Design of Automatic Carrier-Landing Controller Based on Compensating States and Dynamic Inversion

Design of Automatic Carrier-Landing Controller Based on Compensating States and Dynamic Inversion

In this paper, a design scheme of automatic carrier landing system (ACLS) control law based on compensating states and dynamic inversion is proposed, in order to eliminate landing risk and air wake disturbance and improve flight quality during landing. First of all, the mathematical model for an air...

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Bibliographic Details
Main Authors: Lipeng Wang, Zhi Zhang, Qidan Zhu, Zixia Wen
Format: Article
Language:English
Published: IEEE 2019-01-01
Series:IEEE Access
Subjects:
Automatic carrier landing system
nonlinear dynamic inverse
compensating states
landing risk
air wake
Online Access:https://ieeexplore.ieee.org/document/8717581/

Internet

https://ieeexplore.ieee.org/document/8717581/

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