Dynamic Modeling and Stability Analysis of a Flying Structure undertaking Parametric Excitation Forces

매개변수 가진력을 받아 비행하는 구조물의 동적 모델링 및 안정성 해석

  • Published : 1999.12.01

Abstract

Dynamic stability of a flying structure undertaking constnat and pulsating thrust force is investigated in this paper. The equations of motion of the structure, which is idealized as a free-free beam, are derived by using the hybrid variable method and the assumed mode method. The structural system includes a directional control unit to obtain the directional stability. Unstable regions due to periodically pulsating thrust forces are obtained by using the Floquet's theory. Stability diagrams are presented to illustrate the influence of the constant force, the location of gimbal, and the frequency of pulsating force. The validity of the diagrams are confirmed by direct numerical simulations of the dynamic system.

Keywords

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