Parametric study for dynamics of spacecraft with local nonlinearities

AIAA Journal

Volumn 48, Issue 8, 2010, Pages 1700-1707

  Wei, F ^a,c   Liang, L ^b,d   Zheng, G T ^b,d  

^a HARBIN INSTITUTE OF TECHNOLOGY   (China)

^b TSINGHUA UNIVERSITY   (China)

^c Department of Space Engineering and Applied Mechanics ^*  (United States)

^d Center for Advanced Materials Technology (CAMT)   (Australia)

Author keywords

[No Author keywords available]

Indexed keywords

DEGREES OF FREEDOM; DESIGN CONSIDERATIONS; DIRECT METHOD; DYNAMIC CHARACTERISTICS; EXCITATION LEVELS; FINITE-ELEMENT MODELS; HARMONIC RESPONSE; LARGE-SCALE STRUCTURE; NON-LINEAR PARAMETERS; NON-LINEARITY; PARAMETRIC STUDY; PHYSICAL PARAMETERS; RECEPTANCE;

COMPUTATIONAL EFFICIENCY; DYNAMIC ANALYSIS; MECHANICS; SPACECRAFT;

FINITE ELEMENT METHOD;

EID: 77956381409     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.J050145     Document Type: Article

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