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Journal: Applied SciencesVolume: 13Number: 12225
Article: Control Design for Soft Transition for Landing Preparation of Light Compound-Wing Unmanned Aerial Vehicles Based on Incremental Nonlinear Dynamic Inversion
  • Authors:
  • Zheng Ye1,2,
  • Yongliang Chen1,2,* and
  • Pengcheng Cai1,2
  • et al.
Link: https://www.mdpi.com/2076-3417/13/22/12225

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