Abstract
A novel practical predefined-time sliding mode control strategy is proposed for the flight formation of a small tandem-rotor wheeled UAV (TRW-UAV) with unknown upper bound external disturbances and uncertainties in this paper. Firstly, a new predefined-time sliding mode surface is proposed to guide all errors of the position and velocity loops to converge to the origin in a predefined-time. Furthermore, a dynamic surface control approach is utilized to circumvent the higher-order differentiation when controlling the actuator loop. Secondly, a predefined-time adaptive law is designed for estimating external disturbances and uncertainties during the controller design process to construct a distributed practical predefined-time formation cooperative control strategy. Thirdly, a novel practical predefined-time criterion is utilized to rigorously demonstrate the stability of the proposed control strategy. Finally, the simulation results indicate that the proposed control strategy can deliver the practical predefined-time control when there are external disturbances and model uncertainties, and with higher convergence accuracies compared to some of the existing methods.
| Original language | English |
|---|---|
| Pages (from-to) | 575-588 |
| Number of pages | 14 |
| Journal | ISA Transactions |
| Volume | 167 |
| DOIs | |
| State | Published - Dec 2025 |
Keywords
- Adaptive law
- Dynamic surface control
- Formation cooperative control
- Practical predefined-time control
- Tandem-rotor wheeled UAV
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