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181.
The woven fabric membrane materials are widely used in space and terrestrial inflatable reflectors. However the material?s anisotropy makes the design analysis more complex. The deviation from the desired shape, so-called “W-profile error”, influences the precision of the membrane surface significantly. In this study, a model of an axisymmetric paraboloid surface using membrane theory is established for the purpose of facilitating the surface precision optimization. Analytical solutions for displacements of the reflector are derived. An iteration method of initial reflector profile solution is stated and a finite element (FE) software employed in the solution is presented. A case study is illustrated to make a comparison between numerical and theoretical analyses. Finally, the conclusions are drawn that the analytical method and the FE iterative method for initial profile solution are feasible and efficient. 相似文献
182.
飞机油量传感器布局设计的CAD方法的研究 总被引:1,自引:0,他引:1
根据飞机燃油油量测量的原理引出了数字式燃油测量系统中油量传感器的布局原则,由此提出了可测区的概念,并对相应的可测区计算方法中的关键技术作了阐述。最后给出了通过可测区计算及可测性验证进行油箱中油量传感器布局设计的有关结论。 相似文献
183.
社会经济系统的运行规律同生态系统之间存在着极强的相似性和关联性.运用生态学方法解析企业集团生态位现象,并结合系统论和突变论的思想,提出了企业集团生态住因子维度体系,构建了中国电子企业集团生态位突变模型,既为企业仿生研究提供了一个新的研究视角,也可对企业战略管理具有一定的指导作用. 相似文献
184.
The continuous growth of air traffic has led to acute airspace congestion and severe delays, which threatens operation safety and cause enormous economic loss. Flight assignment is an economical and effective strategic plan to reduce the flight delay and airspace congestion by reasonably regulating the air traffic flow of China. However, it is a large-scale combinatorial optimization problem which is difficult to solve. In order to improve the quality of solutions, an effective multi-objective parallel evolution algorithm(MPEA) framework with dynamic migration interval strategy is presented in this work. Firstly, multiple evolution populations are constructed to solve the problem simultaneously to enhance the optimization capability. Then a new strategy is proposed to dynamically change the migration interval among different evolution populations to improve the efficiency of the cooperation of populations. Finally, the cooperative co-evolution(CC) algorithm combined with non-dominated sorting genetic algorithm II(NSGA-II) is introduced for each population. Empirical studies using the real air traffic data of the Chinese air route network and daily flight plans show that our method outperforms the existing approaches, multiobjective genetic algorithm(MOGA), multi-objective evolutionary algorithm based on decomposition(MOEA/D), CC-based multi-objective algorithm(CCMA) as well as other two MPEAs with different migration interval strategies. 相似文献
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H. Cottin P. Coll D. Coscia N. Fray Y.Y. Guan F. Macari F. Raulin C. Rivron F. Stalport C. Szopa D. Chaput M. Viso M. Bertrand A. Chabin L. Thirkell F. Westall A. Brack 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2008
To understand the evolution of organic molecules involved in extraterrestrial environments and with exobiological implications, many experimental programs in the laboratory are devoted to photochemical studies in the gaseous phase as well as in the solid state. The validity of such studies and their applications to extraterrestrial environments can be questioned as long as experiments conducted in space conditions, with the full solar spectrum, especially in the short wavelength domain, have not been implemented. The experiments that are described here will be carried out on a FOTON capsule, using the BIOPAN facility, and on the International Space Station, using the EXPOSE facility. Vented and sealed exposition cells will be used, which will allow us to study the chemical evolution in the gaseous phase as well as heterogeneous processes, such as the degradation of solid compounds and the release of gaseous fragments. 相似文献
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The FIELDS Instrument Suite on MMS: Scientific Objectives,Measurements, and Data Products 总被引:1,自引:0,他引:1
R. B. Torbert C. T. Russell W. Magnes R. E. Ergun P.-A. Lindqvist O. LeContel H. Vaith J. Macri S. Myers D. Rau J. Needell B. King M. Granoff M. Chutter I. Dors G. Olsson Y. V. Khotyaintsev A. Eriksson C. A. Kletzing S. Bounds B. Anderson W. Baumjohann M. Steller K. Bromund Guan Le R. Nakamura R. J. Strangeway H. K. Leinweber S. Tucker J. Westfall D. Fischer F. Plaschke J. Porter K. Lappalainen 《Space Science Reviews》2016,199(1-4):105-135
190.
通过地面试验取得的数据所建立的液体火箭发动机参数计算和误差确定的经验公式,在导弹飞行试验中,对发动机参数计算起重要作用。本文就发动机主要参数及误差的经验公式进行推导和确定。 相似文献