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Acta Aeronautica et Astronautica Sinica ›› 2025, Vol. 46 ›› Issue (19): 531273.doi: 10.7527/S1000-6893.2024.31273

• Special Issue: Aircraft Digital Twin Technology • Previous Articles     Next Articles

Digital-twin’s modelling and dynamic adjustment mechanism of rudder-loop-system under fault conditions

Junqi LEI1, Yuehua CHENG1(), Bin JIANG1, Cheng XU2, Guili XU1, Tianyu SUN1   

  1. 1.College of Automation Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 211106,China
    2.Key Laboratory of Complex System Control and Intelligent Cooperative Technology,Beijing 100074,China
  • Received:2024-09-27 Revised:2024-10-21 Accepted:2024-12-05 Online:2024-12-10 Published:2024-12-10
  • Contact: Yuehua CHENG E-mail:chengyuehua@nuaa.edu.cn
  • Supported by:
    National Key Research and Development Program of China(2023YFB3307100)

Abstract:

To address the challenges of limited and incomplete measurable data in fault detection, diagnosis, and prediction of the rudder-loop-system in long-endurance reusable aircraft, this study introduces a digital twin-based approach for health management of the system. First, a digital twin framework for the aircraft’s rudder-loop-system is proposed, incorporating high-fidelity modelling and simulation of mechanical, electrical, control, and dynamic flight load subsystems using AMESim and FLUENT. The integrated model realizes the coupling of three-phase electro-mechanical control with real-time flight dynamic loading. Subsequently, to ensure consistency between the digital twin and the physical system under various operational conditions including normal, rudder surface degradation, and loosening faults, a virtual-physical consistency perception method and a dynamic adjustment mechanism are developed. This enables the digital twin to continuously track physical system changes and maintain synchronization through online fault perception and dynamic updating. Finally, experimental results demonstrate that under both normal and faulty conditions, the digital and physical systems exhibit consistent trends and amplitudes in multiple time-domain indicators of rudder current and deflection angle. Moreover, the expanded data dimensions provided by the digital twin enhance the comprehensiveness of data available for health management. This research highlights the potential of digital twin applications in improving the reliability and maintainability of electric rudders in advanced flight systems.

Key words: digital twin, aircraft’s rudder-loop-system, health management, electric rudders, digital twin’s applications

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