Autonomous Suspended-Payload UAV with Self-Sensing and Anti-Swing for Outdoor Transportation
Suspended-payload UAVs face a core dilemma in outdoor transportation: their stability is severely compromised by payload swing, yet conventional anti-swing controllers depend on real-time state feedback that is difficult to obtain without external sensors. To resolve this, we propose a fully integrated self-sensing anti-swing control strategy. Its key contribution lies in the seamless co-design of an external-sensor-free autonomous state estimation scheme and a coupled compensation control architecture: it eliminates the dependency on external sensors through an onboard estimation solution, actively suppresses swing via a coupled compensation framework, and rigorously guarantees stability through Lyapunov analysis. Specifically, an inertial measurement unit (IMU) at the suspension point fuses data with a Kalman filter for real-time payload state estimation. A sliding mode anti-swing controller is then integrated into the position control loop through dynamic coupling compensation. Strict Lyapunov-based analysis proves the bounded-error stability of this coupled system. High-fidelity simulations in CoppeliaSim under various scenarios validate the strategy’s engineering feasibility and synergistic performance. Results demonstrate that our method achieves high-precision state estimation and effective swing suppression, offering a practical and reliable solution for outdoor UAV transportation.
Authors
- Haoyang Lin (ORCID: https://orcid.org/0009-0004-9525-662X)
- Zhenyu Song (ORCID: https://orcid.org/0000-0002-6163-0503)
- Qi Shan
- Hongbo Zhang (ORCID: https://orcid.org/0000-0001-7865-5670)
- Chao Liu (ORCID: https://orcid.org/0000-0001-7953-5144)
- Shengyi Yang (ORCID: https://orcid.org/0000-0002-3956-4888)
Institutions
- Guizhou Minzu University (CN)
Publication Details
- Journal
- Aerospace
- Published
- 2025-11-16
- DOI
- https://doi.org/10.3390/aerospace12111016
- Primary Topic
- Adaptive Control of Nonlinear Systems
- Type
- article
- Field-Weighted Citation Impact
- 0.00