航天运载火箭即插即用控制系统体系结构研究

2013 Third International Conference on Instrumentation, Measurement, Computer, Communication and Control Pub Date : 2013-09-21 DOI:10.1109/IMCCC.2013.332

Lin Jin-yong, Zhang Shuo, Liu Jing-jing, Dong Wen-jie, Zhou Chun-mei

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引用次数: 2

摘要

针对响应式航天运载火箭控制系统快速集成的发展要求，提出了一种即插即用/PnP控制系统体系结构，给出了航天运载火箭即插即用控制系统的通用模型和标准化通信机制。然后进行了原理验证实验。试验结果表明，上述PnP结构是可用的，将支持未来航天运载火箭提升响应能力。

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Study on the Architecture of Plug-and-Play Control System for Aerospace Launch Vehicle

Aiming at the developing requirements on rapid integration of control system for responsive aerospace launch vehicle, this paper put forward a kind of architecture of plug-and-play/PnP control system, and presents the generic model of plug-and-play control system for aerospace launch vehicle and the standardization communication machenism. Then the principle validation experiment is carried through. The test result shows that the above PnP architecture is usable and will support the future aerospace launch vehicle for upgrading the responsive ability.

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来源期刊

2013 Third International Conference on Instrumentation, Measurement, Computer, Communication and Control

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