Genetic Algorithm Based Parameter Tuning for Robust Control of Launch Vehicle in Atmospheric Flight

Genetic Algorithm Based Parameter Tuning for Robust Control of Launch Vehicle in Atmospheric Flight

A hybrid approach to the design of the attitude control system for a launch vehicle (LV) in the atmospheric flight phase is proposed in this paper, where a structured <inline-formula> <tex-math notation="LaTeX">$\mathcal {H}_\infty $ </tex-math></inline-formula> con...

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Bibliographic Details
Main Authors: Jose Pablo Belletti Araque, Alessandro Zavoli, Domenico Trotta, Guido De Matteis
Format: Article
Language:English
Published: IEEE 2021-01-01
Series:IEEE Access
Subjects:
Robust control
genetic algorithm
launch vehicle
attitude dynamics
Online Access:https://ieeexplore.ieee.org/document/9492099/

Internet

https://ieeexplore.ieee.org/document/9492099/

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