Attitude control of UAV bicopter using adaptive LQG

Attitude control of UAV bicopter using adaptive LQG

This paper aims to design a controller that is able to maintain the stability of the unmanned aerial vehicle (UAV) bicopter attitude when carrying a payload. When the value of the payload inertia is in uncertainty, it is necessary to design a controller that can carry out the adaptation process. Thi...

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Bibliographic Details
Main Authors: Fahmizal, Hanung Adi Nugroho, Adha Imam Cahyadi, Igi Ardiyanto
Format: Article
Language:English
Published: Elsevier 2024-12-01
Series:Results in Control and Optimization
Subjects:
Attitude control
UAV bicopter
Adaptive LQG
Online Access:http://www.sciencedirect.com/science/article/pii/S2666720724001140
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