Flatness-Based Active Disturbance Rejection Control for a PVTOL Aircraft System with an Inverted Pendular Load

Flatness-Based Active Disturbance Rejection Control for a PVTOL Aircraft System with an Inverted Pendular Load

This paper presents a systematic procedure for the control scheme design for a PVTOL aircraft system with an inverted pendular load, which is a nonlinear underactuated system. The control scheme is based on the use of angular movement as an artificial control in order to propose new auxiliary contro...

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Bibliographic Details
Main Authors: Cesar Alejandro Villaseñor Rios, Alberto Luviano-Juárez, Norma Beatriz Lozada-Castillo, Blanca Esther Carvajal-Gámez, Dante Mújica-Vargas, Octavio Gutiérrez-Frías
Format: Article
Language:English
Published: MDPI AG 2022-07-01
Series:Machines
Subjects:
underactuated systems
inverted pendulum
unmanned aerial vehicle
active disturbance rejection control
nonlinear control
robust control
Online Access:https://www.mdpi.com/2075-1702/10/7/595

Internet

https://www.mdpi.com/2075-1702/10/7/595

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