ePrints@IIScePrints@IISc Home | About | Browse | Latest Additions | Advanced Search | Contact | Help

Design and Experimental Validation of a Robust Output Feedback Control for the Coupled Dynamics of a Micro Air Vehicle

Harikumar, Kandath and Dhall, Sidhant and Bhat, Seetharama (2019) Design and Experimental Validation of a Robust Output Feedback Control for the Coupled Dynamics of a Micro Air Vehicle. In: INTERNATIONAL JOURNAL OF CONTROL AUTOMATION AND SYSTEMS, 17 (1). pp. 155-167.

[img] PDF
Int_Jou_Con_Aut_Sys_17-1_155_2019.pdf - Published Version
Restricted to Registered users only

Download (2MB) | Request a copy
Official URL: https://doi.org/10.1007/s12555-017-0799-2


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 combined dynamics. The control design problem is posed in the framework of static output feedback (SOF) due to the inexpensive computational requirements for implementation. The multiobjective control design problem including stability requirements, closed loop damping ratio requirements and H norm minimization is solved using the hybrid technique of linear matrix inequalities (LMI) and genetic algorithm (GA). The design is carried out in the discrete time domain, facilitating in direct implementation of the multivariable controller in the onboard autopilot hardware. The robustness of the resulting closed loop system under parametric uncertainties is evaluated using structured singular value analysis. The effectiveness of the proposed controller is demonstrated through outdoor flight trial of the micro air vehicle with a customized lightweight autopilot hardware.

Item Type: Journal Article
Additional Information: Copyright of this article belongs to INST CONTROL ROBOTICS & SYSTEMS, KOREAN INST ELECTRICAL ENGINEERS
Keywords: Coupled dynamics; flight testing; genetic algorithm; H control; linear matrix inequalities; micro air vehicle; robustness; static output feedback
Department/Centre: Division of Mechanical Sciences > Aerospace Engineering(Formerly Aeronautical Engineering)
Depositing User: Id for Latest eprints
Date Deposited: 06 Feb 2019 05:54
Last Modified: 06 Feb 2019 05:54
URI: http://eprints.iisc.ac.in/id/eprint/61594

Actions (login required)

View Item View Item