Cascaded Control System Design for Quadrotor UAV through Relay with Embedded Integrator-Based Automatic Tuning Approach

Author:

Hoshu Ayaz Ahmed12ORCID,Mustafa Abro Ghulam E3ORCID,Alhussein Musaed4ORCID,Tunio Irfan Ali2ORCID,Aurangzeb Khursheed4ORCID,Ali Anwar5

Affiliation:

1. School of Engineering, RMIT University, Melbourne, VIC 3000, Australia

2. Department of Electronic Engineering, Quaid-e-Awam University of Engineering, Science and Technology, Campus Larkana 77150, Pakistan

3. Electrical and Electronic Engineering, Universiti Teknologi PETRONAS, Seri Iskandar, 32610 Perak, Malaysia

4. Department of Computer Engineering, College of Computer and Information Sciences, King Saud University, P.O. Box 51178, Riyadh 11543, Saudi Arabia

5. Department of Electronic and Electrical Engineering, Faculty of Science and Engineering, Swansea University Bay Campus Swansea, UK

Abstract

Due to their enormous characteristics and applicability, quadrotor unmanned aerial vehicles (UAVs) have enjoyed much popularity lately. However, designing a stable control strategy for quadrotors still remains one of the major concerns mainly due to the requirement of an accurate system model. They are naturally underactuated systems, with complex and nonlinear dynamics as well as interaxes couplings. Considering the dynamical complexities of these vehicles, one of the efficient methods is to utilize the relay feedback experiments and automatic tuning approach to tackle these issues. This paper investigates the employment of the relay with embedded integrator approach, wherein the quadrotor dynamics are estimated effectively with minimal parameters as compared to previously utilized relay with hysteresis technique. Frequency sampling filter (FSF) is further utilized for the extraction of the needful data through the signals obtained using the relay experiments, followed by the estimation of the plant dynamics. PID controllers have then been developed using the approximated quadrotor models. Which are used in the proposed cascade control structure for the quadrotor. The demonstrated results and analysis present the efficacy of designed control system technique for the quadrotor UAV.

Funder

King Saud University

Publisher

Hindawi Limited

Subject

Aerospace Engineering

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