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111.
As multi-discipline coupling and components interference often affect the aircraft configuration decision-making and analysis during conceptual design process, this article presents an approach of multidimensional game theory based on aircraft components to deal with this problem. The idea is that the configuration decision-making process is regarded as the game for different disciplines and technologies, and the aircraft components are players. The payoff function with highest total gain means that according to the game protocols and multidimensional theory, the optimal aircraft configuration within the strategy set will be chosen. The decision-making model is applied to conceptual design process of the high altitude long endurance (HALE) unmanned aerial vehicle (UAV) based on the assessment of technological risk. The obtained optimum configuration is quite consistent with the current HALE UAV development trends. Thus, taking into account the coupling and interference factors, the multidimensional gaming model based on aircraft components will be an effective analysis method in the decision-making process of aircraft optimum configuration. 相似文献
112.
张鹏 《西安航空技术高等专科学校学报》2012,(6):53-55
文化创意产业作为新兴产业形式,其发展需要大量的创意型人才。及时地分析和认清目前我国文化创意人才现状和存在问题,提出创意人才培养新模式已成为当务之急。基于此,在分析目前我国创意人才现状和存在问题的基础上,有针对性地从四个方面提出了创意人才培养的新模式。 相似文献
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在制品管理中条码技术的应用 总被引:2,自引:0,他引:2
针对面向订单的单件、小批量生产制造企业,设计了一套条码数据采集系统,分析了主要运作流程和功能模块.在在制品的管理中提出了基于不同级别的工件生产状态定义,并给出了相应的加工、检验判定准则.经实际使用证明条码技术运用于工业现场是可行的. 相似文献
115.
Yong-Liang Wang Zheng Bao Ying-Ning Peng 《IEEE transactions on aerospace and electronic systems》2000,36(2):609-620
Space-time adaptive processing (STAP) has been widely discussed for airborne radar systems to improve the system performance of detecting targets. This is especially true for airborne early warning (AEW) radar, which should find long-range and small radar cross section (RCS) targets such as the stealth aircraft and missiles. However, in existing airborne radar literature, STAP is mainly considered for clutter and jamming rejection in side-looking airborne radar (SLAR) applications. There have been fewer discussions on airborne radar with non-side-ways looking array radar (non-SLAR). The STAP of non-SLAR such as forward looking array radar is also very important and can not be avoided for airborne radar to detect targets in all directions. The STAP of the non-SLAR is studied here. A scheme has been proposed, which is processed by the way of STAP combined with multiple staggered medium pulse repetition frequencies (PRFs). We further study the selection of PRFs in order to make the scheme more available for non-SLAR radar. We analyze two typical non-SLAR cases, i.e., inclined-sideways looking array and forward looking array. We examine this scheme by comparing the performances of three processing systems under the criteria of range-velocity blind zone minimization. Computer simulation results show the multiple-PRFs STAP scheme is feasible for non-SLAR and can be applied to phased-array AEW radar systems 相似文献
116.
Huang Yong Peng Yingning Wang Xiqin 《Aerospace and Electronic Systems Magazine, IEEE》1999,14(7):19-21
A new airborne MTI scheme that applies to non-homogeneous clutter environment is presented. Results of simulation have proved that the scheme has a superior ground clutter suppression performance and can effectively prevent the whitening of a target 相似文献
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何君 《郑州航空工业管理学院学报(管理科学版)》2008,26(2):110-112
新的《企业会计准则第1号——存货》废除了存货结算的后进先出法,反映了我国会计准则与国际准则的趋同。在我国目前的经济环境下,先进先出法对我国宏观经济具有利好作用,具体表现在以下方面:(1)在物价持续上升时期有助于企业提高价值,增强投资者对我国总体经济走势的信心;(2)在保持企业稳定发展的同时,税收的增加可以充裕财政,加强政府对我国经济的宏观调控;(3)可以真实反映国有企业资产价值,避免国有资产流失。 相似文献
119.
Cavitation caused by insufficient suction is a major factor that influences the life of aircraft pumps. Currently, pressurizing the tank can solve the cavitation problem under steady large-flow conditions. However, this method is not always effective under transient conditions (from zero flow to full flow in a very short time). Moreover, to apply and design other measures, such as a boost impeller, the suction dynamics during the transient period must be investigated. In this paper, a novel approach based on the pressure wave propagation theory is proposed for predicting the inlet pressure of an aircraft pump under transient conditions. First, a dynamic model of a typical aircraft pump is established in the form of differential equations. Then, the transient flow model of the inlet line is described using momentum and continuity equations, and the governing equations are discretized by the method of characteristics and the finite difference method. The simulated results are in good agreement with the results from verification tests. Further simulation analysis indicates that the wave velocity and transient time may influence the inlet and reservoir pressure as well as the size of the inlet line. Finally, solutions for upgrading the inlet pressure are discussed. These solutions provide guidelines for designing inlet installations. 相似文献
120.