弹道
控制理论(社会学)
PID控制器
群体行为
跟踪(教育)
控制工程
计算机科学
控制(管理)
工程类
人工智能
物理
温度控制
天文
心理学
教育学
作者
Ghulam E Mustafa Abro,Ayman M. Abdallah
标识
DOI:10.1109/tase.2025.3582119
摘要
Quadrotor unmanned aerial vehicles (QUAVs) are inherently underactuated, which makes it challenging to accomplish precision control and trajectory tracking, particularly in flight circumstances that are intricate. This is especially true in situations where flights are complicated. For the goal of this investigation, a sophisticated Fractional-Order PID (FOPID) controller is presented. This controller will be superior in terms of performance to both conventional PID controllers and Integral State Feedback Algorithm (ISFA) controllers. The adoption of the FOPID design results in improvement in tracking accuracy, decreases in overshoot and steady-state error, and better resistance to disturbances and system uncertainties. All of these benefits are obtained through the implementation of the design. The controller demonstrates superior transient and steady-state performance, as demonstrated by simulations carried out in MATLAB/Simulink and validations carried out through experiments utilising two different scenarios, such as helical trajectory tracking and circular swarm formation, and two different hardwares, such as QDrones by Quansar and CoDrones by Robolink. The results proved that the FOPID technique demonstrates a high degree of adaptability and scalability, which makes it an ideal choice for swarm-based missions as well as real-world applications such as environmental monitoring. This is accomplished through its integration with a helical trajectory tracking and circular swarm formation framework that is implemented across two different hardwares. FOPID is a strategy that is both effective and feasible for the regulation of QUAVs of the future generation, as demonstrated by the outcomes of this study.
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