{"title":"Tuning and miniaturization of active vibration controllers of a fixed-wing composite aircraft drone using the experiment-on-the-loop system","authors":"Tarcisio M.P. Silva , Giulio Franchini , Prabakaran Balasubramanian , Abdulaziz Buabdulla , Sudhir Kumar Singh , Mohammed AlNuaimi , Rashed AlHammadi , Marco Amabili","doi":"10.1016/j.ast.2025.111004","DOIUrl":null,"url":null,"abstract":"<div><div>Active vibration control (AVC) in Unmanned Air Vehicles (UAV) enhances flight stability, enables lighter and more efficient designs, and improves fuel efficiency and payload capacity. However, AVC systems require careful design, and this study demonstrates how they can be efficiently tuned on a fixed-wing, composite aircraft drone using a purely experimental approach, leveraging the newly developed Experiment-in-the-Loop (EITL) method. The EITL is a real-time optimizer, capable of autonomously running hundreds or thousands of experimental tests on a target structure. In each test, the EITL iteratively refines the control parameters, progressively improving their performance. The EITL offers the advantage of being fast, tuning the controllers within hours, and not relying on numerical models. In this paper, 9 AVC systems are tuned, including four Positive Position Feedback (PPFs) controllers and five higher-order controllers. Experimental results show that these controllers reduce vibrations on the composite aircraft drone by an average of 55 % over 7 resonant modes in the frequency range from 0 to 250 Hz. In addition, results show how AVC systems can be practically implemented using lightweight hardware. The developed scaled-down AVC system weighs 183.8 g and occupies 273.5 cm<sup>3</sup>, making it a promising solution for onboard UAV applications.</div></div>","PeriodicalId":50955,"journal":{"name":"Aerospace Science and Technology","volume":"168 ","pages":"Article 111004"},"PeriodicalIF":5.8000,"publicationDate":"2025-09-25","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Aerospace Science and Technology","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S1270963825010673","RegionNum":1,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
引用次数: 0
Abstract
Active vibration control (AVC) in Unmanned Air Vehicles (UAV) enhances flight stability, enables lighter and more efficient designs, and improves fuel efficiency and payload capacity. However, AVC systems require careful design, and this study demonstrates how they can be efficiently tuned on a fixed-wing, composite aircraft drone using a purely experimental approach, leveraging the newly developed Experiment-in-the-Loop (EITL) method. The EITL is a real-time optimizer, capable of autonomously running hundreds or thousands of experimental tests on a target structure. In each test, the EITL iteratively refines the control parameters, progressively improving their performance. The EITL offers the advantage of being fast, tuning the controllers within hours, and not relying on numerical models. In this paper, 9 AVC systems are tuned, including four Positive Position Feedback (PPFs) controllers and five higher-order controllers. Experimental results show that these controllers reduce vibrations on the composite aircraft drone by an average of 55 % over 7 resonant modes in the frequency range from 0 to 250 Hz. In addition, results show how AVC systems can be practically implemented using lightweight hardware. The developed scaled-down AVC system weighs 183.8 g and occupies 273.5 cm3, making it a promising solution for onboard UAV applications.
期刊介绍:
Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to:
• The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites
• The control of their environment
• The study of various systems they are involved in, as supports or as targets.
Authors are invited to submit papers on new advances in the following topics to aerospace applications:
• Fluid dynamics
• Energetics and propulsion
• Materials and structures
• Flight mechanics
• Navigation, guidance and control
• Acoustics
• Optics
• Electromagnetism and radar
• Signal and image processing
• Information processing
• Data fusion
• Decision aid
• Human behaviour
• Robotics and intelligent systems
• Complex system engineering.
Etc.