{"title":"Development of Centralized Multivariable Cascade Control Strategy for Quadcopter System","authors":"Vasanthakumar Sekar, K. Srinivasan","doi":"10.3103/S0146411626700409","DOIUrl":null,"url":null,"abstract":"<p>In this article proposes a novel centralized cascade control framework for quadcopter attitude and trajectory tracking that explicitly suppresses secondary cross-coupling effects commonly observed in multivariable UAV dynamics. The nonlinear quadcopter model is transformed into a set of region-dependent linear MIMO state-space representations using a piecewise affine (PWA) formulation, and each region model is converted into a MIMO transfer-function form to support systematic multivariable controller synthesis. To avoid ad hoc loop selection, a hybrid loop-pairing method is introduced to identify feasible pairings and reduce unfavourable inner-loop interactions across operating regions. Based on this pairing, an IMC-based switching enhanced cascade PID/PI design is developed, employing an enhanced PID controller in the outer loop and an enhanced PI controller in the inner loop, with regionwise scheduling to maintain performance over the operating envelope. The proposed method (Ce) achieves the lowest ISE in both Simulation-1 and Simulation-2 for roll <span>\\(\\left( \\phi \\right)\\)</span> and pitch <span>\\(\\left( \\theta \\right)\\)</span>, showing consistent improvement over both De and Ge. The ISE reductions are 14.34 and 11.29% over De in Simulation-1, and 12.91 and 16.83% over De in Simulation-2 for roll and pitch, respectively, with even larger improvements over Ge. Extensive simulations demonstrate improved tracking accuracy with reduced coupling effects while satisfying state and input constraints. Comparisons with a decentralized cascade controller and a conventional cascade controller further confirm the effectiveness and efficiency of the proposed approach.</p>","PeriodicalId":46238,"journal":{"name":"AUTOMATIC CONTROL AND COMPUTER SCIENCES","volume":"60 2","pages":"143 - 163"},"PeriodicalIF":0.5000,"publicationDate":"2026-09-24","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"AUTOMATIC CONTROL AND COMPUTER SCIENCES","FirstCategoryId":"1085","ListUrlMain":"https://link.springer.com/article/10.3103/S0146411626700409","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q4","JCRName":"AUTOMATION & CONTROL SYSTEMS","Score":null,"Total":0}
引用次数: 0
Abstract
In this article proposes a novel centralized cascade control framework for quadcopter attitude and trajectory tracking that explicitly suppresses secondary cross-coupling effects commonly observed in multivariable UAV dynamics. The nonlinear quadcopter model is transformed into a set of region-dependent linear MIMO state-space representations using a piecewise affine (PWA) formulation, and each region model is converted into a MIMO transfer-function form to support systematic multivariable controller synthesis. To avoid ad hoc loop selection, a hybrid loop-pairing method is introduced to identify feasible pairings and reduce unfavourable inner-loop interactions across operating regions. Based on this pairing, an IMC-based switching enhanced cascade PID/PI design is developed, employing an enhanced PID controller in the outer loop and an enhanced PI controller in the inner loop, with regionwise scheduling to maintain performance over the operating envelope. The proposed method (Ce) achieves the lowest ISE in both Simulation-1 and Simulation-2 for roll \(\left( \phi \right)\) and pitch \(\left( \theta \right)\), showing consistent improvement over both De and Ge. The ISE reductions are 14.34 and 11.29% over De in Simulation-1, and 12.91 and 16.83% over De in Simulation-2 for roll and pitch, respectively, with even larger improvements over Ge. Extensive simulations demonstrate improved tracking accuracy with reduced coupling effects while satisfying state and input constraints. Comparisons with a decentralized cascade controller and a conventional cascade controller further confirm the effectiveness and efficiency of the proposed approach.
本文提出了一种新的四轴飞行器姿态和轨迹跟踪集中级联控制框架,该框架明确地抑制了多变量无人机动力学中常见的二次交叉耦合效应。利用分段仿射(PWA)公式将非线性四轴飞行器模型转换为一组区域相关的线性MIMO状态空间表示,并将每个区域模型转换为MIMO传递函数形式,以支持系统多变量控制器综合。为了避免临时环路选择,引入了一种混合环路配对方法来确定可行的配对,并减少跨操作区域的不利内环相互作用。基于这种配对,开发了一种基于imc的交换增强级联PID/PI设计,在外环采用增强型PID控制器,内环采用增强型PI控制器,并采用区域调度来保持运行包络范围内的性能。所提出的方法(Ce)在模拟1和模拟2中实现了滚转\(\left( \phi \right)\)和俯仰\(\left( \theta \right)\)的最低ISE,比De和Ge都有一致的改进。ISE的降幅分别为14.34和11.29% over De in Simulation-1, and 12.91 and 16.83% over De in Simulation-2 for roll and pitch, respectively, with even larger improvements over Ge. Extensive simulations demonstrate improved tracking accuracy with reduced coupling effects while satisfying state and input constraints. Comparisons with a decentralized cascade controller and a conventional cascade controller further confirm the effectiveness and efficiency of the proposed approach.
期刊介绍:
Automatic Control and Computer Sciences is a peer reviewed journal that publishes articles on• Control systems, cyber-physical system, real-time systems, robotics, smart sensors, embedded intelligence • Network information technologies, information security, statistical methods of data processing, distributed artificial intelligence, complex systems modeling, knowledge representation, processing and management • Signal and image processing, machine learning, machine perception, computer vision