Design of Robust Controller for Tail-Sitter VTOL Aircraft-Reference-Cited by-同舟云学术

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Design of Robust Controller for Tail-Sitter VTOL Aircraft

Published:2023-10-25 Issue: Volume: Page:
ISSN:
Container-title:2023 IEEE 8th International Conference on Engineering Technologies and Applied Sciences (ICETAS)
language:
Short-container-title:

Author:

Husain Suha S.¹,Rasheed Luay T.²,Mahmod Rawnaq A.³,Hamza Ekhlas K.²,Noaman Noaman M.⁴,Humaidi Amjad Jaleel⁵

Affiliation:

1. University of Technology,Department of Construction and Projects,Baghdad,Iraq

2. University of Technology,Control and Systems Eng. Department,Baghdad,Iraq

3. Training & Energy Researches Office, Ministry of Electricity,Baghdad,Iraq

4. University of Technology,Department of Mechatronics Engineering,Bahrain

5. University of Technology,Control and Systems Eng. Dept.,Baghdad,Iraq

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/10346240/10346252/10346499.pdf?arnumber=10346499

Reference35 articles.

1. A survey of hybrid Unmanned Aerial Vehicles

2. Robust Tracking Control of a Quadrotor UAV Based on Adaptive Sliding Mode Controller

3. Sliding Mode Control of VTOL System

4. Grey-wolf optimization better enhances the dynamic performance of roll motion for tail-sitter VTOL aircraft guided and controlled by STSMC;Al-Qassar;Journal of Engineering Science and Technology (JESTEC),2021

Cited by 1 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. Adaptive Integral Sliding Mode Controller (SMC) Design for Vehicle Steer-by-Wire System;SAE International Journal of Vehicle Dynamics, Stability, and NVH;2024-06-14

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