Funder
China Scholarship Council
National Natural Science Foundation of China
Publisher
Springer Science and Business Media LLC
Subject
Electrical and Electronic Engineering,Applied Mathematics,Mechanical Engineering,Ocean Engineering,Aerospace Engineering,Control and Systems Engineering
Reference26 articles.
1. Ji, H.R., Li, D.X.: A novel nonlinear finite element method for structural dynamic modeling of spacecraft under large deformation. Thin-Walled Struct. 165, 107926 (2021)
2. Zhang, X.Y., Zong, Q., Dou, L.Q., Tian, B.L., Liu, W.J.: Finite-time attitude maneuvering and vibration suppression of flexible spacecraft. J. Frank. Inst. 357, 11604–11628 (2020)
3. Liu, L., Cao, D.Q., Wei, J.: Rigid-flexible coupling dynamic modeling and vibration control for flexible spacecraft based on its global analytical modes. Sci. China Technol. Sci. 62, 608–618 (2019)
4. Azimi, M., Shahravi, M., Fard, K.M.: Modeling and vibration suppression of flexible spacecraft using higher-order sandwich panel theory. Int. J. Acoust. Vib. 22(2), 1–14 (2017)
5. Shahravi, M., Azimi, M.: Attitude and vibration control of flexible spacecraft using singular perturbation approach. ISRN Aerospace Eng. 2014, 1 (2014)
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