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Full mode flight dynamics modelling and control of stopped-rotor UAV

  • Published:2022-10 Issue:10 Volume:35 Page:95-105
  • ISSN:1000-9361
  • Container-title:Chinese Journal of Aeronautics
  • language:en
  • Short-container-title:Chinese Journal of Aeronautics

Author:

HE Ao,GAO Honggang,ZHANG Shanshan,GAO Zhenghong,MA Bodi,CHEN Lulu,DAI Wei

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference25 articles.

1. Modelling and transition flight control of vertical take-off and landing unmanned tri-tilting rotor aerial vehicle;Hegde,2019

2. Extended state observer based smooth switching control for tilt-rotor aircraft;Zou;J Syst Eng Electron,2020

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

4. Comprehensive sizing and optimization method for series-hybrid unmanned convertiplane;Chen;Chin J Aeronaut,2021

5. A multi-strategy pigeon-inspired optimization approach to active disturbance rejection control parameters tuning for vertical take-off and landing fixed-wing UAV;He;Chin J Aeronaut,2022

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