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Aggressive flight control of quadrotors using incremental nonlinear dynamic inversion with a high-fidelity thrust unit model.

Zeliang WuJianchuan YeTao SongTao JiangXiaojie Su
Published in: J. Frankl. Inst. (2024)
Keyphrases
  • high fidelity
  • nonlinear dynamics
  • mathematical model
  • experimental data
  • neural network
  • video sequences
  • image compression