Thrust vector V/STOL aircraft control based on angular acceleration estimation-Reference-Cited by-同舟云学术

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Thrust vector V/STOL aircraft control based on angular acceleration estimation

Published:2024-06 Issue: Volume:149 Page:109132
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Zhu Qi^ORCID,Lyu Yongxi^ORCID,Huang Shan,Shi Jingping,Qu Xiaobo,Liu Zhunga,Wang Zehao

Funder

Chinese Aeronautical Establishment Aeronautical Science Foundation

Shaanxi Province Natural Science Foundation

Shaanxi Key Laboratory of Flight Control and Simulation Technology

National Natural Science Foundation of China

Publisher

Elsevier BV

Reference24 articles.

1. Anderson S.B.. History overview of VSTOL aircraft technology. NASA -TM81280, (1981).

2. Modelling the effect of unsteady turbulent wakes on a short take-off and vertical landing (STOVL) aircraft;Watson,2019

3. Review of designs and flight control techniques of hybrid and convertible VTOL UAVs;Ducard;Aerosp. Sci. Technol.,2021

4. Holland M.A., D Gettinger. The drone revolution revisited. Center for the Study of the Drone at Bard College, (2016).

5. The Dream machine: The untold History of the Notorious V-22 Osprey;Whittle,2010

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