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Development and Application Test of the Wing State Monitoring System for Civil Large Aircraft
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Ya-yan LIU1, Rui-jie LI1, Can FENG1, *, Jun-xia SONG1, Shang-bin XI2
Science Technology and Engineering | 2025, 25(10) : 4371 - 4376
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Science Technology and Engineering | 2025, 25(10): 4371-4376
• Papers·Aeronautics and Astronautics •
Development and Application Test of the Wing State Monitoring System for Civil Large Aircraft
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Ya-yan LIU1, Rui-jie LI1, Can FENG1, *, Jun-xia SONG1, Shang-bin XI2
Affiliations
  • 1 Shanghai Aircraft Test Flight Engineering Co., Ltd., Shanghai 201323, China
  • 2 Zhejiang Tsinghua Flexible Electronics Research Institute, Jiaxing 314000, China
Published: 2025-04-08 doi: 10.12404/j.issn.1671-1815.2403687
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Unique test requirements in civil large aircraft flight testing, characterized by short task durations, wide measurement point distribution, and numerous measurement locations, are addressed. Challenges in the existing wired Ethernet-based onboard data acquisition systems, including difficult measurement equipment installation, complex test cable layout, and prolonged retrofitting periods, are identified. A flexible, miniaturized, and compact space-compatible measurement system for critical wing structural state parameter measurements during civil aircraft flight testing was proposed. An integrated microsystem, including a flexible antenna module and a multi-sensor parameter collection module, was developed and integrated into the civil aircraft wing. The system's reliability and stable signal transmission were demonstrated. The design and application of a wireless flexible measurement system for wing state monitoring on civil aircraft were detailed. The system design approach, data transmission strategy, and integration with third-party loggers were described. Ground and flight tests were conducted to collect data.The onboard flexible system's capability to measure temperature, three-axis vibration, and pressure is verified.

civil aircraft flight test  /  flexible acquisition system  /  data acquisition and recording  /  system development  /  flexible antenna
Ya-yan LIU, Rui-jie LI, Can FENG, Jun-xia SONG, Shang-bin XI. Development and Application Test of the Wing State Monitoring System for Civil Large Aircraft[J]. Science Technology and Engineering, 2025 , 25 (10) : 4371 -4376 . DOI: 10.12404/j.issn.1671-1815.2403687
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Year 2025 volume 25 Issue 10
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Article Info
doi: 10.12404/j.issn.1671-1815.2403687
  • Receive Date：2024-05-18
  • Online Date：2025-07-09
  • Published：2025-04-08
Article Data
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  • Received：2024-05-18
  • Revised：2025-01-10
Affiliations
    1 Shanghai Aircraft Test Flight Engineering Co., Ltd., Shanghai 201323, China
    2 Zhejiang Tsinghua Flexible Electronics Research Institute, Jiaxing 314000, China
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