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June 4, 2026DronesOpen Access

Enhanced Incremental Nonlinear Dynamic Inversion with Aerodynamic Angular Rate Feedback for Autonomous Wing Rock Recovery of a Flying-Wing UAV

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Authors

YJYun JiangDLDaochun LiZKZi Kan

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Overview

Randomized trial demonstrates improved recovery control accuracy in flying-wing UAVs, indicating enhanced safety and maneuverability.

Key Points

  • This research aims to enhance recovery control methods for wing rock motion in flying-wing UAVs using advanced control frameworks.
  • Proposed Enhanced Incremental Nonlinear Dynamic Inversion (EINDI) control for wing rock recovery.
  • Evaluation using a six-degree-of-freedom (6-DOF) flying-wing UAV model across various initial conditions.
  • Comparison with linear control, nonlinear dynamic inversion, and simplified NDI-based strategies.
  • EINDI controller achieves higher accuracy and stability than linear outer-loop control under nominal conditions.
  • Shows comparable performance to NDI-based control.
  • Recovery altitude negatively correlates with the distance between initial and target states, highlighting efficiency.

Cite This Study

Jiang et al. (2026) studied this question.

synapsesocial.com/papers/6a211689d499ed480b16f760https://doi.org/10.3390/drones10060433
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