講演抄録/キーワード |
講演名 |
2013-12-03 09:30
Random vibration analysis of the F-2 nanosatellite structure ○Thuong Nguyen Van・Hung Nguyen Viet・Khanh Nguyen Phu・Tuan Le Anh(HUST) SANE2013-95 |
抄録 |
(和) |
A random vibration analysis of a Nanosatellite structure in the launch phase is presented in this paper. The objective of this study is to assure the structural integrity of the components in order to survive the launching loads. The structural dynamics analysis was performed using ANSYS software for a finite element model of the chosen satellite. The Finite Element Analysis (FEA) showed the resistance of the satellite components during the launch. These FEA results are important for the satellite structure design team to check the design and make the necessary changes before the physical vibration testing. |
(英) |
A random vibration analysis of a Nanosatellite structure in the launch phase is presented in this paper. The objective of this study is to assure the structural integrity of the components in order to survive the launching loads. The structural dynamics analysis was performed using ANSYS software for a finite element model of the chosen satellite. The Finite Element Analysis (FEA) showed the resistance of the satellite components during the launch. These FEA results are important for the satellite structure design team to check the design and make the necessary changes before the physical vibration testing. |
キーワード |
(和) |
random vibration / structure / ANSYS / nanosatellite / FEA / / / |
(英) |
random vibration / structure / ANSYS / nanosatellite / FEA / / / |
文献情報 |
信学技報, vol. 113, no. 335, SANE2013-95, pp. 139-144, 2013年12月. |
資料番号 |
SANE2013-95 |
発行日 |
2013-11-25 (SANE) |
ISSN |
Print edition: ISSN 0913-5685 Online edition: ISSN 2432-6380 |
著作権に ついて |
技術研究報告に掲載された論文の著作権は電子情報通信学会に帰属します.(許諾番号:10GA0019/12GB0052/13GB0056/17GB0034/18GB0034) |
PDFダウンロード |
SANE2013-95 |