High Maneuverability and Efficiency Control for Hybrid Quadrotor With All-Moving Wings in SE(3) Based on Deep Reinforcement Learning
This article introduces a novel composite aerial vehicle configuration called hybrid quadrotor with all-moving wings (HQWAW), consisting of a conventional quadrotor combined with two independently all-moving wings. A nonlinear geometric controller in the special Euclidean group SE(3) is proposed as the basic controller for the HQWAW, achieving high maneuverability and energy-efficient flight. Lyapunov stability criterion is used to prove that the proposed control scheme can track the reference trajectory almost globally ultimately uniformly bounded. A deep reinforcement learning compensator, based on the twin delayed deep deterministic policy gradient algorithm, is designed to fine-tune all-moving wing angles, ensuring that wing surfaces remain at optimal angles, thereby maximizing aerodynamic efficiency and reducing rotor consumption. Tracking results for a trajectory involving high-speed dive followed by spiral ascent demonstrate that the proposed algorithm achieves both high maneuverability and improved energy efficiency of the HQWAW.
Authors
- Jixiao Liu (ORCID: https://orcid.org/0000-0002-0355-9980)
- Fulin Song (ORCID: https://orcid.org/0000-0001-6373-9791)
- Xinghu Yu (ORCID: https://orcid.org/0000-0001-8181-6199)
- Juan J. Rodríguez-Andina (ORCID: https://orcid.org/0000-0002-0919-1793)
- Zhan Li (ORCID: https://orcid.org/0000-0002-7601-4332)
Institutions
- Harbin Engineering University (CN)
- Harbin Institute of Technology (CN)
- Universidade de Vigo (ES)
Publication Details
- Journal
- IEEE Transactions on Industrial Informatics
- Published
- 2024-11-07
- DOI
- https://doi.org/10.1109/tii.2024.3485790
- Citations
- 1
- Primary Topic
- Real-time simulation and control systems
- Type
- article
- Field-Weighted Citation Impact
- 0.33
Funders
- National Natural Science Foundation of China
- Natural Science Foundation of Heilongjiang Province