Abstract
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.
| Original language | English |
|---|---|
| Pages (from-to) | 1645-1654 |
| Number of pages | 10 |
| Journal | IEEE Transactions on Industrial Informatics |
| Volume | 21 |
| Issue number | 2 |
| DOIs | |
| State | Published - 2025 |
UN SDGs
This output contributes to the following UN Sustainable Development Goals (SDGs)
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SDG 7 Affordable and Clean Energy
Keywords
- Deep reinforcement learning (DRL)
- geometric control in SE(3)
- high maneuverability and energy-efficiency
- hybrid quadrotor with all-moving wings (HQWAW)
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