Wind Field Disturbance Analysis and Flight Control System Design for a Novel Tilt-Rotor UAV-Reference-Cited by-同舟云学术

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Wind Field Disturbance Analysis and Flight Control System Design for a Novel Tilt-Rotor UAV

Published:2020 Issue: Volume:8 Page:211401-211410
ISSN:2169-3536
Container-title:IEEE Access
language:
Short-container-title:IEEE Access

Author:

Zhang Qian^ORCID,Zhang Jingjuan,Wang Xueyun,Xu Yifan,Yu Zelong

Funder

Aviation Science Foundation

Project of Beijing Natural Science Foundation

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Subject

General Engineering,General Materials Science,General Computer Science

Link

http://xplorestaging.ieee.org/ielx7/6287639/8948470/09265198.pdf?arnumber=9265198

Cited by 7 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Nonlinear optimal control for UAVs with tilting rotors;International Journal of Intelligent Unmanned Systems;2023-07-25

2. ℒ₁ adaptive attitude augmentation of a small scale unmanned helicopter;2023 International Conference on Unmanned Aircraft Systems (ICUAS);2023-06-06

3. Obstacle Avoidance and Trajectory Tracking Control of a Quadrotor UAV Under Wind Disturbance;Lecture Notes in Electrical Engineering;2023

4. Wind resistance aerial path planning for efficient reconstruction of offshore ship;International Journal of Digital Earth;2022-11-06

5. Finite time switching optimal control for tilt-rotor aircrafts based on novel time scaling method;2022 34th Chinese Control and Decision Conference (CCDC);2022-08-15

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