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^*

^*Corresponding author for this work

School of Automation Science and Electrical Engineering

Tiangong University
Beihang University
School of Computer Science and Engineering

Research output: Chapter in Book/Report/Conference proceeding › Chapter › peer-review

Abstract

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.

Original language	English
Title of host publication	Micro-Small Fixed-Wing UAV Control
Subtitle of host publication	Design and Practice
Publisher	Springer Nature
Pages	93-146
Number of pages	54
ISBN (Electronic)	9789819519545
ISBN (Print)	9789819519538
DOIs	https://doi.org/10.1007/978-981-95-1954-5_4
State	Published - 1 Jan 2026

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Controlled Dynamic System Modeling Experiment

Abstract

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