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A prediction method for the dynamic environment of spacecraft based on the component mode synthesis
W. Yang,
L. Liu
, W. L. Dong
宇航学院
Beijing Institute of Technology
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Engineering
Structural Dynamics
100%
Auxiliary Equipment
100%
Computer Simulation
50%
Dynamic Models
50%
Degree of Freedom
50%
Finite Element Method
50%
Synthesis Method
50%
Major Problem
50%
Reliability Assessment
50%
Prediction Technology
50%
Material Science
Spacecraft
100%
Structural Dynamics
28%
Finite Element Method
14%
Modal Testing
14%