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Flight parameter system testing platform and method based on PXI bus

A flying parameter system and test platform technology, applied in the field of flying parameter system test platform based on PXI bus, can solve the problems of system complexity, waste of resources and high cost, and achieve the effect of advanced technology, cost reduction and volume reduction.

Active Publication Date: 2018-03-09
SHAANXI QIANSHAN AVIONICS
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  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0003] At present, the test of the flying reference system usually adopts the general test equipment based on the VXI bus or PCI bus suitable for the test of the flying reference system, which has a single type of signal, insufficient number of signal channels, and the test equipment is large in size, heavy in weight, and inconvenient to move. characteristics, high cost, backward technology, complex system, often resulting in waste of resources and insufficient verification of the flight reference system.

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  • Flight parameter system testing platform and method based on PXI bus
  • Flight parameter system testing platform and method based on PXI bus
  • Flight parameter system testing platform and method based on PXI bus

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Embodiment Construction

[0021] Below in conjunction with accompanying drawing the present invention is described in further detail, please refer to Figure 1-3 .

[0022] The invention relates to a PXI bus-based flight reference system test platform, which is based on the PXI bus as a hardware platform, and includes PXI test equipment, a power control box, a DC-controlled stabilized voltage power supply, a KVM display, a shock-absorbing chassis, and a drawer.

[0023] The PXI test equipment takes the PXI controller as the core, and the PXI controller uses the internal PXI bus to control the frequency module, DC analog module, HDLC bus module, RS-422 bus module, HB-6096 bus module, DFTI and Harvard code bus module , signal acquisition module, switch module, multi-function module, synchronizer module and other signal modules, output the simulation signals required by various flight reference systems, and all modules are installed on the backplane, and the power supply module supplies each signal throug...

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Abstract

The invention belongs to the field of aerospace electronic testing and relates to a flight parameter system testing platform and method based on a PXI bus. At present, for flight parameter system testing, universal testing devices suitable for flight parameter system testing and based on a VXI bus or PCI bus are generally adopted and have the shortcomings of single signal type and insufficient signal channels. The flight parameter system testing platform based on the PXI bus comprises a PXI testing device, a power supply control box, a direct-current program control voltage-stabilizing power supply and a KVM display. Based on the flight parameter system testing platform, modules on the PXI bus are driven through a PXI controller to output simulation signals to a flight parameter system, and data recorded by the flight parameter system is downloaded and is compared with originally uploaded data. The cost is reduced, and functions of real-time dynamic signal simulation, synchronous signal simulation, switch quantity valve value testing and the like are provided.

Description

technical field [0001] The invention belongs to the field of avionics testing, and relates to a test platform and method for a flight reference system based on a PXI bus. Background technique [0002] The flight reference system is a device that automatically collects and records various flight data, audio data and video data according to the agreed format during the flight of the aircraft. These data reflect the working status of the aircraft and the operation of the pilot during the flight. The performance, quality, and accuracy of recorded data of the flight reference system directly affect the daily maintenance of the aircraft, the elimination of hidden troubles, the development of new models, and the search and rescue of aircraft crashes. [0003] At present, the test of the flying reference system usually adopts the general test equipment based on the VXI bus or PCI bus suitable for the test of the flying reference system, which has a single type of signal, insufficien...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F5/60
CPCB64F5/60
Inventor 孙爱国刘生桂田博
Owner SHAANXI QIANSHAN AVIONICS