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Three-axis coupled flight control law design for flying wing aircraft using eigenstructure assignment method

  • Published:2020-10 Issue:10 Volume:33 Page:2510-2526
  • ISSN:1000-9361
  • Container-title:Chinese Journal of Aeronautics
  • language:en
  • Short-container-title:Chinese Journal of Aeronautics

Author:

WANG Lixin,ZHANG Ning,YUE Ting,LIU Hailiang,ZHU Jianghui,JIA Xiaopeng

Funder

Fundamental Research Funds for the Central Universities of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference37 articles.

1. Effective design of highly maneuverable tailless aircraft;Colgren;J Aircraft,2008

2. Study on longitudinal stability improvement of flying wing aircraft based on synthetic jet flow control;Xu;Aerosp Sci Technol,2015

3. Dihedral influence on lateral–directional dynamic stability on large aspect ratio tailless flying wing aircraft;Song;Chin J Aeronaut,2014

4. Lateral stability and control of a tailless aircraft configuration;Stenfelt;J Aircraft,2009

5. Design of innovative control surfaces of flying wing aircrafts with large ratio aspect;Ma;J Beijing Univ Aeronaut Astronaut,2007

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1. A Review of Control Methods for Tailless Aircraft;Guidance, Navigation and Control;2024-08-30

2. Longitudinal Attitude Control and Stability Analysis for a Low Aspect Ratio Flying Wing UAV at High Angle of Attack;International Journal of Aerospace Engineering;2024-01

3. Novel yaw effector of a flying wing aircraft based on reverse dual synthetic jets;Chinese Journal of Aeronautics;2023-12

4. Flight control of a flying wing aircraft based on circulation control using synthetic jet actuators;Chinese Journal of Aeronautics;2023-10

5. Model-Reference Sliding Mode Fault Tolerant Control of a Scale Model HALE UAV;2023 8th International Conference on Instrumentation, Control, and Automation (ICA);2023-08-09
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