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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