Virtual flight test of pitch and roll attitude control based on circulation control of tailless flying wing aircraft without rudders-Reference-Cited by-同舟云学术

Virtual flight test of pitch and roll attitude control based on circulation control of tailless flying wing aircraft without rudders

Published:2023-06 Issue:6 Volume:36 Page:52-62
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

ZHANG Liu,HUANG Yong,ZHU Zhenglong,GAO Lihua,CHEN Fuzheng,WU Fuzhang,HE Meng

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference24 articles.

1. Comprehensive study on yaw control characteristic of combined control surfaces of flying wing configuration;Zhou;Acta Aeronautica et Astronautica Sinica,2020

2. A multi-disciplinary global/local optimization method for flying-wing airfoils design;Zhang;Acta Aerodynamica Sinica,2021

3. Attitude control of flying wing aircraft without control surfaces based on active flow control;Sun;Acta Aeronautica et Astronautica Sinica,2020

4. Fluidic flow control effectors for flight control;Warsop;AIAA J,2018

5. Circulation control as a roll effector for unmanned combat aerial vehicles;Hoholis;J Aircr,2016

Cited by 10 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Numerical virtual flight investigation for longitudinal maneuver of a generic fighter based on machine learning;Physics of Fluids;2024-07-01

2. Coupled funnel control for supersonic tailless aerial vehicle on penetrating counter air;CHINESE J AERONAUT;2024

3. Coupled funnel control for supersonic tailless aerial vehicle on penetrating counter air;Chinese Journal of Aeronautics;2024-07

4. Time-delay effect and design of closed-loop control system of circulation control airfoil;Chinese Journal of Aeronautics;2024-06

5. Dynamic characteristics and application of dual throat fluidic thrust vectoring nozzle;Chinese Journal of Aeronautics;2024-04