Nonlinear L1 adaptive control of stagnation pressure in a cryogenic wind tunnel

Author:

Zhu RusongORCID,Xie Mingwei,Liao Daxiong,Tang Gengsheng,Gai Wen

Abstract

AbstractCryogenic wind tunnel is a sophisticated aerodynamics ground test facility, which operates in cryogenic temperature with injection of liquid nitrogen. The multi-variable, nonlinear and coupled dynamics existing between the temperature, pressure and Mach number in the tunnel, poses great challenges for the effective control of the tunnel. L1 adaptive control is a new control methodology developed in recent years with good robustness properties, which has good potentials to address these challenges. But this control method does not provide full adaptive feedforward control in its generic structure. In the paper, adaptive feedforward control action is introduced into the standard L1 adaptive control architecture for nonlinear systems in the presence of matched un-modeled dynamics. This new control structure is applied to the stagnation pressure control in a cryogenic wind tunnel, which could also be used for the control of temperature and Mach number in the tunnel. This new method could effectively compensate known disturbances with linear gain uncertainty, which occur in the nonlinear systems, while retaining the closed-loop control performance of L1 adaptive control. After the proof and discussions on the stability of this method, simulations of the stagnation pressure control in the wind tunnel are presented. The results and analysis demonstrate the effectiveness of the proposed control architecture.

Publisher

Springer Science and Business Media LLC

Reference24 articles.

1. Goodyer MJ, Kilgore RA (1973) High-Reynolds-number cryogenic wind tunnel. AIAA J 11(5):613–619. https://doi.org/10.2514/3.50500

2. Balakrishna S, Kilgore W, Thibodeaux J (1992) “Control of large cryogenic tunnels,” 28th Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics

3. Armstrong ES, Tripp JS, Aeronautics USN, Scientific SA, Branch TI, Center LR (1981) An application of multivariable design techniques to the control of the National Transonic Facility: National Aeronautics and Space Administration, Scientific and Technical Information Branch

4. Gobert J (1994) “ETW control system - design and first results,” 25th Plasmadynamics and Lasers Conference. American Institute of Aeronautics and Astronautics

5. Paryz R (2011) “Recent developments at the NASA Langley research center national transonic facility,” 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, p 877

Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3