Research on the Testbed Framework of Spacecraft

Xu Min Song; Qi Lin; Yong Chen

doi:10.4028/www.scientific.net/AMM.543-547.1955

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 543-547Research on the Testbed Framework of Spacecraft

Research on the Testbed Framework of Spacecraft

Abstract:

Aiming at the characters and requirements of spacecraft design, simulation and test, The test-bed framework was studied in this paper. The framework architecture employ the Data Distribute Service (DDS) to provide communications abstractions and reduce software interface complexity. The time management strategy was studied to keep synchronic of all components. The CAN bus interface was designed to integrate the CAN bus components. The framework will allow rapid-prototyping of high-fidelity simulations of spacecraft during their early project phases, and help reduce the effort, time and expanse to evaluate the performance.

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Periodical:

Applied Mechanics and Materials (Volumes 543-547)

Pages:

1955-1958

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.543-547.1955

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Online since:

March 2014

Authors:

Xu Min Song*, Qi Lin, Yong Chen

Keywords:

CAN Bus, Publish-Subscribe, Test-Bed Framework

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