标题:Design of unmanned aerial vehicle (UAV) flight control system based on DSP and adaptive control theory
作者:Liu, Pengfei ;Li, Zhihao ;Cui, Chen
作者机构:[Liu, Pengfei ] School of Mechanical and Automotive Engineering, South China University of Technology, Taishan, Guangdong, China;[Cui, Chen ] Institut 更多
会议名称:2016 International Conference on Communication and Electronics Systems, ICCES 2016
会议日期:21 October 2016 through 22 October 2016
来源:Proceedings of the International Conference on Communication and Electronics Systems, ICCES 2016
出版年:2016
DOI:10.1109/CESYS.2016.7889898
关键词:adaptive control theory; agro-scientific; component; DSP; Unmanned Aerial Vehicle
摘要:With the advancement of the avionics business, the improvement of the unmanned aerial vehicle (UAV) and the utilization of more get the consideration of individuals, unmanned aerial vehicle (UAV) for its little volume, minimal effort, multi-reason and reusable attributes turn into the center of consideration. Flight control framework is the center substance of unmanned aerial vehicle (UAV) to acknowledge self-sufficient flight, how to outline and confirm the strength, unwavering quality of flight control framework and do not have to spend a great deal of labor and material assets in genuine flight hazard, has turned into a critical subject venture improvement. Despite flight control framework in preparing pace and scaling down necessity is increasingly elevated, the flight control framework utilizing DSP as the center processor has gotten to be one of the highlights in agro-logical examination in the momentum, DSP has rich direction framework, fast and high exactness of figuring influence and the upsides of the copious fringe assets, for the flight control arrangement of innovative work gives a decent stage. This Topic consolidated with versatile control hypothesis, going for the weaknesses of the customary control calculation to give hypothetical improvement. © 2016 IEEE.
收录类别:EI;SCOPUS
资源类型:会议论文;期刊论文
原文链接:https://www.scopus.com/inward/record.uri?eid=2-s2.0-85018386690&doi=10.1109%2fCESYS.2016.7889898&partnerID=40&md5=91b4a47942bac7efc6be0394958dc716
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