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Acta Aeronautica et Astronautica Sinica ›› 2025, Vol. 46 ›› Issue (12): 130972.doi: 10.7527/S1000-6893.2024.30972

• Fluid Mechanics and Flight Mechanics • Previous Articles    

Research and verification of rigid-elastic coupling analysis technology for large passenger aircraft

Kun MAO1,2(), Wuxing JING1, Shi CHEN2, Jun LIU2, Dawei WU2, Jiangtao SI2   

  1. 1.School of Astronautics,Harbin Institute of Technology,Harbin 150001,China
    2.Shanghai Aircraft Design and Research Institute,Shanghai 201210,China
  • Received:2024-07-22 Revised:2024-10-22 Accepted:2024-12-04 Online:2024-12-13 Published:2024-12-12
  • Contact: Kun MAO E-mail:maokunhao@126.com
  • Supported by:
    Provincial or Ministerial Level Project

Abstract:

The difference in the frequency of rigid-body mode and the elastic mode of modern large passenger aircraft is becoming smaller, and the problem of rigid-elastic coupling during maneuvering is becoming increasingly apparent. Traditional flight dynamics simulation with six degrees of freedom cannot simulate this rigid-elastic coupling process, which is unfavorable for the optimization of control laws or the development of flight training simulators. By analyzing the basic motion characteristics of large passenger aircraft, we use the mean axis system method to extend the traditional flight dynamics equation, and construct a rigid-elastic coupling flight dynamics simulation model for large passenger aircraft, significantly simplifying the analysis process while inheriting the original simulation system. Meanwhile, the rigid-elastic coupling simulation model is used to analyze the typical rigid-elastic coupling problem of large passenger aircraft under pitch and roll maneuvers, with comparison with flight test results to verify the accuracy of the model. The model is then adopted to study the rigid-elastic coupling characteristics of large passenger aircraft under typical pitch and roll maneuvers, as well as the impact characteristics of rigid-elastic coupling on dynamic stability and elastic modes.

Key words: rigid-body mode, elastic mode, rigid-elastic coupling, pitch maneuver, roll maneuver, flight test

CLC Number: