Title :
Analysis method about vibration Influence of transfer alignment based on finite element and aerodynamic models
Author :
Li, Fu ; Zhongming, Chen ; Qi, Wang ; Shining, Feng ; Jin, Xu
Author_Institution :
Shenyang Aerosp. Univ., Shenyang, China
Abstract :
In order to meet the need of modern war, rapid and accurate initial-alignment has become one of key technologies in the field of inertial technology. Finite element model and unsteady aerodynamics model of the whole machine structure is constructed in this paper. The sin gust disturbance is added under some flight condition, the writer elucidates vibration Influence for the transfer alignment about the dynamic interference source influence through the time-domain response analysis of the master and sub-inertial navigation.
Keywords :
aerodynamics; finite element analysis; military aircraft; navigation; vibrations; aerodynamic models; dynamic interference; finite element models; flight condition; inertial technology; machine structure; master navigation; sin gust disturbance; subinertial navigation; time-domain response analysis; transfer alignment vibration influence; unsteady aerodynamics model; war; Aerodynamics; Analytical models; Atmospheric modeling; Finite element methods; Inertial navigation; Load modeling; Mathematical model; Aerodynamics; Inertial navigation system; Structure finite element; Transfer alignment;
Conference_Titel :
Control and Decision Conference (CCDC), 2012 24th Chinese
Conference_Location :
Taiyuan
Print_ISBN :
978-1-4577-2073-4
DOI :
10.1109/CCDC.2012.6244309
