Design and experimental validation of a robust output feedback control for the coupled dynamics of a micro air vehicle

Design and experimental validation of a robust output feedback control for the coupled dynamics of a micro air vehicle

This paper addresses the design and experimental validation of a linear robust static output feedback controller for a 150 mm span fixed wing micro air vehicle (MAV). Severe coupling between longitudinal and lateral dynamics of the MAV lead to the design of a multivariable controller for the combine...

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Bibliographic Details
Main Authors: Harikumar, Kandath., Dhall, Sidhant, Bhat, Seetharama
Other Authors: School of Electrical and Electronic Engineering
Format: Journal Article
Language:English
Published: 2020
Subjects:
Engineering::Electrical and electronic engineering
Coupled Dynamics
Flight Testing
Online Access:https://hdl.handle.net/10356/143485

Internet

https://hdl.handle.net/10356/143485

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