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A self-detection method for power-on and start-up of flight control system based on xml technology

A technology of flight control system and electric start, which is applied in the direction of faulty hardware test method, detection of faulty computer hardware, use of power-on test to detect faulty hardware, etc., can solve the problems of increased testing and verification costs, and save development time and verification time, increase software reusability, and strong applicability

Active Publication Date: 2020-04-07
FLIGHT AUTOMATIC CONTROL RES INST
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  • Abstract
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Problems solved by technology

Even for the same requirements, different designers have different code styles, which makes the software codes have their own merits, which eventually leads to an increase in testing and verification costs.

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  • A self-detection method for power-on and start-up of flight control system based on xml technology
  • A self-detection method for power-on and start-up of flight control system based on xml technology
  • A self-detection method for power-on and start-up of flight control system based on xml technology

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Embodiment Construction

[0017] The technical solution will be described in further detail below in conjunction with the accompanying drawings.

[0018] The method mainly integrates the detection item codes required by the flight control system PUBIT into a standard library, manages and transfers the required PUBIT detection items through XML technology, and generates the target code XML control file for the transferred PUBIT detection items, based on This file generates object code matching the flight control system.

[0019] The overall structure of the present invention is as figure 1 As shown, its content mainly includes: the standard library of PUBIT detection module and the XML file cross-linked with the library, the selection of test module and module configuration, the generation of object code XML control file, and the generation of object code.

[0020] 1. Establishment of the standard library of the PUBIT detection module and the XML file cross-linked with the library:

[0021] Select gen...

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Abstract

The invention relates to a power-on starting self-test method of a flight control system, in particular to the power-on starting self-test method of the flight control system based on an XML technology. The method mainly comprises the steps of integrating codes of test items required by the flight control system PUBIT to a standard library, managing and calling the required PUBIT test items through the XML technology, generating a target code XML control file with the called PUBIT test items, and generating a target code matched with the flight control system base on the file. When a power-on starting self-test function of a new type is designed, compared with a prior hand-coding method, according to the power-on starting self-test method of the flight control system based on the XML technology, a code module is managed and called through the XML technology, the software reusability is improved, the software development and verification time is shortened, and the development efficiency is improved.

Description

technical field [0001] The invention relates to a power-on self-detection method of a flight control system, in particular to a power-on self-detection method of a flight control system based on XML technology. Background technique [0002] In the fly-by-wire flight control system, the power-on internal self-test (PUBIT, this abbreviation will be used later to replace the power-on internal self-test) is a self-test module designed to detect the integrity of the flight control computer hardware during power-on. It plays a vital role in the safety of aircraft take-off. In the previous design, PUBIT mainly developed and designed around the required functions. Since the required functions of different aircraft models are not exactly the same, each model needs to be re-coded manually. Even for the same requirements, different designers have different code styles, which makes the software codes have their own merits, which eventually leads to an increase in testing and verificati...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F11/22
CPCG06F11/2273G06F11/2284
Inventor 刘羽武方方张向虎冯博陈皓侯明董康张玉博
Owner FLIGHT AUTOMATIC CONTROL RES INST