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Research on optimization method of spacecraft stiffness bas..:

, In: 1st International Conference on Mechanical System Dynamics (ICMSD 2022),

Zhang, X. ; Tan, Z. ; Wang, .H... - p. None , 2022

Link: https://doi.org/10.1049/icp.2022.1711

RT 
T1 <cTitle>1st International Conference on Mechanical System Dynamics (ICMSD 2022)</cTitle>: T1 <Title>Research on optimization method of spacecraft stiffness based on variable section Timoshenko beam</Title>

UL https://suche.suub.uni-bremen.de/peid=ieee-9997285&Exemplar=1&LAN=DE
				
A1 Zhang, X.
A1 Tan, Z.
A1 Wang, .H
A1 Ren, X.
A1 Zhang, Q.
A1 Lin, H.
A1 Peng, H.
A1 Mao, Y.
YR 2022
K1 beams (structures)
K1 buckling
K1 elastic constants
K1 finite element analysis
K1 mechanical stability
K1 particle swarm optimisation
K1 shells (structures)
K1 thin wall structures
K1 optimization method
K1 spacecraft stiffness
K1 variable section timoshenko beam
K1 truncated conical structures
K1 main load support segments
K1 spacecrafts
K1 rockets
K1 upper stage
K1 fundamental frequencies
K1 structure weight
K1 cylindrical structures
K1 stiffness matrix
K1 truncated conical structure
K1 cross section geometries
K1 variable cross section
K1 thin-walled truncated cone
K1 thin-walled cylinders
K1 truncated cones
K1 mass matrix
K1 preceding frequency-calculation method
K1 variable-cross-section Timoshenko beam theory
K1 optimization process
K1 geometrical parameters including thickness
K1 cylindrical parts
K1 truncated conical parts
K1 structural weight
K1 optimal thicknesses
K1 structural prototype design
SP None
LK http://dx.doi.org/https://doi.org/10.1049/icp.2022.1711
DO https://doi.org/10.1049/icp.2022.1711
SF ELIB - SuUB Bremen

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