Autonomous Landing of Tailless, Blended Wing, and Variable Centre of Mass UAV using Adaptive Control-Reference-Cited by-同舟云学术

Autonomous Landing of Tailless, Blended Wing, and Variable Centre of Mass UAV using Adaptive Control

Published:2022-05-17 Issue: Volume: Page:
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Container-title:2022 8th International Conference on Control, Decision and Information Technologies (CoDIT)
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Author:

Lungu Mihai¹,Flores Gerardo²,Dinu Dana-Aurelia³,Ciuca George Mihail⁴

Affiliation:

1. University of Craiova and University “Politehnica” of Bucharest,Romania

2. Centro de Investigaciones en Optica A.C.,Leon,Guanajuato,Mexico

3. University “Politehnica” of Bucharest, Faculty of Aerospace Engineering,Romania

4. “Ferdinand I” Military Technical Academy,Bucharest,Romania

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/9803856/9803880/09803999.pdf?arnumber=9803999

Reference16 articles.

1. State-of-the-Art Intelligent Flight Control Systems in Unmanned Aerial Vehicles

2. Flight Control System for a Variable Stability Blended-wing-Body Unmanned Aerial Vehicle;blaaw;University of South Africa,2009

3. Backstepping and dynamic inversion based auto-landing system for variable centre of mass UAV;lungu;24th International Conference on System Theory Control and Computing Joint Conference,2020

4. Autonomous Landing of a UAV on a Moving Platform Using Model Predictive Control

5. Synthesis and validation of flight control for UAV;paw;University of Minnesota PhD Dissertation,2009

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