Dynamic modeling and vibration control of a large flexible space truss

被引:0
作者
Mei Liu
Dengqing Cao
Jipeng Li
Xiaoyun Zhang
Jin Wei
机构
[1] Harbin Institute of Technology,School of Astronautics
[2] Yantai University,School of Electromechanical and Automotive Engineering
来源
Meccanica | 2022年 / 57卷
关键词
Large flexible space truss; Dynamic modeling; Analytical method; Vibration control;
D O I
暂无
中图分类号
学科分类号
摘要
Dynamic equivalent modeling is convenient to the vibration controller design of large space truss structures. Consequently, it is important to study the effectiveness of designed vibration controller of the original truss structures based on the equivalent dynamic models. In this study, the dynamic modeling and vibration control for a large flexible space truss are investigated. The space truss is typical periodic triangular prism structure which consists of beams and rods. Considered the transverse deformation of the whole structure, the equivalent dynamic model of the space truss is established using energy equivalence principle. The fourth-order governing equations of the cantilevered equivalent beam model are derived and solved by adopting the Hamilton principle and the Galerkin method to achieve its discrete dynamic model. To obtain analytical mode shapes of the established equivalent model, an exact analytical approach is exploited for purpose of constructing state space equation of the space truss. Then the validity and accuracy of the equivalent beam model are demonstrated by comparing the natural frequencies and mode shapes with the original space truss finite element model. More importantly, to further design the active vibration controller of the space truss based on the equivalent beam model, the LQR vibration controller is designed when the space truss is subjected to periodic and impulse excitations. The control moment is applied to the full-scale finite element model of the space truss and the numerical simulations prove the effectiveness of the designed LQR vibration controller for the vibration suppression of the space truss. Results indicate that the established equivalent beam model is valid and particularly convenient for the vibration suppression of the large space truss, which can successfully settle the difficulty caused by the high degree of freedom of the finite element model of the large truss to its vibration controller design.
引用
收藏
页码:1017 / 1033
页数:16
相关论文
共 108 条
  • [1] Nakka YK(2019)Nonlinear attitude control of a spacecraft with distributed actuation of solar arrays J Guid Control Dyn 42 458-475
  • [2] Chung S-J(2014)Deploying process modeling and attitude control of a satellite with a large deployable antenna Chin J Aeronaut 27 299-312
  • [3] Allison JT(2017)The low frequency vibration control of the hoop truss structure with extended arm J Low Freq Noise Vibr Active Control 36 294-305
  • [4] Aldrich JB(2015)Dynamic modeling and vibration control of a flexible satellite IEEE Trans Aerosp Electron Syst 51 1422-1431
  • [5] Alvarez-Salazar OS(2018)Simulation-free hyper-reduction for geometrically nonlinear structural dynamics: a quadratic manifold lifting approach J Comput Nonlinear Dynam 13 071003-570
  • [6] Xing Z(2006)Control of the continuum model of a large flexible space structure, ASME Int Mech Eng Congress Expos 2006 561-95
  • [7] Zheng G(2019)Equivalent Timoshenko linear beam model for the static and dynamic analysis of tower buildings Appl Math Model 71 77-1863
  • [8] Ma G(2020)Equivalent dynamic model of the space antenna truss with initial stress AIAA J 58 1851-535
  • [9] Xu M(1982)Trends in large space structure control theory: fondest hopes, wildest dreams IEEE Trans Autom Control 27 522-24
  • [10] Gao B(2015)PD control for vibration attenuation in hoop truss structure based on a novel piezoelectric bending actuator J Sound Vib 339 11-1695