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Hard-landing Simulation by a Hierarchical Aircraft Landing Model and an Extended Inertia Relief Technique

Lee, Kyu Beom;Jeong, Seon Ho;Cho, Jin Yeon;Kim, Jeong Ho;Park, Chan Yik

  • 투고 : 2015.02.11
  • 심사 : 2015.09.14
  • 발행 : 2015.09.30

초록

In this work, an efficient aircraft landing simulation strategy is proposed to develop an efficient and reliable hard-landing monitoring procedure. Landing stage is the most dangerous moment during operation cycle of aircraft and it may cause structural damage when hard-landing occurs. Therefore, the occurrence of hard-landing should be reported accurately to guarantee the structural integrity of aircraft. In order to accurately determine whether hard-landing occurs or not from given landing conditions, full nonlinear structural dynamic simulation can be performed, but this approach is highly time-consuming. Thus, a more efficient approach for aircraft landing simulation which uses a hierarchical aircraft landing model and an extended inertia relief technique is proposed. The proposed aircraft landing model is composed of a multi-body dynamics model equipped with landing gear and tire models to extract the impact force and inertia force at touch-down and a linear dynamic structural model with an extended inertia relief method to analyze the structural response subject to the prescribed rigid body motion and the forces extracted from the multi-body dynamics model. The numerical examples show the efficiency and practical advantages of the proposed landing model as an essential component of aircraft hard-landing monitoring procedure.

키워드

Structural integrity;Hard-landing monitoring;Landing simulation;Inertia relief

참고문헌

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피인용 문헌

  1. Topology Optimization Application for Initial Platform Design of 10 MW Grade Floating Type Wave-wind Hybrid Power Generation System vol.19, pp.3, 2016, https://doi.org/10.5139/IJASS.2015.16.3.394
  2. Modified Inertia Relief Method Based on Accurate Inertia Loads vol.55, pp.8, 2017, https://doi.org/10.5139/IJASS.2015.16.3.394