The design of total pressure control strategy for 0.6m continuous transonic wind tunnel
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摘要: 总压作为连续式风洞控制系统关键指标之一,其控制精度及快速性对提高风洞试验效率、降低能耗具有重要意义。0.6m风洞为国内首座具备负压试验能力的连续式跨声速风洞,其试验工况多,压力范围广,针对该风洞压力特性,设计了总压控制策略,根据不同的压力工况确定不同的阀门组合控制方式;同时针对模糊PID对连续式跨声速风洞宽压力范围、多调节工况下压力控制适应性较差的问题,提出分段变参数加模糊PID相结合的控制算法,即先根据目标总压确定不同分段区间下基本合理的基准P、I参数,再结合模糊控制算法对基准参数进行修正。风洞调试结果表明,总压控制精度优于0.1%,控制策略能够有效满足不同工况的控制要求。Abstract: The total pressure is one of the key indicators of the continuous tunnel control system, the control precision and speed of which are very important to improve the efficiency of wind tunnel test and reduce energy consumption. The 0.6m wind tunnel is the first domestic continuous transonic wind tunnel with the negative pressure test ability, which can provide lots of test conditions covering wide total pressures. Based on its pressure condition, the total pressure control strategy is designed, and the different control ways of valve combination are ascertained depending on the different pressure conditions. Meanwhile, the control algorithm of segmented parameters combining with the fuzzy PID is proposed, to improve the poor adaptability of fuzzy PID to the wide pressure range and multi-adjustment condition in continuous transonic wind tunnels. In our algorithm, the reasonable benchmark parameters P and I under the different segmentation interval due to the target total pressure should been determined firstly. Then it would been modified by fuzzy control algorithm. The result shows that the total pressure control accuracy is better than 0.1%, and the control strategy can adapt to the control requirement of different working conditions.
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表 1 阀门控制系统
参数 Table 1.
parameter of valve control system E EC NB NM NS 0 PS PM PB NB PB/NL PB/NL PB/NM PB/NM PB/NS PS/0 PS/0 NM PB/NB PB/NB PB/NM PB/NS PB/NS 0/0 0/0 NS PM/NM PM/NM PM/NS PS/NS 0/0 NS/PS NS/PS ZP PS/NS PS/NS PS/NS 0/0 NS/PS NM/PM NM/PM ZN NP/PS NP/PS PS/NS 0/0 NS/PS PM/PS PM/PS PS NS/NS NS/NS 0/0 NS/PS NS/PS PM/PS PM/PS PM 0/0 0/0 NS/PS NM/PS NM/PM PB/NB PB/NB PB PS/0 PS/0 NM/PS NM/PM NM/PM PB/NL PB/NL -
[1] 张永双, 陈旦, 陈娇. NF-6连续式跨声速风洞马赫数控制方式比较与研究[J]. 实验流体力学, 2013, 27(2): 95-99. http://www.syltlx.com/CN/abstract/abstract10340.shtmlZhang Y S, Chen D, Chen J. Comparison and research on the Mach number control methods for the NF-6 continuous transonic wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2013, 27(2): 95-99. http://www.syltlx.com/CN/abstract/abstract10340.shtml [2] 郝礼书, 乔志德, 张永双, 等. NF-6风洞马赫数闭环控制系统设计研究[J]. 实验流体力学, 2010, 24(4): 85-88. http://www.syltlx.com/CN/abstract/abstract9851.shtmlHao L S, Qiao Z D, Zhang Y S, et al. Design research on the Mach number closed-loop control system in the NF-6 wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2010, 24(4): 85-88. http://www.syltlx.com/CN/abstract/abstract9851.shtml [3] Jonathan R Potts1, Ian Lunnon, William J Crowther. Development of a transonic wind tunnel test bed for MEMS flow control actuators and sensors[R]. AIAA-2009-319, 2009. [4] Nhan Nguyen, Mark Ardema. Adjoint method and predictive control for 1-D flow in NASA ames 11-foot transonic wind tunnel[R]. AIAA-2006-1433, 2006. http://cn.bing.com/academic/profile?id=2072608735&encoded=0&v=paper_preview&mkt=zh-cn [5] Edward J Mickle, Capt Carmen Evans. Restoration of AEDC's 16-ft transonic propulsion test capability[R]. AIAA-2005-7614, 2005. [6] Tirres C, Baxter L E. AEDC test facility planning "toward new horizons" to today[R]. AIAA-2004-2731, 2004. [7] 廖达雄, 陈吉明, 彭强, 等. 连续式跨声速风洞设计关键技术[J]. 实验流体力学, 2011, 25(4): 74-78. http://www.syltlx.com/CN/abstract/abstract10640.shtmlLiao D X, Chen J M, Peng Q, et al. Key design techniques of the low noise continuous transonic wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2011, 25(4): 74-78. http://www.syltlx.com/CN/abstract/abstract10640.shtml [8] 连晓飞. 基于遗传算法优化BP网络的风洞马赫数控制研究[D]. 沈阳: 东北大学, 2011. http://cdmd.cnki.com.cn/article/cdmd-10141-2009040779.htmLian X F. Wind tunnel mach number control based on genetic algorithm optimized bp-neural network[D]. Shenyang: Northeastern University, 2011. http://cdmd.cnki.com.cn/article/cdmd-10141-2009040779.htm [9] 高川, 周波, 蒋婧妍, 等. 基于labview的大型超声速风洞总压测控系统设计与应用[J]. 测控技术, 2014, 33(8): 84-87. http://www.cnki.com.cn/Article/CJFDTOTAL-IKJS201408022.htmGao C, Zhou B, Jiang J Y, et al. Design and implementation of total pressure measurement and control system of large-scare supersonic wind tunnel based on LabVIEW[J]. Measurement & Control Technology, 2014, 33(8): 84-87. http://www.cnki.com.cn/Article/CJFDTOTAL-IKJS201408022.htm [10] 芮伟, 易凡, 杜宁, 等. 2.4m跨声速风洞颤振试验流场控制技术研究[J]. 实验流体力学, 2012, 26(6): 83-86. http://www.syltlx.com/CN/abstract/abstract10483.shtmlRui W, Yi F, Du N, et al. Study on flow field control technique of flutter test in 2. 4m transonic wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2012, 26(6): 83-86. http://www.syltlx.com/CN/abstract/abstract10483.shtml [11] 褚卫华, 汤更生, 王帆. 2m×2m超声速风洞流场控制策略研究与实现[J]. 实验流体力学, 2012, 26(5): 98-102. http://www.syltlx.com/CN/abstract/abstract10506.shtmlChu W H, Tang G S, Wang F. Research and realization on the control strategies of the 2m×2m supersonic wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2012, 26(5): 98-102. http://www.syltlx.com/CN/abstract/abstract10506.shtml [12] 李可, 刘旺开, 王浚. 专家_模糊PID在低速风洞风速控制系统中的应用[J]. 北京航空航天大学学报, 2007, 33(12): 1387-1390. http://www.cnki.com.cn/Article/CJFDTOTAL-BJHK200712003.htmLi K, Liu W K, Wang J. Parameters self-tuning fuzzy-PID combined with expert control on wind velocity control system of wind tunnels at home[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(12): 1387-1390. http://www.cnki.com.cn/Article/CJFDTOTAL-BJHK200712003.htm [13] 杨海滨, 张伟, 罗承友, 等. 模糊控制在风洞主气流压力自动调节系统中的应用[J]. 兵工自动化, 2015, 34(4): 39-43. http://www.cnki.com.cn/Article/CJFDTOTAL-BGZD201504012.htmYang H B, Zhang W, Luo C Y, et al. Application of fuzzy control in wind tunnel main airflow pressure auto-adjust system[J]. Ordnance Industry Automation, 2015, 34(4): 39-43. http://www.cnki.com.cn/Article/CJFDTOTAL-BGZD201504012.htm [14] 张永双. 某型连续式跨声速风洞测控系统初步设计方案[R]. 中国空气动力研究与发展中心, 2008. http://www.cnki.com.cn/article/cjfdtotal-jxkx201404001.htmZhang Y S. The design scheme of measurement and control system for one type of continuous transonic wind tunnel[R]. China Aerodynamics Research and Development Center, 2008. http://www.cnki.com.cn/article/cjfdtotal-jxkx201404001.htm [15] 陈旦. 某型连续式跨声速风洞阀门控制系统技术设计[R]. 中国空气动力研究与发展中心, 2012.Chen D. The technological design of measurement and control system for one type of continuous transonic wind tunnel[R]. China Aerodynamics Research and Development Center, 2012. [16] 安延涛. 大型压力调节阀的动态分析及故障检测研究[D]. 山东: 山东大学, 2012. http://www.cnki.com.cn/article/cjfdtotal-gzha201008091.htmAn Y T. Dynamic analysis and fault detection of large pressure control valve[D]. Shandong: Shan dong University, 2012. http://www.cnki.com.cn/article/cjfdtotal-gzha201008091.htm [17] 明赐东. 调节阀计算选型使用[M]. 成都: 成都科技大学出版社, 1999.Ming C D. Adjusting valve calculation lectotype use[M]. Chengdu: Chengdu University of Science & Technology publishing house, 1999. [18] 国防科工委. GJB 1179-91. 高速风洞和低速风洞流场品质规范[S]. 北京, 1992.State Commission of Science and Technology for National Defense Industry. GJB 1179-91. Specification for flow quality of high and low speed wind tunnels[S]. Beijing, 1992. [19] 陈吉明, 柳新民, 张永双. 某型连续式跨声速风洞设计技术总结[R]. 中国空气动力研究与发展中心, 2015.Chen J M, Liu X M, Zhang Y S. The summarization of design for one type of continuous transonic wind tunnel[R]. China Aerodynamics Research and Development Center, 2015. [20] 总装备部. GJB 5221-2004. 风洞控制系统设计及检定准则[S]. 北京, 2004.General Armament Department. GJB 5221-2004. Design and calibration criteria of control systems for wind tunnels[S]. Beijing, 2004.