Trajectory-Tracking Controller Design of Rotorcraft Using an Adaptive Incremental-Backstepping Approach
This paper treats a robust adaptive trajectory-tracking control design for a rotorcraft using a high-fidelity math model subject to model uncertainties. In order to control the nonlinear rotorcraft model which shows strong inter-axis coupling and high nonlinearity, incremental backstepping approach...
Gardado en:
| Principais autores: | , , , |
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| Formato: | Artigo |
| Idioma: | Inglês |
| Publicado: |
MDPI AG
2021-09-01
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| Series: | Aerospace |
| Assuntos: | |
| Acceso en liña: | https://www.mdpi.com/2226-4310/8/9/248 |
| Tags: |
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