期刊文献+

超燃冲压发动机燃烧室传感器最佳位置选择 被引量:3

Optimal sensor location of scramjet combustor
下载PDF
导出
摘要 超燃冲压发动机的燃烧控制和性能评估需要有效的燃烧室测量信息,而如何确定传感器的最佳位置和数量是非常重要的,要求选择最小的传感器数目和最佳的测量位置来较准确的描述燃烧室工作特性.这是一个组合优化问题,直接求解比较复杂.为此本文利用遗传算法对超燃冲压发动机燃烧室的测点位置和数量进行了选择,利用遗传算法的全局最优搜索和大规模并行计算能力来获得最佳的传感器位置和数量. Combustion control and performance evaluation for scramjets need effective measurement information, therefore it is important to choose the optimal location and number of sensors. This problem is a combinatorial optimization problem which is difficult to solve. This paper applies genetic algorithm to choose the optimal location and number of sensors, and the genetic algorithm performs a parallel, non-comprehensive search for the global optimal results.
出处 《航空动力学报》 EI CAS CSCD 北大核心 2007年第3期475-479,共5页 Journal of Aerospace Power
关键词 航空 航天推进系统 超燃冲压发动机 最佳位置选择 遗传算法 aerospace propulsion system scramjet optimal sensor location (OSL) genetic algorithm (GA)
  • 相关文献

参考文献7

  • 1Johns Hopkins University Applied Physics Laboratory.Ramjet technology[M].1980:10-12.
  • 2张鹏,俞刚.超燃燃烧室一维流场分析模型的研究[J].流体力学实验与测量,2003,17(1):88-92. 被引量:28
  • 3Kenneth T M.Optimal sensor plancement for control of a supersonic mixed-compression inlet with variable geometry[D].Ph.D.Paper,1998.
  • 4Martin J E.Optimal allocation of actuators for distributed systems[J].Journal of Dynamic Systems Measurement and Control,1978,100:227-228.
  • 5Aidarous S E,Gevers M R,Installe M J.Optimal pointwise discrete control and controllers[J].International Journal of Control,1976,24:493-508.
  • 6郑荣跃,许凯明,唐国金,黄剑源.斜拉桥监测系统传感器位置的寻优[J].国防科技大学学报,2005,27(2):107-110. 被引量:3
  • 7Holst T L.Genetic algorithms applied to multi-objective aerospace shape optimization[J].Journal of Aerspace Computing Information and Communication,2005,2:1389-1392.

二级参考文献13

  • 1[1]HEISER W H, PRATT D T, DELEY D H, et al. Hypersonic air-breathing propulsion. American Institute of Aeronautics and Astronautics Inc, Washington, D.C.
  • 2[2]CURRAN E T, MURTHY S N B. Scramjet propulsion.Progress in Astronautics and Aeronautics, vol. 189.
  • 3[3]YU G, LI J G, ZHAO J R, et al. Experimental studies on H2/Air model scramjet combustor. AIAA Paper 99-2449,June 1999.
  • 4[4]SHAPIRO A H. The dynamics and thermodynamics of compressible fluid flow. The Ronald Press Company, New York.
  • 5[5]YU G, LI J G, CHANG X Y,et al. Investigation of fuel injection and flame stsbilization in liquid hydrocarbon-fueled supersonic combustors. AIAA Paper 2001-3608, July 2001.
  • 6Kammer D C. Sensor Placement for On-orbit Modal Identification of Large Space Structure[J]. Journal of Guidance, Control and dynamics, 1991, 14(2):251-259.
  • 7O'Callahan J. A Procedure for an Improved Reduced System(IRS) Modal[A]. In: Demichele D J ed. Proceedings of the 7th IMAC Conference[C],1989:17-21.
  • 8Larson C B, Zimmerman D C, Marek E L. A Comparison of Modal Test Planning Technique: Excitation and Sensor Placement Using the NASN 8-bay Truss[A]. In: Allemang R ed. Proceeding of the 12th IMAC conference[C],1994:205-211.
  • 9Hafkta R T, Adelman H M.Selection of Actuator Locations for Static Shape Control of Large Space Structures by Heuristic Integer Programming[J]. Computers and Structures, 1985, 20(3): 575-58.
  • 10许凯明.[D].宁波大学,2004.

共引文献29

同被引文献23

引证文献3

二级引证文献4

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部