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Coupled Vibration Analysis of the Spacecraft with the Flexible Shaft and Solar Panels Assembly

https://doi.org/10.2139/ssrn.4677640
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inferredcites →https://doi.org/10.1007/s00419-016-1155-3openalex-extracted
Studies on global analytical mode for a three-axis attitude stabilized spacecraft by using the Rayleigh–Ritz method
inferredcites →https://doi.org/10.1007/s00419-018-1358-xopenalex-extracted
Dynamics of a multi-beam structure connected with nonlinear joints: modelling and simulation
inferredcites →https://doi.org/10.1016/j.actaastro.2018.10.024openalex-extracted
Thermal-structural analysis for flexible spacecraft with single or double solar panels: A comparison study
inferredcites →https://doi.org/10.1016/j.actaastro.2022.01.038openalex-extracted
Vibration characteristics analysis of rigid-flexible spacecraft with double-direction hinged solar arrays
inferredcites →https://doi.org/10.1016/j.actaastro.2023.03.043openalex-extracted
Nonlinear attitude maneuvering of a flexible spacecraft for space debris tracking and collision avoidance
inferredcites →https://doi.org/10.1016/j.apm.2016.06.005openalex-extracted
A unified solution for free in-plane vibration of orthotropic circular, annular and sector plates with general boundary conditions
inferredcites →https://doi.org/10.1016/j.apm.2018.07.058openalex-extracted
Dynamical modeling and attitude analysis for the spacecraft with lateral solar arrays
inferredcites →https://doi.org/10.1016/j.apm.2020.10.044openalex-extracted
Study on analytical global modes for a multi-panel structure connected with flexible hinges
inferredcites →https://doi.org/10.1016/j.apm.2022.03.047openalex-extracted
An isogeometric boundary element method for heat transfer problems of multiscale structures in electronic packaging with arbitrary heat sources
inferredcites →https://doi.org/10.1016/j.apm.2022.08.026openalex-extracted
Study on the coupled dynamics of rigid-liquid-flexible spacecraft by using isogeometric analysis for liquid sloshing
inferredcites →https://doi.org/10.1016/j.asr.2021.10.057openalex-extracted
Rigid-flexible coupling identification and attitude control based on deep neural networks
inferredcites →https://doi.org/10.1016/j.ast.2020.105875openalex-extracted
Dynamic modeling and vibration control of a coupled rigid-flexible high-order structural system: A comparative study
inferredcites →https://doi.org/10.1016/j.ast.2022.107641openalex-extracted
Rigid-flexible coupling dynamic modeling and analysis of dumbbell-shaped spacecraft
inferredcites →https://doi.org/10.1016/j.ast.2022.107750openalex-extracted
Distributed cooperative control for vibration suppression of a flexible satellite
inferredcites →https://doi.org/10.1016/j.ast.2022.107952openalex-extracted
Parametric control for flexible spacecraft attitude maneuver based on disturbance observer
inferredcites →https://doi.org/10.1016/j.ast.2023.108499openalex-extracted
Dynamic modeling and control of a solar sail considering large-amplitude nonlinear vibration
inferredcites →https://doi.org/10.1016/j.compstruc.2014.09.008openalex-extracted
Proof of convergence for a set of admissible functions for the Rayleigh–Ritz analysis of beams and plates and shells of rectangular planform
inferredcites →https://doi.org/10.1016/j.compstruct.2019.111549openalex-extracted
A unified Fourier series solution for vibration analysis of FG-CNTRC cylindrical, conical shells and annular plates with arbitrary boundary conditions
inferredcites →https://doi.org/10.1016/j.compstruct.2020.112765openalex-extracted
Free vibration and buckling behavior of functionally graded porous plates reinforced by graphene platelets using spectral Chebyshev approach
inferredcites →https://doi.org/10.1016/j.compstruct.2021.114138openalex-extracted
In-plane modal studies of arbitrary laminated triangular plates with elastic boundary constraints by the Chebyshev-Ritz approach
inferredcites →https://doi.org/10.1016/j.compstruct.2021.114355openalex-extracted
Analysis of layered panels with mixed edge boundary conditions using state space differential quadrature method
inferredcites →https://doi.org/10.1016/j.euromechsol.2019.04.014openalex-extracted
New analytic buckling solutions of rectangular thin plates with two free adjacent edges by the symplectic superposition method
inferredcites →https://doi.org/10.1016/j.ijmecsci.2013.08.003openalex-extracted
A unified approach for the vibration analysis of moderately thick composite laminated cylindrical shells with arbitrary boundary conditions
inferredcites →https://doi.org/10.1016/j.ijmecsci.2020.106051openalex-extracted
New analytic buckling solutions of side-cracked rectangular thin plates by the symplectic superposition method
inferredcites →https://doi.org/10.1016/j.ijnonlinmec.2022.104037openalex-extracted
Nonlinear vibration analysis of CNT-reinforced functionally graded composite cylindrical shells resting on elastic foundations
inferredcites →https://doi.org/10.1016/j.istruc.2021.06.056openalex-extracted
Thin rectangular plates under axial point loading: Accuracy of the classical single Fourier series solution for stresses
inferredcites →https://doi.org/10.1016/j.jsv.2012.03.027openalex-extracted
Vibration analysis of functionally graded annular plates with mixed boundary conditions in thermal environment
inferredcites →https://doi.org/10.1016/j.jsv.2019.115001openalex-extracted
Forced vibration analysis of Timoshenko double-beam system under compressive axial load by means of Green's functions
inferredcites →https://doi.org/10.1016/j.jsv.2020.115809openalex-extracted
Modelling and vibration analysis for the multi-plate structure connected by nonlinear hinges
inferredcites →https://doi.org/10.1016/j.jsv.2021.116020openalex-extracted
Local nonlinear stores induce global modal interactions in the steady-state dynamics of a model airplane
inferredcites →https://doi.org/10.1016/j.taml.2021.100293openalex-extracted
On the symplectic superposition method for free vibration of rectangular thin plates with mixed boundary constraints on an edge
inferredcites →https://doi.org/10.1016/j.tws.2015.01.020openalex-extracted
Forced vibration analysis of arbitrarily constrained rectangular plates and stiffened panels using the assumed mode method
inferredcites →https://doi.org/10.1016/j.tws.2021.107926openalex-extracted
A novel nonlinear finite element method for structural dynamic modeling of spacecraft under large deformation
inferredcites →https://doi.org/10.1016/j.ymssp.2019.05.034openalex-extracted
Semi-active vibration control of two flexible plates using an innovative joint mechanism
inferredcites →https://doi.org/10.1016/j.ymssp.2021.108083openalex-extracted
Dynamic modeling and orbit maneuvering response analysis for a three-axis attitude stabilized large scale flexible spacecraft installed with hinged solar arrays
inferredcites →https://doi.org/10.1061/(asce)as.1943-5525.0001133openalex-extracted
Natural Frequencies and Global Mode Functions for Flexible Jointed-Panel Structures
inferredcites →https://doi.org/10.1115/1.1827250openalex-extracted
Three-Dimensional Vibration Analysis of Rectangular Plates With Mixed Boundary Conditions
inferredcites →https://doi.org/10.1142/s175882512150112xopenalex-extracted
Rigid-Flexible Coupled Dynamics and PD-Robust Control Design for the Spacecraft with Rotating Solar Panels
inferredcites →https://doi.org/10.3390/act12010003openalex-extracted
Natural Characteristics Analysis for the Spacecraft Equipped with Constructed Cantilever Solar Panels
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