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Cascade control for heterogeneous multirotor UAS

Ayaz Ahmed Hoshu (RMIT University, Melbourne, Australia)
Liuping Wang (RMIT University, Melbourne, Australia)
Alex Fisher (RMIT University, Melbourne, Australia)
Abdul Sattar (RMIT University, Melbourne, Australia)

International Journal of Intelligent Unmanned Systems

ISSN: 2049-6427

Article publication date: 29 April 2021

Issue publication date: 22 November 2022

121

Abstract

Purpose

Despite of the numerous characteristics of the multirotor unmanned aircraft systems (UASs), they have been termed as less energy-efficient compared to fixed-wing and helicopter counterparts. The purpose of this paper is to explore a more efficient multirotor configuration and to provide the robust and stable control system for it.

Design/methodology/approach

A heterogeneous multirotor configuration is explored in this paper, which employs a large rotor at the centre to provide majority of lift and three small tilted booms rotors to provide the control. Design provides the combined characteristics of both quadcopters and helicopters in a single UAS configuration, providing endurance of helicopters keeping the manoeuvrability, simplicity and control of quadcopters. In this paper, rotational as well as translational dynamics of the multirotor are explored. Cascade control system is designed to provide an effective solution to control the attitude, altitude and position of the rotorcraft.

Findings

One of the challenging tasks towards successful flight of such a configuration is to design a stable and robust control system as it is an underactuated system possessing complex non-linearities and coupled dynamics. Cascaded proportional integral (PI) control approach has provided an efficient solution with stable control performance. A novel motor control loop is implemented to ensure enhanced disturbance rejection, which is also validated through Dryden turbulence model and 1-cosine gust model.

Originality/value

Robustness and stability of the proposed control structure for such a dynamically complex UAS configuration is demonstrated with stable attitude and position performance, reference tracking and enhanced disturbance rejection.

Keywords

Citation

Hoshu, A.A., Wang, L., Fisher, A. and Sattar, A. (2022), "Cascade control for heterogeneous multirotor UAS", International Journal of Intelligent Unmanned Systems, Vol. 10 No. 4, pp. 363-384. https://doi.org/10.1108/IJIUS-02-2021-0008

Publisher

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Emerald Publishing Limited

Copyright © 2021, Emerald Publishing Limited

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