3-D modeling and finite elements analysis of KM6 motion simulator

Q. S. Xiao; J. W. Zhang; G. F. Wang; Z. H. Du; H. Fang

doi:10.1088/1757-899X/504/1/012072

3-D modeling and finite elements analysis of KM6 motion simulator

Q. S. Xiao^*
, J. W. Zhang
, G. F. Wang
, Z. H. Du
, H. Fang

^*Corresponding author for this work

School of Materials Science and Engineering

Research output: Contribution to journal › Conference article › peer-review

Abstract

As an important part of the satellite space sport simulation system of the KM6 manned spacecraft space environmental test equipment, the satellite motion simulator has the function of simulating and testing the satellites on the ground. In this paper, the 3-D model of the motion simulator is established, and its performance is analysed using finite elements simulation software under different conditions. Under the different conditions of static force and dynamics, the simulation results of the vertical state of the spin axis and tilted 30 state of the spin axis are compared and the optimal working conditions is designed. Modal analysis and buckling analysis are performed to prove that the design of the structure is feasible.

Original language	English
Article number	012072
Journal	IOP Conference Series: Materials Science and Engineering
Volume	504
Issue number	1
DOIs	https://doi.org/10.1088/1757-899X/504/1/012072
State	Published - 26 Apr 2019
Event	2nd International Workshop on Materials Science and Mechanical Engineering, IWMSME 2018 - Qingdao, China Duration: 26 Oct 2018 → 28 Oct 2018

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10.1088/1757-899X/504/1/012072

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title = "3-D modeling and finite elements analysis of KM6 motion simulator",

abstract = "As an important part of the satellite space sport simulation system of the KM6 manned spacecraft space environmental test equipment, the satellite motion simulator has the function of simulating and testing the satellites on the ground. In this paper, the 3-D model of the motion simulator is established, and its performance is analysed using finite elements simulation software under different conditions. Under the different conditions of static force and dynamics, the simulation results of the vertical state of the spin axis and tilted 30 state of the spin axis are compared and the optimal working conditions is designed. Modal analysis and buckling analysis are performed to prove that the design of the structure is feasible.",

author = "Xiao, \{Q. S.\} and Zhang, \{J. W.\} and Wang, \{G. F.\} and Du, \{Z. H.\} and H. Fang",

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T1 - 3-D modeling and finite elements analysis of KM6 motion simulator

AU - Xiao, Q. S.

AU - Zhang, J. W.

AU - Wang, G. F.

AU - Du, Z. H.

AU - Fang, H.

N1 - Publisher Copyright: © Published under licence by IOP Publishing Ltd.

PY - 2019/4/26

Y1 - 2019/4/26

N2 - As an important part of the satellite space sport simulation system of the KM6 manned spacecraft space environmental test equipment, the satellite motion simulator has the function of simulating and testing the satellites on the ground. In this paper, the 3-D model of the motion simulator is established, and its performance is analysed using finite elements simulation software under different conditions. Under the different conditions of static force and dynamics, the simulation results of the vertical state of the spin axis and tilted 30 state of the spin axis are compared and the optimal working conditions is designed. Modal analysis and buckling analysis are performed to prove that the design of the structure is feasible.

AB - As an important part of the satellite space sport simulation system of the KM6 manned spacecraft space environmental test equipment, the satellite motion simulator has the function of simulating and testing the satellites on the ground. In this paper, the 3-D model of the motion simulator is established, and its performance is analysed using finite elements simulation software under different conditions. Under the different conditions of static force and dynamics, the simulation results of the vertical state of the spin axis and tilted 30 state of the spin axis are compared and the optimal working conditions is designed. Modal analysis and buckling analysis are performed to prove that the design of the structure is feasible.

UR - https://www.scopus.com/pages/publications/85065557540

U2 - 10.1088/1757-899X/504/1/012072

DO - 10.1088/1757-899X/504/1/012072

M3 - 会议文章

AN - SCOPUS:85065557540

SN - 1757-8981

VL - 504

JO - IOP Conference Series: Materials Science and Engineering

JF - IOP Conference Series: Materials Science and Engineering

IS - 1

M1 - 012072

T2 - 2nd International Workshop on Materials Science and Mechanical Engineering, IWMSME 2018

Y2 - 26 October 2018 through 28 October 2018

ER -

3-D modeling and finite elements analysis of KM6 motion simulator

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