可扩展性
模块化设计
控制工程
控制器(灌溉)
计算机科学
线性二次调节器
工程类
控制(管理)
控制理论(社会学)
PID控制器
实时计算
控制系统
数字控制
理论(学习稳定性)
惯性测量装置
四轴飞行器
飞行动力学
模拟
钥匙(锁)
作者
Xunhua Dai,Wanqi Gong,Jiajing Tu,Yong Chen
标识
DOI:10.1142/s2301385027500464
摘要
As multicopter Unmanned Aerial Vehicles (UAVs) are increasingly adopted in industrial and manufacturing applications, there is a growing demand for robust, efficient, and cost-effective control algorithm development. However, traditional trial-and-error approaches relying heavily on real-flight experiments remain time-consuming and resource-intensive, particularly in dynamic or uncertain environments. To address these challenges, this paper presents a digital twin-level modeling framework that enables high-fidelity simulation, accelerated controller design, and seamless sim2real transfer. The framework integrates detailed physical modeling of multicopter dynamics, realistic sensor emulation, and Hardware-In-the-Loop (HIL) simulation within a modular architecture. Each subsystem — including propulsion, aerodynamics, ground interaction, and onboard sensors — is systematically constructed and verified using experimental data. A representative application is demonstrated by designing a model-based Linear Quadratic Regulator (LQR) controller trained using hybrid data composed of digital simulations and a small amount of real-world flight data. The controller is evaluated under external wind disturbances and benchmarked against baseline PX4 and hand-tuned PID controllers. Quantitative comparisons using standard performance metrics demonstrate that the hybrid-trained LQR outperforms alternatives while significantly reducing tuning time and testing costs. The results confirm the proposed digital twin framework as a promising tool for enhancing the efficiency, reliability, and scalability of UAV control algorithm development.
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