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Fault simulation device of fiber channel avionics environment (FC-AE)-1533 device

A technology for simulating device and equipment failures, used in instruments, simulators, electrical testing/monitoring, etc.

Active Publication Date: 2012-09-12
HARBIN INST OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At present, there is no FC-AE-1533 equipment fault simulation device that can test FC-AE-1533 through fault injection in the domestic market

Method used

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  • Fault simulation device of fiber channel avionics environment (FC-AE)-1533 device
  • Fault simulation device of fiber channel avionics environment (FC-AE)-1533 device
  • Fault simulation device of fiber channel avionics environment (FC-AE)-1533 device

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Experimental program
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specific Embodiment approach 1

[0013] Specific implementation mode 1. Combination figure 1 Describe this specific implementation mode, FC-AE-1533 equipment failure simulation device, it includes programmable logic device 1, photoelectricity / electro-optic conversion module 2 and failure simulation upper computer 4;

[0014] The internal construction of programmable logic device 1 has Qsys system, and described Qsys system comprises NIOSII processor 11, optical fiber interface module 12, PCIe module 13 and AVALON bus 14;

[0015] NIOSII processor 11, optical fiber interface module 12 and PCIe module 13 are all mounted on the AVALON bus 14;

[0016] NIOSII processor 11 is used to send control order to optical fiber interface module 12 and PCIe module 13;

[0017] The PCIe module 13 is used to receive the injection fault information from the fault simulation host computer 4 and carry out data interaction with the simulation host computer 4 through the PCIe interface;

[0018] The optical fiber interface modul...

specific Embodiment approach 2

[0035] Embodiment 2. The difference between this embodiment and the FC-AE-1533 equipment failure simulation device described in Embodiment 1 is that the power module 3 is used to provide work to the programmable logic device 1 and the photoelectric / electrical-optical conversion module 2. power supply.

specific Embodiment approach 3

[0036] Specific Embodiment 3. The difference between this specific embodiment and the FC-AE-1533 equipment failure simulation device described in specific embodiment 1 is that the programmable logic device 1 is an FPGA with a model number of EP2AGX45DF29.

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Abstract

The invention discloses a fault simulation device of a fiber channel avionics environment (FC-AE)-1533 device, which relates to the fault simulation device. In order to simulate a fault of the FC-AE-1533 device so as to detect the fault of the FC-AE-1533 device, a Qsys system is built inside a programmable logic device. An NIOSII processor in the Qsys system is used for transmitting a control command to an optical fibre interface module; a PCIe module is used for receiving the fault injected from a fault simulation host computer and carrying out data interaction with the simulation host computer, and the optical fibre interface module is used for carrying out 8B / 10B encoding and transmitting on the data, transmitting the injected fault, and carrying out decoding and CRC (cyclic redundancy check) on the received data. The fault simulation device of the FC-AE-1533 device disclosed by the invention can be widely applied to an avionic device, a fighter plane, a civil airplane, naval vessels and other occasions with the device meeting the FC-AE-1533 protocol, and can carry out the work such as maintaining, testing, fault overhauling and the like on the product.

Description

technical field [0001] The invention relates to an equipment failure simulation device. Background technique [0002] With the development of aerospace electronic buses, the interconnection performance between devices and the requirements for data throughput are also gradually increasing, and the FC-AE-1553 bus based on Fiber Channel technology has advantages in data transmission bandwidth and network performance. It has become the military bus standard following the MIL-STD-1553B bus, and will be more and more used in spaceborne, shipborne, airborne and other equipment. With the in-depth research on FC-AE-1533, FC-AE-1533 equipment will emerge in large numbers, and the problem of lack of bus test means becomes increasingly prominent. At present, there is no FC-AE-1533 equipment fault simulation device that can test FC-AE-1533 through fault injection in the domestic market. Contents of the invention [0003] The present invention aims at performing fault simulation on FC...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B17/02G05B23/02
Inventor 凤雷乔家庆冯收刘冰尹洪涛付平孟升卫赵加凤李红杰
Owner HARBIN INST OF TECH
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