A Novel Engine Fault-Tolerant Control Method Based on Input Scheduling for Tiltrotor Aircraft-Reference-Cited by-同舟云学术

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A Novel Engine Fault-Tolerant Control Method Based on Input Scheduling for Tiltrotor Aircraft

Published:2024-07-10 Issue: Volume: Page:
ISSN:2093-274X
Container-title:International Journal of Aeronautical and Space Sciences
language:en
Short-container-title:Int. J. Aeronaut. Space Sci.

Author:

Guo Haoran^ORCID,Wang Yong,Peng Yerong,Li Shancheng,Zhang Haibo,Zhao Qijun

Funder

National Natural Science Foundation of China

National Science and Technology Major Project

Innovation Centre for Advanced Aviation Power

Fonden for Lægevidenskabelig Forskning for Fyns Amt

Postgraduate Research and Practice Innovation Program of NUAA

Publisher

Springer Science and Business Media LLC

Link

https://link.springer.com/content/pdf/10.1007/s42405-024-00770-0.pdf

Reference27 articles.

1. Biggi M, Nour PA, Vicenzotti G (2024) Next generation civil tiltrotor technology demonstrator program: towards flight test. In: AIAA SCITECH 2024 Forum,

2. Wu X (2015) Current situation, trend and countermeasures of high-speed helicopter development. J Nanjing Univ Aeronaut Astron 47(2):173–179. https://doi.org/10.16356/j.1005-2615.2015.02.001

3. Appleton W (2023) Tiltrotor aeromechanics. Lecture Notes in Rotorcraft Engineering. Springer International Publishing, Cham, pp 115–139

4. Luo K, Shi S, Peng C (2023) Smooth tracking control for conversion mode of a tilt-rotor aircraft with switching modeling. Front Inf Technol Electron Eng 24(11):1591–1600

5. Wu X, Mou X (2021) Key technologies and future development and assumption of helicopters. J Aerodyn 39(3):1–10. https://doi.org/10.7638/kqdlxxb-2021.0042

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