An intelligent control method based on artificial neural network for numerical flight simulation of the basic finner projectile with pitching maneuver-Reference-Cited by-同舟云学术

An intelligent control method based on artificial neural network for numerical flight simulation of the basic finner projectile with pitching maneuver

Published:2024-02 Issue: Volume:32 Page:663-674
ISSN:2214-9147
Container-title:Defence Technology
language:en
Short-container-title:Defence Technology

Author:

Liang Yiming^ORCID,Li Guangning,Xu Min,Zhao Junmin,Hao Feng,Shi Hongbo

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Reference28 articles.

1. Numerical virtual flight simulation of quasi-cobra maneuver of a fighter aircraft;Wang;J Aircraft,2020

2. Digital Flight: the last CFD aeronautical grand challenge;Salas;J Sci Comput,2006

3. Validation of numerical virtual flight system with wind-tunnel virtual flight testing;Zhang;AIAA J,2020

4. Achievements and predicaments of CFD in aeronautics in past forty years;Yan;Acta Aeronautica Astronautica Sinica,2022

5. Review of aerodynamics/kinematics/flight-control coupling methods in virtual flight simulations;Zhang;Advances in Mechanics,2014

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3. Comparison of Machine Learning and Classic Methods on Aerodynamic Modeling and Control Law Design for a Pitching Airfoil;International Journal of Aerospace Engineering;2024-01