Pressure regulation inside a hypersonic wind tunnel using H-infinity optimization control
- 作者: Rajani S.H.1, Krishna B.M.2, Nair U.1
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隶属关系:
- School of Engineering
- Sophisticated Test and Instrumentation Center
- 期: 卷 51, 编号 6 (2017)
- 页面: 399-409
- 栏目: Article
- URL: https://journals.rcsi.science/0146-4116/article/view/174963
- DOI: https://doi.org/10.3103/S0146411617060074
- ID: 174963
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详细
Hypersonic wind tunnel is a ground-based facility used to study the aerodynamic properties of space vehicles during re-entry. This paper aims at designing an H-infinity controller with krill herd optimization algorithm to regulate pressure inside the settling chamber of a hypersonic wind tunnel. The krill herd algorithm is a novel stochastic algorithm for improving the performance characteristics by optimizing the H-infinity controller parameters. The proposed algorithm minimizes the H-infinity norms by tuning the controller weighing function parameters. The dynamic characteristics of the settling chamber pressure with H-infinity and H-infinity control based on krill herd algorithm is studied by numerical simulations. The proposed algorithm is highly efficient and robust in controlling the settling chamber pressure in terms of performance parameters.
作者简介
S. Rajani
School of Engineering
编辑信件的主要联系方式.
Email: rajaniiyer00@gmail.com
印度, Kochi, 682022
Bindu Krishna
Sophisticated Test and Instrumentation Center
Email: rajaniiyer00@gmail.com
印度, Kochi, 682022
Usha Nair
School of Engineering
Email: rajaniiyer00@gmail.com
印度, Kochi, 682022
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