Computer Simulation Research of Self-adaptive Compensation Control Based on Neural Network for Control Surface Failure of Uncertain Tailless Flying Wing Aircraft-Reference-Cited by-同舟云学术

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Computer Simulation Research of Self-adaptive Compensation Control Based on Neural Network for Control Surface Failure of Uncertain Tailless Flying Wing Aircraft

Published:2022 Issue: Volume:208 Page:347-353
ISSN:1877-0509
Container-title:Procedia Computer Science
language:en
Short-container-title:Procedia Computer Science

Author:

Shi Xianzhu,Wu Shuang

Publisher

Elsevier BV

Subject

General Engineering

Reference14 articles.

1. The study of concept design criteria for large-scale passenger aircraft with new technologies;Song;Acta Aeronaut. Astronaut. Sin.,2008

2. Flying Wings and Tailless Aircraft;Rose;Midland,2010

3. Conceptual design for a laminar-flying-wing aircraft;Saeed,2012

4. Summary for control method of flying wing UAV;Meng;Aerodyn. Missile J.,2015

5. Predictions of stability and control for a flying wing;Tomac;Aerosp. Sci. Technol.,2014

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