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341.
试论高校职业指导工作的开展与推动 总被引:1,自引:0,他引:1
高校职业指导工作是一项复杂的系统工程,这项工作的开展与推动,是贯彻落实党和国家的就业方针、政策的需要,事关毕业生的职业前途与人生目标的实现,对高校教育事业的可持续发展,具有明显的现实意义和重要的战略意义,需要采取切实有效的策略。 相似文献
342.
刑事评议程序是介于庭审程序和宣告程序之间的一个重要程序,它既是庭审的自然延续,又是裁判结论形成的前提和基础。然而,欲保证刑事评议程序的正常运行,刑事评议主体之独立必须得到保证;刑事评议之客体还应被全面考虑,并对其进行细化,以确保刑事评议的针对性和有效性,防止出现"估堆"现象。本文以域外刑事评议程序为对象,从评议的主体、客体等角度进行梳理,得出规律性的认识,以期对我国关于刑事评议的立法有所裨益。 相似文献
343.
对广州市产业发展现状进行评价,认为其主要问题表现为产业发展方式整体粗放、资源供给紧张、产业发展调节能力差、成熟完备的产业系统尚未形成,等等.进而借用循环经济有关理念,提出广州产业升级的四大思路:资源型向资本型转变、实体经济向真空经济转变、断裂经济向循环经济转变和产业分割向产业整合转变.最后,对广州发展新型现代产业体系提出若干建议:建立常设性机构、完善现行法规体系、进行制度建设、鼓励技术创新、树立循环经济发展理念. 相似文献
344.
张文 《华北航天工业学院学报》2002,12(3):56-57,62
在高等教育深化改革的今天,使得课表编制工作的复杂程度越来越高。在这种新形势下,如何才能编制出科学、合理、高效、周密的课表,以达到建立优良的教学秩序和教学环境,提高教学质量的目的,这是高校教学管理工作者急需认真研究的问题。 相似文献
345.
The objective of this paper is to present the experience of EADS in using a common test support system for integration and qualification testing, aircraft ground equipment (AGE), in-service software maintenance facilities (ISMF) and ground crew training. EADS uses its test support system AIDASS (Advanced Integrated Data Acquisition and Stimulation System) in different phases of the aircraft life cycle. AIDASS is comprised of a real-time front-end system and a standard PC for the user interface. The EADS test support system is used in almost all phases of the aircraft life cycle, for instance, for integration and verification testing, as aircraft ground equipment, for in-service software maintenance and training of ground crews. This test support system is used for the software maintenance in the TORNADO program at different airforces in Europe. The airforces also share test setups with industry 相似文献
346.
A new paradigm is suggested for 3D magnetic reconnection where the interaction of reconnection processes with current aligned
instabilities plays an important role. According to the new paradigm, the initial equilibrium is rendered unstable by current
aligned instabilities (lower-hybrid drift instability first, drift-kink instability later) and the non-uniform development
of kinking modes leads to a compression of magnetic field lines in certain locations and a rarefaction in others. The areas
where the flow is compressional are subjected to a driven reconnection process. In the present paper we illustrate this series
of events with a selection of simulation results.
This revised version was published online in August 2006 with corrections to the Cover Date. 相似文献
347.
文章阐述RFID物流配送系统的构成及其信息处理过程,探讨RFID电子标签在物流配送全过程中的信息识别作用,提出了RFID技术在现代物流配送中的一种新型应用模型和方法。 相似文献
348.
A. Sh. Dzhabrailov Yu. V. Klochkov S. S. Marchenko A. P. Nikolaev 《Russian Aeronautics (Iz VUZ)》2007,50(2):115-120
We demonstrate that it is possible to express each component of the displacement vector for the interior point of the finite element (FE) through all components of nodal unknowns in curvilinear coordinates. The effectiveness of the valid technique of vector approximation for displacement fields has been verified on an example. 相似文献
349.
D. Koschny V. Dhiri K. Wirth J. Zender R. Solaz R. Hoofs R. Laureijs T.-M Ho B. Davidsson G. Schwehm 《Space Science Reviews》2007,128(1-4):167-188
ESA’s Rosetta mission was launched in March 2004 and is on its way to comet 67P/Churyumov-Gerasimenko, where it is scheduled
to arrive in summer 2014. It comprises a payload of 12 scientific instruments and a Lander. All instruments are provided by
Principal Investigators, which are responsible for their operations.
As for most ESA science missions, the ground segment of the mission consists of a Mission Operations Centre (MOC) and a Science
Operations Centre (SOC). While the MOC is responsible for all spacecraft-related aspects and the final uplink of all command
timelines to the spacecraft, the scientific operations of the instruments and the collection of the data and ingestion into
the Planetary Science Archive are coordinated by the SOC. This paper focuses on the tasks of the SOC and in particular on
the methodology and constraints to convert the scientific goals of the Rosetta mission to operational timelines. 相似文献
350.
Maciel J.J. Slocum J.F. Smith J.K. Turtle J. 《Aerospace and Electronic Systems Magazine, IEEE》2007,22(11):17-20
Large apertures are of great benefit to applications that are prime powered limited as is found on aerostat and other airborne platforms. Electronically scanned array antennas are often proposed for these applications. However, increasing the aperture area with conventional array technology is met with prohibitive cost, weight, and prime power increases because of the dense spacing of phase shifters and/or active T/R modules. This discusses the recent development of RF MEMS (Microelectromechanical System) switch technology and the use of these switches in a Radanttrade lens configuration for arrays of approximately 10 m2 at X-band. A proof-of-concept 0.4 m2 MEMS Electronically Steerable Antenna (ESA) containing 25,000 MEMS switches has been successfully designed, fabricated, and tested. The 0.4 m2 MEMS ESA was then integrated with an AN/APG-67 radar system to form the MEMS Demonstration Radar System. The MEMS Demonstration Radar System successfully detected both airborne and ground moving targets during a series of extensive radar demonstrations. This is believed to be the first large scale employment of MEMS switches in a scanning antenna and radar system. The low-cost, lightweight, and low power technology demonstrated can enable weight and power constrained platforms with electronic steering. 相似文献