Flight control system flexible integration test platform and test method

An integrated test platform and flight control system technology, applied in the field of airborne system simulation, can solve problems such as the inability to meet the requirements of integrated test tasks, and achieve low-cost effects

Pending Publication Date: 2022-07-29
中航机载系统共性技术有限公司
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Under the conditions of limited funds and development cycle, the current development of a specific integrated test platform model for model projects can no longer meet the requirements of actual integrated test tasks

Method used

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  • Flight control system flexible integration test platform and test method
  • Flight control system flexible integration test platform and test method

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Embodiment Construction

[0032] Embodiments of the technical solutions of the present invention will be described in detail below with reference to the accompanying drawings. The following examples are only used to illustrate the technical solutions of the present invention more clearly, and are therefore only used as examples, and cannot be used to limit the protection scope of the present invention.

[0033] It should be noted that, unless otherwise specified, the technical or scientific terms used in this application should have the usual meanings understood by those skilled in the art to which the present invention belongs.

[0034] figure 1 For a structural block diagram of a flexible integrated test platform for a flight control system provided by an embodiment of the present invention, refer to figure 1 , the test platform includes: flight control test configuration and management module, flight control manipulation command simulation module, distributed simulation system and flight control in...

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Abstract

The invention belongs to the technical field of airborne system simulation, and provides a flight control system flexible integration test platform and test method. The test platform comprises a flight control test configuration and management module, a flight control manipulation instruction simulation module, a distributed simulation system and a flight control interface simulation system. The flight control test configuration and management module comprises a plurality of components I, and is used for selecting a plurality of components I to generate test configuration and management software; the flight control command simulation module comprises a plurality of second components and is used for selecting the second components to generate flight control command simulation software; and the distributed simulation system is used for receiving and processing instructions of the flight control test configuration and management software and the flight control operation instruction simulation software, and performing data interaction with the real flight control equipment through the flight control interface simulation system. According to the test platform, the flight control integrated test platform with complete functions and stable performance can be quickly customized based on requirements, and task requirements are met.

Description

technical field [0001] The invention relates to the technical field of airborne system simulation, in particular to a flexible integrated test platform and a test method of a flight control system. Background technique [0002] With the continuous progress of electronic technology, the civil aircraft flight control system is developing in the direction of integration, generalization and modularization. While the functions are becoming more and more powerful, the degree of integration is becoming higher and higher, and the system cross-linking relationship is also becoming more and more important. complex. At the same time, the flight control system has become the most critical component of the aircraft, which plays a vital role in the safe flight of the aircraft and is one of the key objects of the airworthiness review. Therefore, in order to meet the flight airworthiness requirements, it is necessary to carry out multi-level and sufficient testing and verification of the c...

Claims

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Application Information

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Patent Type & AuthorityApplications(China)
IPC IPC(8): G05B23/02
CPCG05B23/0213G05B2219/24065
Inventor王闯牟明贺莹邹方林张博林李阳赵文周乐凯陈亮
Owner中航机载系统共性技术有限公司