Design and Flight Control of a Novel Tilt-Rotor Octocopter Using Passive Hinges-Reference-Cited by-同舟云学术

Design and Flight Control of a Novel Tilt-Rotor Octocopter Using Passive Hinges

Published:2024-01 Issue:1 Volume:9 Page:199-206
ISSN:2377-3766
Container-title:IEEE Robotics and Automation Letters
language:
Short-container-title:IEEE Robot. Autom. Lett.

Author:

Qin Zijie¹^ORCID,Wei Jingbo¹^ORCID,Cao Mingzhi¹^ORCID,Chen Baihui²^ORCID,Li Kaixin¹^ORCID,Liu Kun¹^ORCID

Affiliation:

1. School of Aeronautics and Astronautics, Sun Yat-sen University, Shenzhen, China

2. Faculty of Aerospace Engineering, Delft University of Technology, Delft, The Netherland

Funder

Shenzhen Science and Technology Program

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Subject

Artificial Intelligence,Control and Optimization,Computer Science Applications,Computer Vision and Pattern Recognition,Mechanical Engineering,Human-Computer Interaction,Biomedical Engineering,Control and Systems Engineering

Link

http://xplorestaging.ieee.org/ielx7/7083369/10320104/10265217.pdf?arnumber=10265217

Reference26 articles.

1. An Over-Actuated Multi-Rotor Aerial Vehicle With Unconstrained Attitude Angles and High Thrust Efficiencies

2. A Simple Six Degree-of-Freedom Aerial Vehicle Built on Quadcopters

3. A Fast and Efficient Attitude Control Algorithm of a Tilt-Rotor Aerial Platform Using Inputs Redundancies

4. Control and experiments of a novel tiltable-rotor aerial platform comprising quadcopters and passive hinges

5. A Novel Robotic Platform for Aerial Manipulation Using Quadrotors as Rotating Thrust Generators

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1. Stochastic optimal tuning for flight control system of morphing arm octorotor;Aircraft Engineering and Aerospace Technology;2024-06-05

2. Robust Attitude Control of a Tilt Trirotor in VTOL mode;2024 3rd Conference on Fully Actuated System Theory and Applications (FASTA);2024-05-10