某型舵机放大器电老炼模拟负载方案论证

通过对舵机放大器电老炼各类负载进行权衡论证,研究出功率电阻与电感串联的模拟负载。经过方案论证和充分的试验,设计特定的激励信号,对该方案不断地优化和完善,最终基本模拟了电机特性。证明该方案可最大限度地模拟了实际负载电机的工作特性,更适合本单位目前的批生产状态。     

浅论企业网络营销的项目管理

网络营销(Electronic Marketing)是企业整体营销战略的一个组成部分,是建立在互联网基础之上,借助于互联网特性来完成企业一定营销目标的一种营销活动.网络的迅速普及和网络营销的迅速崛起以及全球经济一体化的形成,对当代项目管理提出了更高的要求.如何尽快采用信息化手段实施项目管理和决策,在项目的有限生命周期内...     

浅论企业网络营销的项目管理

网络营销（Electronic Marketing）是企业整体营销战略的一个组成部分,是建立在互联网基础之上,借助于互联网特性来完成企业一定营销目标的一种营销活动。网络的迅速普及和网络营销的迅速崛起以及全球经济一体化的形成,对当代项目管理提出了更高的要求。如何尽快采用信息化手段实施项目管理和决策,在项目的有限生命周期内尽其所能地发挥管理的功效使企业立于不败之地,开发和研究基于网络营销的项目管理是出路所在。     

On the measurements of the moon’s infrared temperature and its relation to the phase angle

Radiometric measurements of the thermal radiation originating from the moon’s surface were obtained using an infrared detector operating at wavelengths between 8 and 14 μm. The measurements cover a full moon cycle. The variation of the moon’s temperature with the lunar phase angle was established. The lunar temperatures were 391 ± 2.0 K for the full moon, 240 ± 3.5 K for the first quarter, and 236 ± 3 K for the last quarter. For the rest of the phase angles, the lunar temperature varied between 170 and 380 K. Our results are comparable with those obtained previously at these phase angles. For the new moon phase, the obtained temperature was between 120 and 133 K. With the exception of the new moon phase, our measurements at all the phase angles were consistent with those obtained using Earth-based data and those obtained by the Diviner experiment and the Clementine spacecraft. At the new phase, our measurements were comparable with those obtained from the ground but were significantly higher than those obtained by the Diviner and Clementine data. We attribute this inconsistency to either the calibration curve of our detector, which does not perform well at very low temperatures, or to infrared emission from the atmosphere. A simple linear model to predict the lunar temperature as a function of the phase angle was proposed. The experimental errors that affect the measured temperatures are discussed.     

基于博弈模型的航空型号异地协同知识共享激励研究

在航空型号异地协同研发的过程中需要参研单位进行知识共享,针对知识共享过程中产生的问题,构建知识共享博弈模型并对其进行分析,提出了对采取共享策略的参研单位给予奖励,在博弈模型中引入激励因素,并分析了激励对参研单位知识共享行为的影响。     

航天器外表面导电面积对朗缪尔探针科学探测的影响

朗缪尔探针的科学探测会受到航天器外表面导电面积与朗缪尔探针传感器有效面积之比大小的影响。如果航天器的外表面导电面积不足够大,朗缪尔探针以扫描电压模式工作时,就会造成航天器地电位的扰动,进而导致朗缪尔探针测量结果的偏差。分析了此问题的物理原理,并进行了相应的理论计算。子午工程探空火箭有效载荷朗缪尔探针在进行科学探测的同时,测量了火箭外表面导电面积与朗缪尔探针传感器有效面积之比不足造成的扰动,测量结果与理论分析基本一致。     

通用飞机批产项目进度计划体系研究与构建

以某型通用飞机产品为例,阐述其批产项目进度计划体系构建过程,实现批产项目进度计划管理的规范化、精细化、信息化,并建立一套适用于通用航空制造企业高效率、低成本的批产项目进度计划管理方法.     

An overview of RADOM results for earth and moon radiation environment on Chandrayaan-1 satellite

The RADiatiOn Monitor (RADOM) is a miniature dosimeter-spectrometer that flew onboard the Chandrayaan-1 lunar mission in order to monitor the local radiation environment. Primary objective of the RADOM experiment was to measure the total absorbed dose, flux of surrounding energetic particles and spectrum of the deposited energy from high energy particles both en-route and in lunar orbit. RADOM was the first experiment to be switched on after the launch of Chandrayaan-1 and was operational until the end of the mission. This paper summarizes the observations carried out by RADOM during the entire life time (22 October 2008–31 August 2009) of the Chandrayaan-1 mission and compares the measurement by RADOM with the radiation belt models such as AP-8, AE-8 and CRRESS.     

AutoCAD/CAPP/PDM一体化解决方案研究

AutoCAD 是机械制造行业最为广泛应用的辅助设计软件.在制造业技术信息化建设中,如何实现CAD/CAPP/PDM信息集成是企业信息化建设的现实问题.提出了论述了应用AutoCAD VBA开发AutoCAD系统,构建AutoCAD与数据库系统的接口关系,开发实用高效的CAD/CAPP/PDM集成产品数据管理系统解决方案.     

基于TOPSIS法的飞机维修方案的决策

针对航空公司如何选择一种经济高效的维修方案的难题,提出了基于TOPSIS法的飞机维修方案决策方法。利用TOPSIS法的原理,通过对维修方案进行定量与定性相结合的分析,给出了飞机维修方案最优决策模型。此模型可对飞机维修备选方案进行优劣排序,确定最优的飞机维修方案,从而提高飞机维修方案决策的科学性。