巧用Creat()和SyntaxFromSQL()函数创建动态数据窗口

本文以两个实例介绍了在PB环境下,利用Creat()和SyntaxfromSQL()函数创建动态数据窗口的设计方法.     

大Q（经营质量）的不良质量成本（COPQ）（下）

[类型XⅦ]不理解“质量是重中之重”，为了追求近期利润，把质量还达不到必要要求的产品／服务投入市场     

天问（节选）

作品概要 《天问》是屈原的重要代表作之一。全诗自始至终以问句构成,作者或一句一问,或两句一问,或四句一问,一口气对天、对地、对自然、对社会、对历史、对人生提出173个问题,以层层设问的方式表达自己的观念和价值取向,情理交融,声情并茂。宛若梦笔生花,读来兴趣盎然。因此,清代学者刘献庭在《离骚经讲录》中赞其为“千古万古至奇之作”。     

对（广义的）质量、可靠性工程（技术与管理）之管见（续）

三、（广义）质量、可靠性管理 广义质量、可靠性管理（以下简称质量、可靠性管理）是提高产品满足需求能力的管理工作项目．其主要内容如下：     

中国航天质量奖（组织类）评审管理办法（试行）

第一章 总则 第一条为提高航天行业整体质量效益和竞争能力。引导和激励航天企事业单位追求卓越绩效．中国航天科技集团公司和中国航天科工集团公司共同授权中国航天工业质量协会（简称航天质协）设立中国航天质量奖（简称航天质量奖）。为了科学、客观、公正地开展航天质量奖（组织类）的评审工作．特制订本办法。     

月球（火星）中子（水冰）探测仪初步方案研究

中子（水冰）探测仪在月球、火星和太阳系其它天体的水冰存在和含量分布的探测中有重要应用。文章主要介绍了美国、俄罗斯等国在月球、火星水冰探测中的中子探测仪的使用情况和探测结果,以及搭载于奥德赛（Odyssey）火星探测器上的中子谱仪、高能中子探测仪和＂月球勘测轨道器＂（LRO）上的月球勘测中子探测仪、计划搭载于美国＂火星科学实验室＂（MSL）上的中子反射动能测量仪的主要原理。最后提出了我国的一种中子探测仪的初步方案设想。     

Applying international space station (ISS) and solar-sail technology to the exploration and diversion of small,dark near earth objects (NEO's)

Space-Station technology, micron-thick 100-m solar sails, and a near-Earth propulsion system allow exploration of small, dark Near-Earth-Objects (NEO's) of cometary origin. Early crewed missions to NEO's could analyze the objects' properties and evaluate resource-mining possibilities. Later missions to Earth-threatening 100-m radius NEO's could deploy NEO-centered, high-area, low-mass reflective structures. The solar gravitational parameter (GM_sun) on a NEO is slightly reduced by increased radiation pressure. The central-force-field equations reveal that NEO eccentricity and average solar distance are thereby slightly increased. Given decades of warning and long-lived reflective canopies, such structures can convert Earth-impacts into near-misses. Although not suitable for NEO mining, such structures are superior to nuclear detonations because (as revealed by the 1994 Jupiter-comet interaction) NEO calving may be a consequence of explosions. NEO despinning is not required.     

Availability of O(2) and H(2)O(2) on pre-photosynthetic Earth

Old arguments that free O(2) must have been available at Earth's surface prior to the origin of photosynthesis have been revived by a new study that shows that aerobic respiration can occur at dissolved oxygen concentrations much lower than had previously been thought, perhaps as low as 0.05?nM, which corresponds to a partial pressure for O(2) of about 4?×?10(-8) bar. We used numerical models to study whether such O(2) concentrations might have been provided by atmospheric photochemistry. Results show that disproportionation of H(2)O(2) near the surface might have yielded enough O(2) to satisfy this constraint. Alternatively, poleward transport of O(2) from the equatorial stratosphere into the polar night region, followed by downward transport in the polar vortex, may have brought O(2) directly to the surface. Thus, our calculations indicate that this "early respiration" hypothesis might be physically reasonable.     

[Interior] Configuration options,habitability and architectural aspects of the transfer habitat module (THM) and the surface habitat on Mars (SHM)/ESA's AURORA human mission to Mars (HMM) study

This paper discusses the findings for [Interior] configuration options, habitability and architectural aspects of a first human spacecraft to Mars.In 2003 the space architecture office LIQUIFER was invited by the European Space Agency's (ESA) AURORA Program committee to consult the scientists and engineers from the European Space and Technology Center (ESTEC) and other European industrial communities with developing the first human mission to Mars, which will take place in 2030, regarding the architectural issues of crewed habitats.The task was to develop an interior configuration for a transfer vehicle (TV) to Mars, especially a transfer habitation module (THM) and a surface habitat module (SHM) on Mars. The total travel time Earth—Mars and back for a crew of six amounts to approximately 900 days. After a 200-day-flight three crewmembers will land on Mars in the Mars excursion vehicle (MEV) and will live and work in the SHM for 30 days. For 500 days before the 200-day journey back the spacecraft continues to circle the Martian orbit for further exploration. The entire mission program is based on our present knowledge of technology. The project was compiled during a constant feedback-design process and trans-disciplinary collaboration sessions in the ESA-ESTEC concurrent design facility.Long-term human space flight sets new spatial conditions and requirements to the design concept. The guidelines were developed from relevant numbers and facts of recognized standards, interviews with astronauts/cosmonauts and from analyses about habitability, sociology, psychology and configuration concepts of earlier space stations in combination with the topics of the individual's perception and relation of space.Result of this study is the development of a prototype concept for the THM and SHM with detailed information and complete plans of the interior configuration, including mass calculations. In addition the study contains a detailed explanation of the development of the Design process including all suggested design and configuration options.     

The Suess-Urey mission (return of solar matter to Earth)

The Suess-Urey (S-U) mission has been proposed as a NASA Discovery mission to return samples of matter from the Sun to the Earth for isotopic and chemical analyses in terrestrial laboratories to provide a major improvement in our knowledge of the average chemical and isotopic composition of the solar system. The S-U spacecraft and sample return capsule will be placed in a halo orbit around the L1 Sun-Earth libration point for two years to collect solar wind ions which implant into large passive collectors made of ultra-pure materials. Constant Spacecraft-Sun-Earth geometries enable simple spin stabilized attitude control, simple passive thermal control, and a fixed medium gain antenna. Low data requirements and the safety of a Sun-pointed spinner, result in extremely low mission operations costs.     

Io Volcano Observer (IVO): Budget travel to the outer Solar System

The IVO mission would make multiple close encounters with Io while orbiting Jupiter in an inclined elliptical orbit. The payload includes narrow-angle and wide-angle cameras (NAC and WAC), dual fluxgate magnetometers (FGM), a thermal mapper (ThM), dual ion and neutral mass spectrometers (INMS), and dual plasma ion analyzers (PIA). The mission is designed to answer key outstanding questions about Io, especially the nature of the intense active volcanism and internal processes that drive the volcanism. IVO can collect and return 20 Gb of compressed science data per Io encounter, 100 times the total Io data return from the 8yr Galileo tour.     

Nucleobases and prebiotic molecules in organic residues produced from the ultraviolet photo-irradiation of pyrimidine in NH(3) and H(2)O+NH(3) ices

Although not yet identified in the interstellar medium (ISM), N-heterocycles including nucleobases-the information subunits of DNA and RNA-are present in carbonaceous chondrites, which indicates that molecules of biological interest can be formed in non-terrestrial environments via abiotic pathways. Recent laboratory experiments and ab initio calculations have already shown that the irradiation of pyrimidine in pure H(2)O ices leads to the formation of a suite of oxidized pyrimidine derivatives, including the nucleobase uracil. In the present work, NH(3):pyrimidine and H(2)O:NH(3):pyrimidine ice mixtures with different relative proportions were irradiated with UV photons under astrophysically relevant conditions. Liquid- and gas-chromatography analysis of the resulting organic residues has led to the detection of the nucleobases uracil and cytosine, as well as other species of prebiotic interest such as urea and small amino acids. The presence of these molecules in organic residues formed under abiotic conditions supports scenarios in which extraterrestrial organics that formed in space and were subsequently delivered to telluric planets via comets and meteorites could have contributed to the inventory of molecules that triggered the first biological reactions on their surfaces.     

Readaptation of the vestibuloocular reflex to 1g-condition in immature lower vertebrates (Xenopus laevis) after micro- or hypergravity exposure

The effects of altered gravitational conditions (AGC) on the development of the static vestibulo-ocular reflex (VOR) and readaptation to 1g were investigated in the amphibian Xenopus laevis. Tadpoles were exposed to microgravity (μg) during the German Space Mission D-2 for 10 days, using the STATEX closed survival system, or to 3g for 9 days during earth-bound experiments. At the beginning of AGC, the tadpoles had not yet developed the static VOR.

The main results were: (i) Tadpoles with ug- or 3g-experience had a lower gain of the static VOR than the 1g-controls during the 2nd and 5th post-AGC days, (ii) Readaptation to response levels of 1g-reared controls usually occurred during the following weeks, except in slowly developing tadpoles with 3g-experience. Readaptation was less pronounced if, during the acute VOR test, tadpoles were rolled from the inclined to the normal posture than in the opposite test situation.

It is postulated that (i) gravity is necessarily involved in the development of the static VOR, but only during a period including the time before onset of the first behavioural response; and (ii) readaptation which is superimposed by the processes of VOR development depends on many factors including the velocity of development, the actual excitation level of the vestibular systems and the neuroplastic properties of its specific pathways.     

Balloon-borne air traffic management (ATM) as a precursor to space-based ATM

The International Space University—Balloon Air traffic control Technology Experiment (I-BATE¹) has flown on board two stratospheric balloons and has tracked nearby aircraft by receiving their Automatic Dependent Surveillance-Broadcast (ADS-B) transmissions. Air traffic worldwide is facing increasing congestion. It is predicted that daily European flight volumes will more than double by 2030 compared to 2009 volumes. ADS-B is an air traffic management system being used to mitigate air traffic congestion. Each aircraft is equipped with both a GPS receiver and an ADS-B transponder. The transponder transmits an equipped aircraft's unique identifier, position, heading, and velocity once per second. The ADS-B transmissions can then be received by ground stations for use in traditional air traffic management. Airspace not monitored by these ground stations or other traditional means remains uncontrolled and poorly monitored. A constellation of space-based ADS-B receivers could close these gaps and provide global air traffic monitoring. By flying an ADS-B receiver on a stratospheric balloon, I-BATE has served as a precursor to a constellation of ADS-B-equipped Earth-orbiting satellites. From the ～30 km balloon altitude, I-BATE tracked aircraft ranging up to 850 km. The experiment has served as a proof of concept for space-based air traffic management and supports a technology readiness level 6 of space-based ADS-B reception.