A Novel Rolling Takeoff Flight Control for Fixed-Wing Unmanned Aerial Vehicle-Reference-Cited by-同舟云学术

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A Novel Rolling Takeoff Flight Control for Fixed-Wing Unmanned Aerial Vehicle

Published:2024-05-10 Issue: Volume: Page:1520-1525
ISSN:
Container-title:2024 3rd Conference on Fully Actuated System Theory and Applications (FASTA)
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Author:

Liu Wangkui¹,Wang Xiangyu¹,Shui Zunshi¹,Chen Zhihua²,Qiu Huabing¹,Yang Xuefei³

Affiliation:

1. Beijing Institute of Aerospace Technology,Beijing,China,100074

2. Beijing Institute of Control Engineering,Beijing,China,100190

3. Harbin Institute of Technology,Harbin,China,150001

Funder

National Natural Science Foundation of China

National Defense Basic Scientific Research Program of China

Fundamental Research Funds for the Central Universities

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx8/10595059/10595098/10595258.pdf?arnumber=10595258

Reference18 articles.

1. Unmanned Aerial Vehicles: Control Methods and Future Challenges

2. A survey on technologies for automatic forest fire monitoring, detection, and fighting using unmanned aerial vehicles and remote sensing techniques

3. COMPARISON OF A FIXED-WING AND MULTI-ROTOR UAV FOR ENVIRONMENTAL MAPPING APPLICATIONS: A CASE STUDY

4. SONGBIRD – AN INNOVATIVE UAS COMBINING THE ADVANTAGES OF FIXED WING AND MULTI ROTOR UAS

5. Stabilisation of quadrotor aircraft with constrained controls

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