Dynamic simulation of semi-active landing gear system of aircraft using MATLAB-RECURDYN software

https://doi.org/10.31130/ud-jst.2025.048

Abstract: 222 | PDF: 124

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Author

  • Quoc Viet Luong
    Ho Chi Minh City University of Industry and Trade, Vietnam
    Tran Ngoc Nien Nguyen
    Ho Chi Minh City University of Industry and Trade, Vietnam
    Huy Hoang Pham
    Ho Chi Minh City University of Industry and Trade, Vietnam

Keywords:

RECURDYN
MATLAB
dynamic simulation, landing gear system
landing gear shock absorber

Abstract

This article adopts the performance of the semi-active landing gear system for aircraft under FAR standard landing conditions. A six-degree-of-freedom dynamic model of the semi-active landing gear system was developed and integrated with a skyhook controller. To evaluate performance and identify optimal parameters for the controller, co-simulations using RECURDYN-MATLAB software were conducted. The results indicate that, the semi-active system not only enhances vibration damping on the taxi phase but also minimizes adverse impacts during touchdown, thereby improving the safety and stability of the aircraft. Based on these findings, the semi-active landing gear system with a skyhook controller is expected to become a viable alternative to passive systems, not only enhancing landing performance but also contributing to a safer flying experience for passengers.

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Published

May 31, 2025
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How to Cite
Việt, L. Q., N. T. N. Niên, and P. H. Hoàng. “Dynamic Simulation of Semi-Active Landing Gear System of Aircraft Using MATLAB-RECURDYN Software”. The University of Danang - Journal of Science and Technology, vol. 23, no. 5A, May 2025, pp. 32-37, doi:10.31130/ud-jst.2025.048.

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