Flight control systems of a quad tilt rotor Unmanned Aerial Vehicle for a large attitude change-Reference-Cited by-同舟云学术

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Flight control systems of a quad tilt rotor Unmanned Aerial Vehicle for a large attitude change

Published:2015-05 Issue: Volume: Page:
ISSN:
Container-title:2015 IEEE International Conference on Robotics and Automation (ICRA)
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Author:

Oosedo Atsushi,Abiko Satoko,Narasaki Shota,Kuno Atsushi,Konno Atsushi,Uchiyama Masaru

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/7128761/7138973/07139508.pdf?arnumber=7139508

Cited by 51 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. An overactuated aerial robot based on cooperative quadrotors attached through passive universal joints: Modeling, control and 6-DoF trajectory tracking;Robotics and Autonomous Systems;2024-10

2. Geometric Tracking Control of A Quadrotor with Tilted Propellers;2024 IEEE International Conference on Advanced Intelligent Mechatronics (AIM);2024-07-15

3. Aggressive flight control of quadrotors using incremental nonlinear dynamic inversion with a high-fidelity thrust unit model;Journal of the Franklin Institute;2024-07

4. Agile Flight Control Using Incremental Nonlinear Dynamic Inversion with Highly Realistic Model of Actuator;2024 8th International Conference on Robotics, Control and Automation (ICRCA);2024-01-12

5. Motor-level Nonlinear Model Predictive Control for a Tilting Quadrotor;2023 IEEE Conference on Control Technology and Applications (CCTA);2023-08-16

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