UAV’s Pitch Angle Control Scheme based on Terminal Sliding Mode Control

DOI

10.2991/978-94-6463-540-9_49How to use a DOI?

Keywords

Fixed-wing UAV; Terminal Sliding Mode (TSM); Control

Abstract

As their application scenarios become more diverse, the demand for control methods that can resist interference is also growing. This is particularly important for UAVs operating in some scene happened in complex environments, where they may be susceptible to various external interference factors, such as wind, which can affect their stability and performance. To address this issue, this paper aims to provide a novel control method based on Terminal Sliding Mode (TSM) control. TSM control is a type of robust control strategy that has been successfully applied to a wide range of systems, including UAVs. By using various stimulations, the aim is set to create a tailor-made TSM method that can effectively weaken the influence of interference, such as wind, on fixed-wing UAVs. The verification of the effectiveness of the proposed TSM control method will be conducted through simulations and experiments. This research not only contributes to the development of UAV control technology but also has practical significance for the application of UAVs in fields such as disaster relief, environmental monitoring, and military operations, where stable and reliable flight performance is of paramount importance. Furthermore, the proposed TSM control method can be potentially applied to other types of UAVs and even other types of robotic systems, providing a more general solution for the interference problem in robotic control.

Copyright

© 2024 The Author(s)

Open Access

Open Access This chapter is licensed under the terms of the Creative Commons Attribution-NonCommercial 4.0 International License (http://creativecommons.org/licenses/by-nc/4.0/), which permits any noncommercial use, sharing, adaptation, distribution and reproduction in any medium or format, as long as you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons license and indicate if changes were made.

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TY  - CONF
AU  - Xiaosong Xie
PY  - 2024
DA  - 2024/10/16
TI  - UAV’s Pitch Angle Control Scheme based on Terminal Sliding Mode Control
BT  - Proceedings of the 2024 2nd International Conference on Image, Algorithms and Artificial Intelligence (ICIAAI 2024)
PB  - Atlantis Press
SP  - 494
EP  - 503
SN  - 2352-538X
UR  - https://doi.org/10.2991/978-94-6463-540-9_49
DO  - 10.2991/978-94-6463-540-9_49
ID  - Xie2024
ER  -