Modeling and identification of electric propulsion system for multirotor unmanned aerial vehicle design-Reference-Cited by-同舟云学术

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Modeling and identification of electric propulsion system for multirotor unmanned aerial vehicle design

Published:2014-05 Issue: Volume: Page:
ISSN:
Container-title:2014 International Conference on Unmanned Aircraft Systems (ICUAS)
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Author:

Szafranski Grzegorz,Czyba Roman,Blachuta Marian

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/6835384/6842225/06842287.pdf?arnumber=6842287

Cited by 19 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. Development and Evaluation of Multirotor Flight Dynamic Models for Estimation and Control;AIAA SCITECH 2024 Forum;2024-01-04

2. Robust Linear Parameter-Varying Control for Safe and Effective Unstable Aircraft System Identification;AIAA SCITECH 2024 Forum;2024-01-04

3. Mixed H ₂ / H _∞ model reference control of linear parameter‐varying discrete‐time systems with real‐time application to aeropendulum system;International Journal of Robust and Nonlinear Control;2022-10-14

4. Experimental Measurement of a UAV Propeller's Thrust;Tehnicki vjesnik - Technical Gazette;2022-02-05

5. Control robusto H-infinito para la velocidad de desplazamiento de un UAV en base a estimación de flujo óptico;Revista Iberoamericana de Automática e Informática industrial;2021-07-01

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