Active Sidestick Control Integration for Enhanced Aircraft Flight Envelope Protection
Fuente:
arXiv
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| Autores principales: | , , , , , , |
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| Formato: | Preprint |
| Publicado: |
2024
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| Materias: | |
| Acceso en línea: | |
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| _version_ | 1866909222127534080 |
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| author | Altunkaya, Çağrı Ege Erol, Fatih Çatak, Akın Mert, Volkan Capone, Pierluigi Ertürk, Şükrü Akif Koyuncu, Emre |
| author_facet | Altunkaya, Çağrı Ege Erol, Fatih Çatak, Akın Mert, Volkan Capone, Pierluigi Ertürk, Şükrü Akif Koyuncu, Emre |
| contents | 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. |
| format | Preprint |
| id |
arxiv_https___arxiv_org_abs_2406_07690 |
| institution | arXiv |
| publishDate | 2024 |
| record_format | arxiv |
| spellingShingle | Active Sidestick Control Integration for Enhanced Aircraft Flight Envelope Protection Altunkaya, Çağrı Ege Erol, Fatih Çatak, Akın Mert, Volkan Capone, Pierluigi Ertürk, Şükrü Akif Koyuncu, Emre Systems and Control 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. |
| title | Active Sidestick Control Integration for Enhanced Aircraft Flight Envelope Protection |
| topic | Systems and Control |
| url | https://arxiv.org/abs/2406.07690 |