Lin Jin-yong, Zhang Shuo, Liu Jing-jing, Dong Wen-jie, Zhou Chun-mei
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引用次数: 2
Abstract
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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