Fuzzy Sliding Mode Predictive Control of Air Flow Rate for a High-Speed High-Temperature Heat-Airflow Test System-Reference-Cited by-同舟云学术

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Fuzzy Sliding Mode Predictive Control of Air Flow Rate for a High-Speed High-Temperature Heat-Airflow Test System

Published:2020-02-12 Issue:3 Volume:21 Page:806-815
ISSN:2093-274X
Container-title:International Journal of Aeronautical and Space Sciences
language:en
Short-container-title:Int. J. Aeronaut. Space Sci.

Author:

Cai Chaozhi^ORCID,Guo Lubin,Liu Jiachen

Funder

Natural Science Foundation of Hebei Province

Hebei Normal University of Science and Technology

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering

Link

http://link.springer.com/content/pdf/10.1007/s42405-020-00256-9.pdf

Reference24 articles.

1. Huang Q (2017) Future research of the hypersonic and space vehicle technology. Sci Technol Inf 15(31):76–77, 79

2. Cai C, Li Y, Dong S (2016) Experimental study on control of gas temperature for a high-speed heat-airflow wind tunnel. J Aerosp Eng 29(6):04016054

3. Li Y, Cai C, Lee KM, Teng F (2013) A novel cascade temperature control system for a high-speed heat-airflow wind tunnel. IEEE/ASME Trans Mechatron 18(4):1310–1319

4. Cai C, Yang Y, Liu T (2016) Coordinated control of fuel flow-rate for a high-temperature high-speed wind tunnel. Proc Inst Mech Eng G J Aerosp Eng 230(13):2504–2514

5. Cai C, Li Y (2014) Undisturbed switching control of fuel flow-rate for a high-speed heat-airflow wind tunnel. Proc Inst Mech Eng G J Aerosp Eng 228(12):2245–2254

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