TY - JOUR
T1 - A coupled dynamic loads analysis of satellites with an enhanced Craig–Bampton approach
AU - Lim, Jae Hyuk
AU - Hwang, Do Soon
AU - Kim, Kyoung Won
AU - Lee, Geun Ho
AU - Kim, Jin Gyun
PY - 2017/10/1
Y1 - 2017/10/1
N2 - In this work, we conducted a coupled dynamic loads analysis (CDLA) of satellites with an enhanced Craig–Bampton (ECB) approach to predict maximum response (acceleration, displacement, and stress). The satellite was subjected to a relatively high frequency launch vehicle (LV) interface load (20–50 Hz) when it was launched by multiple satellite launcher or experienced the combustion instability caused by LV instead of a typical low frequency LV interface load (0–10 Hz). To minimize the error caused by mode truncation, ECB-like formulation, which considers the effect of residual modes, is employed and computes the maximum response of the given dynamic system. By using this method, we found that the response by the ECB model is more accurate and efficient over the classical Craig–Bampton (CB) model due to the enhanced transformation matrix from being subjected to an unexpected high frequency LV load. To demonstrate this performance, we solved several benchmark problems associated with CDLA.
AB - In this work, we conducted a coupled dynamic loads analysis (CDLA) of satellites with an enhanced Craig–Bampton (ECB) approach to predict maximum response (acceleration, displacement, and stress). The satellite was subjected to a relatively high frequency launch vehicle (LV) interface load (20–50 Hz) when it was launched by multiple satellite launcher or experienced the combustion instability caused by LV instead of a typical low frequency LV interface load (0–10 Hz). To minimize the error caused by mode truncation, ECB-like formulation, which considers the effect of residual modes, is employed and computes the maximum response of the given dynamic system. By using this method, we found that the response by the ECB model is more accurate and efficient over the classical Craig–Bampton (CB) model due to the enhanced transformation matrix from being subjected to an unexpected high frequency LV load. To demonstrate this performance, we solved several benchmark problems associated with CDLA.
KW - CB (Craig–Bampton)
KW - CDLA (Coupled dynamics loads analysis)
KW - ECB (Enhanced Craig–Bampton)
KW - Model reduction
KW - Structural dynamics
UR - http://www.scopus.com/inward/record.url?scp=85021643519&partnerID=8YFLogxK
U2 - 10.1016/j.ast.2017.06.023
DO - 10.1016/j.ast.2017.06.023
M3 - Article
AN - SCOPUS:85021643519
SN - 1270-9638
VL - 69
SP - 114
EP - 122
JO - Aerospace Science and Technology
JF - Aerospace Science and Technology
ER -