Research on Altitude Control of Flapping-Wing Aircraft Based on Nonlinear Backstepping Method-Reference-Cited by-同舟云学术

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Research on Altitude Control of Flapping-Wing Aircraft Based on Nonlinear Backstepping Method

Published:2023-09-22 Issue: Volume: Page:170-174
ISSN:
Container-title:2023 5th International Symposium on Robotics & Intelligent Manufacturing Technology (ISRIMT)
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Author:

Zhang Shuhan¹,Li Xiangxi²,Zou Junheng³,Liu Yifan²,Hu Minjie²,Zhang Mingkang⁴,He Tao¹,Shi Weiling²,Liu Ping²

Affiliation:

1. School of Mechatronics and Vehicle Engineering, Chongqing Jiao-tong University,Chong-Qing,China,400074

2. School of Aviation, Chongqing Jiao tong University,Chong-Qing,China,400074

3. School of Information Science and Engineering, Chongqing Jiao tong University,Chong-Qing,China,400074

4. Sungkyunkwan University,Department of electronics and electrical,Chong-Qing,China

Funder

Chongqing Jiaotong University

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/10428112/10428099/10428450.pdf?arnumber=10428450

Reference20 articles.

1. Research on autonomous planning and control technology of UAV swarm formation [D];Zhang;Tianjin university,2022

2. Extended State Observer based Attitude Control of a Bird-like Flapping-wing Flying Robot

3. Design and development considerations for biologically inspired flapping-wing micro air vehicles

4. Adaptive Control of Flapping-Wing Micro Aerial Vehicle with Coupled Dynamics and Unknown Model Parameters

5. Multiobjective Optimization-Based Terrestrial Laser Scanning Layout Planning for Landslide Monitoring

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