Study of RCS characteristics of tilt-rotor aircraft based on dynamic calculation approach-Reference-Cited by-同舟云学术

Study of RCS characteristics of tilt-rotor aircraft based on dynamic calculation approach

Published:2022-04 Issue:4 Volume:35 Page:426-437
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

ZHOU Zeyang,HUANG Jun

Funder

China Postdoctoral Science Foundation

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference29 articles.

1. Application of improved active disturbance rejection control algorithm in tilt quad rotor;Wang;Chin J Aeronaut,2020

2. Yan XF, Chen RL. Control strategy optimization of dynamic conversion procedure of tilt-rotor aircraft. Acta Aeronaut et Astronaut Sin 2017;38(7):520865 Chinese.

3. Influence of rotor dynamic scattering on helicopter radar cross-section;Zhou;Sensors,2020

4. CFD calculations on the unsteady aerodynamic characteristics of a tilt-rotor in a conversion mode;Li;Chin J Aeronaut,2015

5. Comprehensive optimization of aerodynamic noise and radar stealth for helicopter rotor based on Pareto solution;Zhou;Aerosp Sci Technol,2018

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