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Dynamic Inversion Flight Control Laws for Autonomous Transition of Tilt-Rotor Aircraft



Dynamic Inversion Flight Control Laws for Autonomous Transition of Tilt-Rotor Aircraft

  • 14 pages
  • SKU # : sm-2024-ICAAMS-S4-17-Saetti
  • April 2025 Paper of the Month
    Session 4: Systems 1

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Dynamic Inversion Flight Control Laws for Autonomous Transition of Tilt-Rotor Aircraft

Authors / Details: Umberto Saetti, University of Maryland