Spacecraft docking simulation using hardware-in-the-loop simulator with stewart platform

Qitao Huang; Hongzhou Jiang; Shangying Zhang; Junwei Han

doi:10.3901/cjme.2005.03.415

Spacecraft docking simulation using hardware-in-the-loop simulator with stewart platform

Qitao Huang, Hongzhou Jiang, Shangying Zhang, Junwei Han

Harbin Institute of Technology

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

30 Scopus citations

Abstract

A ground-based hardware-in-the-loop (HIL) simulation system with hydraulically driven Stewart platform for spacecraft docking simulation is presented. The system is used for simulating docking process of the on-orbit spacecraft. Principle and structure of the six-degree-of-freedom simulation system are introduced. The docking process dynamic of the vehicles is modeled. Experiment results and mathematical simulation data are compared to validating the simulation system. The comparisons of the results prove that the simulation system proposed can effectively simulate the on-orbit docking process of the spacecraft.

Original language	English
Pages (from-to)	415-418
Number of pages	4
Journal	Chinese Journal of Mechanical Engineering (English Edition)
Volume	18
Issue number	3
DOIs	https://doi.org/10.3901/cjme.2005.03.415
State	Published - Sep 2005
Externally published	Yes

Keywords

Dynamic modeling
Hardware-in-the-loop simulation
Spacecraft docking
Stewart platforms

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10.3901/cjme.2005.03.415

Cite this

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abstract = "A ground-based hardware-in-the-loop (HIL) simulation system with hydraulically driven Stewart platform for spacecraft docking simulation is presented. The system is used for simulating docking process of the on-orbit spacecraft. Principle and structure of the six-degree-of-freedom simulation system are introduced. The docking process dynamic of the vehicles is modeled. Experiment results and mathematical simulation data are compared to validating the simulation system. The comparisons of the results prove that the simulation system proposed can effectively simulate the on-orbit docking process of the spacecraft.",

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AU - Zhang, Shangying

AU - Han, Junwei

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N2 - A ground-based hardware-in-the-loop (HIL) simulation system with hydraulically driven Stewart platform for spacecraft docking simulation is presented. The system is used for simulating docking process of the on-orbit spacecraft. Principle and structure of the six-degree-of-freedom simulation system are introduced. The docking process dynamic of the vehicles is modeled. Experiment results and mathematical simulation data are compared to validating the simulation system. The comparisons of the results prove that the simulation system proposed can effectively simulate the on-orbit docking process of the spacecraft.

AB - A ground-based hardware-in-the-loop (HIL) simulation system with hydraulically driven Stewart platform for spacecraft docking simulation is presented. The system is used for simulating docking process of the on-orbit spacecraft. Principle and structure of the six-degree-of-freedom simulation system are introduced. The docking process dynamic of the vehicles is modeled. Experiment results and mathematical simulation data are compared to validating the simulation system. The comparisons of the results prove that the simulation system proposed can effectively simulate the on-orbit docking process of the spacecraft.

KW - Dynamic modeling

KW - Hardware-in-the-loop simulation

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KW - Stewart platforms

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Spacecraft docking simulation using hardware-in-the-loop simulator with stewart platform

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Keywords

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