Numerical and experimental investigation on dynamics of deployable space telescope experiencing deployment and attitude adjustment motions coupled with laminated composite shell

Nonlinear dynamic modeling methods for a flower-like clustered deployable space telescope (DST) with laminated composite material experiencing large deployment and attitude adjustment motions is pr...

[2]  Dong Liang,et al.  Numerical and experimental investigation on nonlinear dynamic behavior of satellite antenna reflector mechanism considering geometrical nonlinear effect and laminated composite material , 2018, Proceedings of the Institution of Mechanical Engineers, Part K: Journal of Multi-body Dynamics.

[3]  Ik-Hyeon Choi,et al.  Geometrically nonlinear transient analysis of composite laminated plate and shells subjected to low-velocity impact , 2016 .

[4]  Wesley A. Traub,et al.  Advanced Technology Large-Aperture Space Telescope: science drivers and technology developments , 2012 .

[5]  Ayman A. Nada,et al.  Absolute nodal coordinate formulation of large-deformation piezoelectric laminated plates , 2012 .

[6]  Yang Zhao,et al.  Nonlinear analysis and vibration suppression control for a rigid–flexible coupling satellite antenna system composed of laminated shell reflector , 2014 .

[7]  Wan-Suk Yoo,et al.  A New Thin Spatial Beam Element Using the Absolute Nodal Coordinates: Application to a Rotating Strip , 2005 .

[8]  Yangsheng Xu,et al.  Dynamics modeling and analysis of a flexible-base space robot for capturing large flexible spacecraft , 2014 .

[9]  J. N. Reddy,et al.  A higher-order shear deformation theory of laminated elastic shells , 1985 .

[10]  Aki Mikkola,et al.  A study of moderately thick quadrilateral plate elements based on the absolute nodal coordinate formulation , 2013, Multibody System Dynamics.

[11]  Keqi Pan,et al.  Rigid-flexible-thermal coupling dynamic formulation for satellite and plate multibody system , 2016 .

[12]  Johannes Gerstmayr,et al.  Analysis of Stress and Strain in the Absolute Nodal Coordinate Formulation , 2006 .

[13]  Wei Zhang,et al.  Multi-pulse orbits dynamics of composite laminated piezoelectric rectangular plate , 2011 .

[14]  Jin Duan,et al.  THERMAL–DYNAMIC COUPLING ANALYSIS OF LARGE SPACE STRUCTURES CONSIDERING GEOMETRIC NONLINEARITY , 2008 .

[15]  Ahmed A. Shabana.  Effect of using composites on the dynamic response of multi-body systems , 1986 .

[16]  Ahmed A. Shabana,et al.  Flexible Multibody Dynamics: Review of Past and Recent Developments , 1997 .

[17]  Aouni A. Lakis,et al.  GENERAL EQUATIONS OF ANISOTROPIC PLATES AND SHELLS INCLUDING TRANSVERSE SHEAR DEFORMATIONS, ROTARY INERTIA AND INITIAL CURVATURE EFFECTS , 2000 .

[18]  Xiao-Feng Liu,et al.  Deployment and control of flexible solar array system considering joint friction , 2017 .

[19]  Qiang Tian,et al.  Modal Analysis of a Rotating Thin Plate via Absolute Nodal Coordinate Formulation , 2011 .

[20]  Xiao-Feng Liu,et al.  Deployment dynamics and control of large-scale flexible solar array system with deployable mast , 2016 .