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121.
基于TRIZ直接进化理论的切削技术进展 总被引:4,自引:0,他引:4
为进一步开发新型切削技术,探索切削加工的未来发展趋势,必须研究和跟踪切削技术的进化历程。TR IZ(T heory of inven tive prob lem so lv ing)技术进化理论是专门研究技术系统进化预测的重要分支。本文着重对TR IZ直接进化理论进行了评述,根据TR IZ直接进化模式,分析和总结了切削技术的进化路线。提出改进的进化潜能图,基于该进化潜能图,指出增加切削技术的可控性、充分利用系统资源和继续增加切削技术的理想度是未来切削技术可能的开发方向。 相似文献
122.
仿生物态模拟型硬件理论与关键技术研究 总被引:4,自引:1,他引:4
阐述了模拟型仿生硬件的概念、基本思想与技术瓶颈,分析了基于FPTA(Field programmable transistor array)的模拟型仿生硬件的结构与电子细胞电路工作原理。给出了模拟型仿生硬件的电路编码方案、个体电路测试评估方法和进化实现过程。提出了基于单染色体自适应变异进化机制的模拟型仿生硬件进化算法。以信号放大器、半波整流器、异或门数字电路作为典型应用实例,来验证模拟型仿生硬件的进化特性,并讨论了进化算法的参数选取、染色体适应度评估问题。仿真结果表明:所提出硬件进化算法的进化速度快、成功率高,所设计的FPTA细胞阵列可以实现模拟信号放大、信号处理和数字电路逻辑功能。 相似文献
123.
A new hybrid aerodynamic optimization framework based on differential evolution and invasive weed optimization 总被引:1,自引:2,他引:1
Since many aerodynamic optimization problems in the area of aeronautics contain highly nonlinear objectives and multiple local optima, it is still a challenge for most of the traditional optimization methods to find the global optima. In this paper, a new hybrid optimization framework based on Differential Evolution and Invasive Weed Optimization (IWO_DE/Ring) is developed, which combines global and local search to improve the performance, where a Multiple-Output Gaussian Process (MOGP) is used as the surrogate model. We first use several test functions to verify the performance of the IWO_DE/Ring method, and then apply the optimization framework to a supercritical airfoil design problem. The convergence and the robustness of the proposed framework are compared against some other optimization methods. The IWO_DE/Ring-based approach provides much quicker and steadier convergence than the traditional methods. The results show that the stability of the dynamic optimization process is an important indication of the confidence in the obtained optimum, and the proposed optimization framework based on IWO_DE/Ring is a reliable and promising alternative for complex aeronautical optimization problems. 相似文献
124.
S. Valk A. Lemaître L. Anselmo 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2008,41(7):1077-1090
This paper provides a Hamiltonian formulation of the averaged equations of motion with respect to short periods (1 day) of a space debris subjected to direct solar radiation pressure and orbiting near the geostationary ring. This theory is based on a semi-analytical theory of order 1 regarding the averaging process, formulated using canonical and non-singular elements for eccentricity and inclination. The analysis is based on an expansion in powers of the eccentricity and of the inclination, truncated at an arbitrary high order. 相似文献
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Evolution and composition of baryonic matter is influenced by the evolution of other forms of matter and energy in the universe.
At the time of primordial nucleosynthesis the universal expansion and thus the decrease of the density and temperature of
baryonic matter were controlled by leptons and photons. Non-baryonic dark matter initiated the formation of clusters and galaxies,
and to this day, dark matter largely determines the dynamics and geometries of these baryonic structures and indirectly influences
their chemical evolution. Chemical analyses and isotopic abundance measurements in the solar system established the composition
in the protosolar cloud (PSC). The abundances of nuclear species in the PSC led to the discovery of the magic numbers and
the nuclear shell model, and they allowed the identification of nucleosynthetic sites and processes. To this day, we know
the abundances of the ∼300 stable and long-lived nuclides infinitely better in the PSC than in any other sample of matter
in the universe. Thus, we know the exact composition of a Galactic sample of intermediate age, allowing us to check on theories
of Galactic evolution before and after the formation of the solar system. This paper specifically discusses the nucleosynthesis
in the early universe and the Galactic evolution during the last 5 Gyr. 相似文献
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Prognostics and health management (PHM) is very important to guarantee the reliability and safety of aerospace systems, and sensing and test are the precondition of PHM. Integrating design for testability into early design stage of system early design stage is deemed as a fundamental way to improve PHM performance, and testability model is the base of testability analysis and design. This paper discusses a hierarchical model-based approach to testability modeling and analysis for heading attitude system health management. Quantified directed graph, of which the nodes represent components and tests and the directed edges represent fault propagation paths, is used to describe fault-test dependency, and quantitative testability information is assigned to nodes and directed edges. The fault dependencies between nodes can be obtained by functional fault analysis methodology that captures the physical architecture and material flows such as energy, heat, data, and so on. By incorporating physics of failure models into component, the dynamic process of a failing or degrading component can be projected onto system behavior, i.e., system symptoms. Then, the analysis of extended failure modes, mechanisms and effects is utilized to construct fault evolution-test dependency. Using this integrated model, the designers and system analysts can assess the test suite’s fault detectability, fault isolability and fault predictability. And heading attitude system application results show that the proposed model can support testability analysis and design for PHM very well. 相似文献