Active Sidestick Control Integration for Enhanced Aircraft Flight Envelope Protection
<|reference_start|>Active Sidestick Control Integration for Enhanced Aircraft Flight Envelope Protection: The design of Envelope and Pilot-Induced Oscillation (PIO) Protection Features, and Failure Cases detection and prevention using Active Control Sidestick (ACS) is a challenging task. While helping the pilot to respect the envelope limitations also in failure scenarios and, therefore, increasing mission effectiveness, these features may have a significant impact on the aircraft's agility. ACS characteristics are investigated in an integrated environment. A set of effective and flexible control laws based on Incremental Nonlinear Dynamic Inversion have been developed in a state-of-the-art aircraft simulation model and coupled with a two-ways communication with the selected ACS. The model can run in real-time in a fixed-based simulator composed of representative cockpit and out-of-the-window.<|reference_end|>
@article{altunkaya2024active,
    title={Active Sidestick Control Integration for Enhanced Aircraft Flight
  Envelope Protection},
    author={c{C}au{g}r{i} Ege Altunkaya, Fatih Erol, Ak{i}n c{C}atak, Volkan
  Mert, Pierluigi Capone, c{S}"ukr"u Akif Ert"urk, Emre Koyuncu},
    journal={arXiv preprint arXiv:2406.07690},
    year={2024},
    archivePrefix={arXiv},
    eprint={2406.07690},
    primaryClass={eess.SY cs.SY}
}