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Automatic detection method for digital aircraft source program written by artificial intelligence programmer

An artificial intelligence and automatic detection technology, applied in program control, instrumentation, electrical testing/monitoring, etc., can solve the problems of complex structure, error-prone, and heavy detection workload of digital aircraft simulation source program, so as to improve efficiency and results. Reliability, reduce test errors, improve test efficiency

Active Publication Date: 2020-12-29
BEIHANG UNIV
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AI Technical Summary

Problems solved by technology

The digital aircraft simulation source program has the characteristics of complex structure, mass production, and large differences. If all the source program correctness detection is completed by humans, the workload is heavy, the content is cumbersome, and error-prone

Method used

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  • Automatic detection method for digital aircraft source program written by artificial intelligence programmer
  • Automatic detection method for digital aircraft source program written by artificial intelligence programmer
  • Automatic detection method for digital aircraft source program written by artificial intelligence programmer

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Embodiment

[0043] The content of the digital aircraft source code assembly for automatic detection is to detect the digital satellite simulation source program, and the satellite subsystem performs the simulation of the attitude and orbit control subsystem and the thermal control subsystem. Among them, the attitude and orbit control subsystem includes the following components: GPS, on-board computer, momentum wheel, and the thermal control subsystem include temperature measuring resistors and heaters. The simulation content carried out includes orbital dynamics simulation, attitude dynamics simulation, and space thermal simulation.

[0044] Firstly, the detection content is determined according to the assembly result. The static test process is as follows. The components for information transmission are GPS, on-board computer and momentum wheel. The GPS communicates with the on-board computer through the UART line, and the on-board computer communicates with the momentum wheel through th...

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Abstract

The invention discloses an automatic detection method for writing digital aircraft source programs by artificial intelligence programmers, comprising the following steps: 1) building and maintaining a test database; 2) selecting test items in the test database, determining the items to be tested, and arranging Test process; 3) automatic scheduling detection method: according to the determined item to be tested, select the detection method from the test database; 4) automatically execute the detection process: formulate the simulation working conditions of each detection method in the test database , using the method of batch processing to run the simulation program sequentially, to archive the detection results, and to compare the correctness of the results according to the comparison method of the detection results; 5) automatically generating a detection report. The invention provides an automatic detection method for an artificial intelligence programmer to write a digital aircraft source program, which improves the efficiency of the digital aircraft simulation source program detection work and the reliability of the result.

Description

technical field [0001] The invention relates to the technical field of automatic testing, and more specifically relates to an automatic testing method for writing digital aircraft source programs by artificial intelligence programmers. Background technique [0002] The aircraft has the characteristics of high cost, low repeatability, and high reliability requirements. The space environment in which the aircraft operates is complex. Ground digital simulation technology and semi-physical simulation technology provide a guarantee for verifying the rationality of the aircraft design and the actual operation of the aircraft. [0003] A digital aircraft is one or more aircraft integrated in the digital space according to the composition and structure of the real aircraft. The aircraft runs in the space environment simulated by the software, which is consistent with the model and parameters of the real aircraft. It dynamically simulates the various subsystems and components of the ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05B23/02
CPCG05B23/0213G05B2219/24065
Inventor 董云峰何昌远
Owner BEIHANG UNIV
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