Augusto H.B.M. Tavares , Saulo O.D. Luiz , Tiago P. Nascimento , Antonio M.N. Lima
{"title":"Trade-off between flight performance and energy consumption of a quadrotor","authors":"Augusto H.B.M. Tavares , Saulo O.D. Luiz , Tiago P. Nascimento , Antonio M.N. Lima","doi":"10.1016/j.mechatronics.2025.103316","DOIUrl":null,"url":null,"abstract":"<div><div>This paper studies analytically and quantitatively the influence of the power source on the dynamic performance of the altitude control system of a quadrotor powered by an electrochemical battery. This paper also proposes the formulation of the altitude control system design as a constrained optimization problem in which the drone, actuators, control law, and electrochemical battery models are considered, to define a trade-off between the power consumption rate and the closed-loop dynamic performance loss. An analytical representation of the effect of the battery discharge over the altitude dynamics is obtained through a linear approximation, enabling an analysis of the system poles. The problem of designing an altitude controller is then posed as a constrained optimization problem that can include the battery as a factor. A comparison of the error transient response between the cases of the battery-unaware controller design and the battery-aware controller design is performed in simulations and experimental flight tests. The results lead to the following conclusions: i. the analytical demonstration agrees with the worse performance observed in the in-flight dynamics as the battery discharges and ii. through a battery-aware controller design approach this effect can be diminished, at the cost of a trade-off in the battery discharge rate.</div></div>","PeriodicalId":49842,"journal":{"name":"Mechatronics","volume":"108 ","pages":"Article 103316"},"PeriodicalIF":3.1000,"publicationDate":"2025-04-24","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Mechatronics","FirstCategoryId":"94","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S095741582500025X","RegionNum":3,"RegionCategory":"计算机科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q2","JCRName":"AUTOMATION & CONTROL SYSTEMS","Score":null,"Total":0}
引用次数: 0
Abstract
This paper studies analytically and quantitatively the influence of the power source on the dynamic performance of the altitude control system of a quadrotor powered by an electrochemical battery. This paper also proposes the formulation of the altitude control system design as a constrained optimization problem in which the drone, actuators, control law, and electrochemical battery models are considered, to define a trade-off between the power consumption rate and the closed-loop dynamic performance loss. An analytical representation of the effect of the battery discharge over the altitude dynamics is obtained through a linear approximation, enabling an analysis of the system poles. The problem of designing an altitude controller is then posed as a constrained optimization problem that can include the battery as a factor. A comparison of the error transient response between the cases of the battery-unaware controller design and the battery-aware controller design is performed in simulations and experimental flight tests. The results lead to the following conclusions: i. the analytical demonstration agrees with the worse performance observed in the in-flight dynamics as the battery discharges and ii. through a battery-aware controller design approach this effect can be diminished, at the cost of a trade-off in the battery discharge rate.
期刊介绍:
Mechatronics is the synergistic combination of precision mechanical engineering, electronic control and systems thinking in the design of products and manufacturing processes. It relates to the design of systems, devices and products aimed at achieving an optimal balance between basic mechanical structure and its overall control. The purpose of this journal is to provide rapid publication of topical papers featuring practical developments in mechatronics. It will cover a wide range of application areas including consumer product design, instrumentation, manufacturing methods, computer integration and process and device control, and will attract a readership from across the industrial and academic research spectrum. Particular importance will be attached to aspects of innovation in mechatronics design philosophy which illustrate the benefits obtainable by an a priori integration of functionality with embedded microprocessor control. A major item will be the design of machines, devices and systems possessing a degree of computer based intelligence. The journal seeks to publish research progress in this field with an emphasis on the applied rather than the theoretical. It will also serve the dual role of bringing greater recognition to this important area of engineering.