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Fuzzy adaptive fixed-time fault-tolerant attitude tracking control for tailless flying wing aircrafts

  • Published:2022-11 Issue: Volume:130 Page:107950
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Hou YueqiORCID,Lv MaolongORCID,Liang Xiaolong,Yang Aiwu

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference46 articles.

1. Tailless aircraft control allocation;Buffington,1997

2. Passive gust alleviation of a flying-wing aircraft by analysis and wind-tunnel test of a scaled model in dynamic similarity;He;Aerosp. Sci. Technol.,2021

3. A novel yaw control method for flying-wing aircraft in low speed regime;Qu;Aerosp. Sci. Technol.,2017

4. Incremental nonlinear control allocation for a tailless aircraft with innovative control effectors;Cid,2018

5. Challenges and opportunities in tailless aircraft stability and control;Bowlus,1997

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