Dynamics of 3D Timoshenko gyroelastic beams with large attitude changes for the gyros

被引:21
作者
Hassanpour, Soroosh [1 ]
Heppler, G. R. [1 ]
机构
[1] Univ Waterloo, Syst Design Engn, Waterloo, ON N2L 3G1, Canada
基金
加拿大自然科学与工程研究理事会;
关键词
Gyroelastic beam; Timoshenko beam; Control moment gyros; Stored angular momentum; Vibration control; Curve veering; SPACE STRUCTURES; MODAL-ANALYSIS; STABILITY;
D O I
10.1016/j.actaastro.2015.09.012
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This work is concerned with the theoretical development of dynamic equations for undamped gyroelastic beams which are dynamic systems with continuous inertia, elasticity, and gyricity. Assuming unrestricted or large attitude changes for the axes of the gyros and utilizing generalized Hooke's law, Duleau torsion theory, and Timoshenko bending theory, the energy expressions and equations of motion for the gyroelastic beams in three-dimensional space are derived. The so-obtained comprehensive gyroelastic beam model is compared against earlier gyroelastic beam models developed using Euler-Bernoulli beam models and is used to study the dynamics of gyroelastic beams through numerical examples. It is shown that there are significant differences between the developed unrestricted Timoshenko gyroelastic beam model and the previously derived zero-order restricted Euler-Bernoulli gyroelastic beam models. These differences are more pronounced in the short beam and transverse gyricity cases. (C) 2015 IAA. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:33 / 48
页数:16
相关论文
共 43 条
[1]  
[Anonymous], P ASME 2014 INT DES
[2]  
[Anonymous], THESIS
[3]  
[Anonymous], CONTINUUM MECH
[4]  
Aubrun J., 1979, 159171 NASA
[5]  
Bathe KJ., 1996, Finite element procedures
[6]   Optimal Gyricity Distribution for Space Structure Vibration Control [J].
Chee, Stephen A. ;
Damaren, Christopher J. .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2015, 38 (07) :1218-1228
[7]   ATTITUDE STABILITY OF A DUAL-SPIN SATELLITE WITH A LARGE FLEXIBLE SOLAR ARRAY [J].
CHERCHAS, DB ;
HUGHES, PC .
JOURNAL OF SPACECRAFT AND ROCKETS, 1973, 10 (02) :126-132
[8]  
D'Eleuterio G., 1985, 26 AIAA ASME ASCE AH, P384
[9]  
D'Eleuterio G., 1986, 300 U TOR I AER STUD
[10]  
Damaren C., 1987, THESIS