Disturbance rejection in a fixed wing UAV using nonlinear H<inf>∞</inf> state feedback-Reference-Cited by-同舟云学术

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Disturbance rejection in a fixed wing UAV using nonlinear H∞ state feedback

Published:2011-12 Issue: Volume: Page:
ISSN:
Container-title:2011 9th IEEE International Conference on Control and Automation (ICCA)
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Author:

Ferreira Henrique C.,Baptista Roberto S.,Ishihara Joao Y.,Borges Geovany A.

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx5/6126159/6137867/06138036.pdf?arnumber=6138036

Cited by 9 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. Auto-Landing of Moving-Mass Actuated Unmanned Aerial Vehicles Based on Linear Active Disturbance Rejection Control;Drones;2023-08-21

2. Path Planning Based on Improved MPC for Fixed Wing UAVs with Collision Avoidance;Lecture Notes in Electrical Engineering;2021-10-30

3. Comparison of the Satellite Attitude Control System Design using the H∞ Method and H∞/MLI with Pole Allocation Considering the Parametric Uncertainty;WSEAS TRANSACTIONS ON CIRCUITS AND SYSTEMS;2021-06-28

4. Immersion and invariance control for Euler angles of a fixed‐wing unmanned aerial vehicle;Asian Journal of Control;2021-05-04

5. A Survey of Controller Designs for New Generation UAVs: The Challenge of Uncertain Aerodynamic Parameters;International Journal of Control, Automation and Systems;2019-11-29

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