基于独立函数的通用逻辑模块

本文提出一种新型的通用逻辑模块(ULM),它以独立函数为核心(细胞),细胞之间以相同的方式——“异或”——相联结,可以生成全部2~(2n)个逻辑函数。它具有算法简单、使用灵活的特点。在伪随机信号的产生及自动控制中有着广阔的应用前景。     

ExoMars 2016火星探测计划进入、减速、着陆的验证任务分析

对欧洲航天局(ESA)火星探测的ExoMars 2016计划进行了概述,着重分析了进入、减速、着陆验证任务的关键环节,详细分析了进入、减速、着陆验证的任务组成、任务目标、任务规划以及相关关键技术等。结合我国火星探测目前的技术状态,需要针对进入、减速、着陆各关键技术进行合理的规划,并适时开展相关的试验验证。首先完成整个火星探测进入、减速、着陆平台的验证与研制,再进一步开展深入的火星探测科学任务研究。文章所述内容和分析可为我国下一步开展火星等深空探测任务提供参考。     

ALPHA900系列数据采集器测试系统的设计

介绍了一个数据采集器测试系统的构成及其软件设计，并对系统软件的设计方法、主要功能和主要特色进行了讨论。     

一种新型的分布式数据采集器(一)

介绍了一种新型的分布式智能数据采集系统──ALPHA900系列数据采集器。该采集器由中国航空工业总公司第三0四研究所与英国ADAS公司联合设计研制。它集中了90年代采集器的优点，如可变字长、可编程智能前端、带温度补偿的连接器、可脱机工作等，并为突出各自功能形成系列。该采集器已成功地投入了工业生产，并且应用于工业过程监测、条件监测或加工监测。该系统使用价格低廉的RS485网络，各种型号模块提供了精确的温度、压力、应变及数字事件和频率等数据的测量及控制，并有相当突出的性能价格比。     

Exploration life support technology challenges for the Crew Exploration Vehicle and future human missions

As NASA implements the U.S. Space Exploration Policy, life support systems must be provided for an expanding sequence of exploration missions. NASA has implemented effective life support for Apollo, the Space Shuttle, and the International Space Station (ISS) and continues to develop advanced systems. This paper provides an overview of life support requirements, previously implemented systems, and new technologies being developed by the Exploration Life Support Project for the Orion Crew Exploration Vehicle (CEV) and Lunar Outpost and future Mars missions. The two contrasting practical approaches to providing space life support are (1) open loop direct supply of atmosphere, water, and food, and (2) physicochemical regeneration of air and water with direct supply of food. Open loop direct supply of air and water is cost effective for short missions, but recycling oxygen and water saves costly launch mass on longer missions. Because of the short CEV mission durations, the CEV life support system will be open loop as in Apollo and Space Shuttle. New life support technologies for CEV that address identified shortcomings of existing systems are discussed. Because both ISS and Lunar Outpost have a planned 10-year operational life, the Lunar Outpost life support system should be regenerative like that for ISS and it could utilize technologies similar to ISS. The Lunar Outpost life support system, however, should be extensively redesigned to reduce mass, power, and volume, to improve reliability and incorporate lessons learned, and to take advantage of technology advances over the last 20 years. The Lunar Outpost design could also take advantage of partial gravity and lunar resources.     

民机地面扰流板伸出自动控制逻辑研究及对飞行安全影响分析

对7种型号民机的地面扰流板伸出自动控制逻辑进行了对比研究,对地面扰流板待命、完全与部分伸出、主轮接地、推力手柄位置等方面进行了分析讨论;最后以A320 为例,就着陆时冲出跑道和发生弹跳两种情况,分析了地面扰流板伸出自动控制逻辑对飞行安全的影响。分析表明,完善的地面扰流板伸出自动控制逻辑,可以提升对飞行操作的容错性,降低因人为因素导致飞行事故的可能性。     

从毛泽东诗词看毛泽东的社会历史观

在毛泽东诗词中,既有广大民众创造世界、创造历史的观念,亦有英雄人物创造世界、创造历史的思想。毛泽东理想中的英雄人物不是通常意义上的英雄人物,而是探得了“大本大源”、洞晓宇宙真理的人物。这样的英雄人物才是创造世界、创造历史的人物。     

多频段多目标海上测控模拟器的设计与实现

介绍了多频段多目标海上测控模拟器的设计和实现方法。在硬件设计上,模拟器采用工控机和工作站架构,数字化可重组基带硬件平台技术,实现了不同频段、不同目标航天器的仿真功能。在软件设计上,采用RS422/232接口双中断驱动技术,实现了遥测和数传的同步;采用软件模块化和数据库融合设计技术,实现了多型号目标航天器的仿真需求。     

空管安全管理体系之框架搭建

结合我国建设民航强国的战略构想和中国民航局2010年"安全体系建设年"的工作部署,设计了空管系统安全管理体系(SMS)的总体框架,并对其模块和要素以及相互间关系进行了说明和论述,以期对空管系统的SMS建设起到一定的促进作用.     

Non-BBN Constraints on the Key Cosmological Parameters

Since the baryon-to-photon ratio 10 is in some doubt at present, we ignore the constraints on 10 from big bang nucleosynthesis (BBN) and fit the three key cosmological parameters (h, M, 10) to four other observational constraints: Hubble parameter (ho), age of the universe (to), cluster gas (baryon) fraction (fo fGh3/2), and effective shape parameter (o). We consider open and flat CDM models and flat CDM models, testing goodness of fit and drawing confidence regions by the 2 method. CDM models with M = 1 (SCDM models) are accepted only because we allow a large error on ho, permitting h < 0.5. Open CDM models are accepted only for _M 0.4. CDM models give similar results. In all of these models, large 10 ( 6) is favored strongly over small 10 ( 2), supporting reports of low deuterium abundances on some QSO lines of sight, and suggesting that observational determinations of primordial 4He may be contaminated by systematic errors. Only if we drop the crucial o constraint are much lower values of M and 10 permitted.