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An IDRA approach for modeling helicopter based on Lagrange dynamics

Author

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  • Li, Yingjie
  • Zhao, Dingxuan
  • Zhang, Zhongjun
  • Liu, Jingang

Abstract

In order to accelerate the algorithm speed of dynamic model of helicopter, an IDRA approach for modeling helicopter was proposed and a dynamic model of six degrees of freedom (6 DOF) combining flying and landing was established in this paper. As the dynamic model is derived from the Lagrange equation of a non-conservative system, treating micro displacements and rotating angles of airframe in a simulation step as generalized coordinates, the relationship between energy dissipation, kinetic energy, potential energy and the generalized coordinates was analyzed. Finally, the reliability of this method and real-time of dynamic model were verified on the experimental platform of helicopter flight simulator, which could provide reliable theoretical foundation for solving the retardance of data transfer of helicopter simulator.

Suggested Citation

  • Li, Yingjie & Zhao, Dingxuan & Zhang, Zhongjun & Liu, Jingang, 2015. "An IDRA approach for modeling helicopter based on Lagrange dynamics," Applied Mathematics and Computation, Elsevier, vol. 265(C), pages 733-747.
    • Handle: RePEc:eee:apmaco:v:265:y:2015:i:c:p:733-747
    DOI: 10.1016/j.amc.2015.05.111
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    References listed on IDEAS

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    1. Gomes, Jose O. & Woods, David D. & Carvalho, Paulo V.R. & Huber, Gilbert J. & Borges, Marcos R.S., 2009. "Resilience and brittleness in the offshore helicopter transportation system: The identification of constraints and sacrifice decisions in pilots’ work," Reliability Engineering and System Safety, Elsevier, vol. 94(2), pages 311-319.
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    Cited by:

    1. Nguyen Xuan-Mung & Mehdi Golestani, 2022. "Smooth, Singularity-Free, Finite-Time Tracking Control for Euler–Lagrange Systems," Mathematics, MDPI, vol. 10(20), pages 1-18, October.
    2. Yin, Zeyang & Luo, Jianjun & Wei, Caisheng, 2019. "Quasi fixed-time fault-tolerant control for nonlinear mechanical systems with enhanced performance," Applied Mathematics and Computation, Elsevier, vol. 352(C), pages 157-173.

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