulation functions of multiple electromechanical subsystems can be realized by a multifunctional electromechanical system simulator, various electromechanical subsystem simulators share the same hardware resources, and utilization rate of the hardware resources is improved. In addition, the multifunctional electromechanical system simulator is small in volume, light in weight and convenient in carrying. Besides, the multifunctional electromechanical system simulation method is quickly adaptive to changes of a scheme of an electromechanical system by means of updating the software, and is high in flexibility.

Description

technical field [0001] The invention belongs to computer simulation technology, and in particular relates to the improvement of a multifunctional electromechanical system simulation method for simulation of an aircraft power supply control management system. Background technique [0002] The aircraft power supply system is one of the important support systems of the aircraft, which consists of a power supply system and a power distribution system. With the increasing electrification of aircraft on-board systems, there is a trend of using electric energy to gradually replace or even completely replace other secondary energy sources on the aircraft. The substantial increase in aircraft electrical equipment has led to an increase in power supply, an increase in the weight of the aircraft grid, reduced reliability, and difficult maintenance. In order to solve these problems, modern advanced aircraft use a distributed control system to reduce the weight of the grid. Increase sys...

Claims

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Application Information

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IPC IPC(8): G05B17/02
Inventor 张勇李忍锁闫云娟
Owner XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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