一种模块化微小型卫星对接机构建模仿真

Xiao Tian Zhang; Ning Bo He; Rui Qing Wang; Wen Long Wang

doi:10.3873/j.issn.1000-1328.2018.04.002

一种模块化微小型卫星对接机构建模仿真

Translated title of the contribution: Modeling and Simulation of a Modular Satellite Docking Mechanism

Xiao Tian Zhang^*
, Ning Bo He
, Rui Qing Wang
, Wen Long Wang

^*Corresponding author for this work

School of Astronautics

Research output: Contribution to journal › Article › peer-review

6 Scopus citations

Abstract

With the focus on docking and separation technology for on-orbit servicing, a novel docking mechanism designed for a modular satellite offers a highly effective approach for on-orbit satellite servicing and assembly. This paper introduces its mechanism and describes the kinematic equation of the mechanism. The numerical simulation results given by MATLAB demonstrate that the kinematic equation deduced is rational. According to the equation, the potential interference issue of the mechanism is analyzed and the noninterference moving condition is also given. The modeling and simulation methods proposed can be referenced for further study in designing and manufacturing other modular satellite docking mechanisms.

Translated title of the contribution	Modeling and Simulation of a Modular Satellite Docking Mechanism
Original language	Chinese (Traditional)
Pages (from-to)	368-375
Number of pages	8
Journal	Yuhang Xuebao/Journal of Astronautics
Volume	39
Issue number	4
DOIs	https://doi.org/10.3873/j.issn.1000-1328.2018.04.002
State	Published - 28 Apr 2018

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title = "一种模块化微小型卫星对接机构建模仿真",

abstract = "With the focus on docking and separation technology for on-orbit servicing, a novel docking mechanism designed for a modular satellite offers a highly effective approach for on-orbit satellite servicing and assembly. This paper introduces its mechanism and describes the kinematic equation of the mechanism. The numerical simulation results given by MATLAB demonstrate that the kinematic equation deduced is rational. According to the equation, the potential interference issue of the mechanism is analyzed and the noninterference moving condition is also given. The modeling and simulation methods proposed can be referenced for further study in designing and manufacturing other modular satellite docking mechanisms.",

keywords = "Docking mechanism, Kinematical modeling, Modular satellite, Numerical simulation, On-orbit servicing",

author = "Zhang, \{Xiao Tian\} and He, \{Ning Bo\} and Wang, \{Rui Qing\} and Wang, \{Wen Long\}",

year = "2018",

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doi = "10.3873/j.issn.1000-1328.2018.04.002",

language = "繁体中文",

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T1 - 一种模块化微小型卫星对接机构建模仿真

AU - Zhang, Xiao Tian

AU - He, Ning Bo

AU - Wang, Rui Qing

AU - Wang, Wen Long

PY - 2018/4/28

Y1 - 2018/4/28

N2 - With the focus on docking and separation technology for on-orbit servicing, a novel docking mechanism designed for a modular satellite offers a highly effective approach for on-orbit satellite servicing and assembly. This paper introduces its mechanism and describes the kinematic equation of the mechanism. The numerical simulation results given by MATLAB demonstrate that the kinematic equation deduced is rational. According to the equation, the potential interference issue of the mechanism is analyzed and the noninterference moving condition is also given. The modeling and simulation methods proposed can be referenced for further study in designing and manufacturing other modular satellite docking mechanisms.

AB - With the focus on docking and separation technology for on-orbit servicing, a novel docking mechanism designed for a modular satellite offers a highly effective approach for on-orbit satellite servicing and assembly. This paper introduces its mechanism and describes the kinematic equation of the mechanism. The numerical simulation results given by MATLAB demonstrate that the kinematic equation deduced is rational. According to the equation, the potential interference issue of the mechanism is analyzed and the noninterference moving condition is also given. The modeling and simulation methods proposed can be referenced for further study in designing and manufacturing other modular satellite docking mechanisms.

KW - Docking mechanism

KW - Kinematical modeling

KW - Modular satellite

KW - Numerical simulation

KW - On-orbit servicing

UR - https://www.scopus.com/pages/publications/85051371289

U2 - 10.3873/j.issn.1000-1328.2018.04.002

DO - 10.3873/j.issn.1000-1328.2018.04.002

M3 - 文章

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SN - 1000-1328

VL - 39

SP - 368

EP - 375

JO - Yuhang Xuebao/Journal of Astronautics

JF - Yuhang Xuebao/Journal of Astronautics

IS - 4

ER -

一种模块化微小型卫星对接机构建模仿真

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