Dynamic inversion- and neural network- based five-stage cascaded control for automatic carrier landing subject to multiple disturbances and uncertainties

This work proposes a novel control scheme for automatic carrier landing to enhance the landing precision and improve both the tracking of the reference trajectory and the touchdown accuracy. First, the nonlinear dynamics of the carrier-based aircraft is written under a five-stage cascaded strict fee...

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Veröffentlicht in:	Journal of the Franklin Institute Jg. 362; H. 9; S. 107719
Hauptverfasser:	Lungu, Mihai, Chen, Mou, Ebrahimpour, MohammadReza, Guo, Hongzhen
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	Elsevier Inc 01.06.2025
Schlagworte:	Airwake Automatic carrier landing system Dynamic inversion Neural network Uncertainty Airwake Uncertainty Neural network Dynamic inversion Automatic carrier landing system
ISSN:	0016-0032
Online-Zugang:	Volltext
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