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NTIS 바로가기International journal of aeronautical and space sciences, v.17 no.4, 2016년, pp.476 - 490
Kim, Yongha (Graduate School of Aerospace and Mechanical Engineering, Korea Aerospace University) , Kim, Myungjun (Graduate School of Aerospace and Mechanical Engineering, Korea Aerospace University) , Kim, Pyeunghwa (Graduate School of Aerospace and Mechanical Engineering, Korea Aerospace University) , Kim, Hwiyeop (Graduate School of Aerospace and Mechanical Engineering, Korea Aerospace University) , Park, Jungsun (Department of Aerospace and Mechanical Engineering, Korea Aerospace University) , Roh, Jin-Ho (Department of Aerospace and Mechanical Engineering, Korea Aerospace University) , Bae, Jaesung (Department of Aerospace and Mechanical Engineering, Korea Aerospace University)
This paper defines mode shape function of a composite solar panel assumed as Kirchhoff-Love plate for considering a torsional mode of composite solar panel. It then goes on to define dynamic model of a high-agility satellite considering the flexibility of composite solar panel as well as stiffness o...
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