Controlled Dynamic System Modeling Experiment

Lin Xu; Wenhan Gao; Hao Sha; Xunhua Dai; Quan Quan

doi:10.1007/978-981-95-1954-5_4

Controlled Dynamic System Modeling Experiment

Lin Xu
, Wenhan Gao
, Hao Sha
, Xunhua Dai
, Quan Quan^*

^*此作品的通讯作者

自动化科学与电气工程学院

Tiangong University
Beihang University
School of Computer Science and Engineering

科研成果: 书/报告/会议事项章节 › 章节 › 同行评审

摘要

Establishing the controlled dynamic model of a micro-small fixed-wing Unmanned Aerial Vehicle (UAV) is fundamental. In order to describe the attitude and position of the micro-small fixed-wing UAV, appropriate coordinate systems must be established. The attitude of the fixed-wing UAV in space is mainly described by the rotation relationship among the ground coordinate system, the body coordinate system, the wind coordinate system, and the flight path coordinate system.

源语言	英语
主期刊名	Micro-Small Fixed-Wing UAV Control
主期刊副标题	Design and Practice
出版商	Springer Nature
页	93-146
页数	54
ISBN（电子版）	9789819519545
ISBN（印刷版）	9789819519538
DOI	https://doi.org/10.1007/978-981-95-1954-5_4
出版状态	已出版 - 1 1月 2026

访问文件

10.1007/978-981-95-1954-5_4

其它文件与链接

链接到 Scopus 的出版物

引用此

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