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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 JiangBeihang UniversityDLDaochun LiBeijing City UniversityZKZi KanBeihang University

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Implication

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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Also Consider

Synapse has enriched 5 closely related papers on similar clinical questions. Consider them for comparative context:

  1. 1Design and Implementation of an Incremental Nonlinear Dynamic Inversion (INDI) based Control Law for a Quad-plane UAV2024 · 1 citations
  2. 2Design and Wind Tunnel Test of Control Laws for High Angle of Attack Flight of Low-Aspect-Ratio Flying-Wing UAVs Based on NDI2026
  3. 3INDI control for the take-off and landing phases of an eVTOL2026
  4. 4Contributions to Incremental Nonlinear Dynamic Inversion for Flight Control2026
  5. 5Adaptive Incremental Nonlinear Dynamic Inversion Control for Aerial Manipulators2024 · 13 citations