A Digital Twin-Level Modeling Framework for UAV Control Algorithm Optimization and Sim2real
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.
Authors
- Jiajing Tu
- Wanqi Gong (ORCID: https://orcid.org/0000-0002-4078-0748)
- Yong Chen (ORCID: https://orcid.org/0000-0002-5287-0767)
- Xunhua Dai
Institutions
- Central South University (CN)
Publication Details
- Journal
- Unmanned Systems
- Published
- 2025-11-20
- DOI
- https://doi.org/10.1142/s2301385027500464
- Citations
- 1
- Primary Topic
- Aerospace and Aviation Technology
- Type
- article
- Field-Weighted Citation Impact
- 4.99