标题:Study on Integrated Flight/Propulsion Control Method of Compound Adjustable Ducted Rocket
作者:Cai, Feichao ;Shao, Mingyu
通讯作者:Shao, Mingyu
作者机构:[Cai, Feichao ] School of Power and Energy, Northwestern Polytechnical University, Xi’an; 710072, China;[Shao, Mingyu ] School of Transportation 更多
会议名称:Asia-Pacific International Symposium on Aerospace Technology, APISAT 2018
会议日期:16 October 2018 through 18 October 2018
来源:Lecture Notes in Electrical Engineering
出版年:2019
卷:459
页码:2398-2409
DOI:10.1007/978-981-13-3305-7_192
关键词:Compound adjustment; Ducted rocket; Integrated flight/propulsion control
摘要:For the integrated control of the missile and the compound adjustable ducted rocket, the Integrated Flight/Propulsion Control (IFPC) system was constructed by hierarchical dispersion method based on the mathematical model of the system and the coupling characteristics analysis between the subsystems. According to the work principle of the integrated system, the integration and the coordination of the subsystems were achieved by the motion control commands and the coordination control commands respectively. The IFPC method was validated by simulation based on typical mission. The results show that the IFPC system can control the motion of the missile and coordinate the operating status of the subsystems effectively. © 2019, Springer Nature Singapore Pte Ltd.
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-s2.0-85070777739&doi=10.1007%2f978-981-13-3305-7_192&partnerID=40&md5=2c6369b8fa58d5fae9f096982f44f256
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