The Science Case for STEP

The Satellite Test of the Equivalence Principle (STEP) will advance experimental limits on violations of Einstein’s Equivalence Principle (EP) from their present sensitivity of 2 parts in 10¹³${10}^{13}$ to 1 part in 10¹⁸${10}^{18}$ through multiple comparison of the motions of four pairs of test masses of different compositions in an earth-orbiting drag-free satellite. Dimensional arguments suggest that violations, if they exist, should be found in this range, and they are also suggested by leading attempts at unified theories of fundamental interactions (e.g., string theory) and cosmological theories involving dynamical dark energy. Discovery of a violation would constitute the discovery of a new force of nature and provide a critical signpost toward unification. A null result would be just as profound, because it would close off any possibility of a natural-strength coupling between standard-model fields and the new light degrees of freedom that such theories generically predict (e.g., dilatons, moduli, quintessence). STEP should thus be seen as the intermediate-scale component of an integrated strategy for fundamental physics experiments that already includes particle accelerators (at the smallest scales) and supernova probes (at the largest). The former may find indirect evidence for new fields via their missing-energy signatures, and the latter may produce direct evidence through changes in cosmological equation of state—but only a gravitational experiment like STEP can go further and reveal how or whether such a field couples to the rest of the standard model. It is at once complementary to the other two kinds of tests, and a uniquely powerful probe of fundamental physics in its own right.     

SGKW轨道在线生成技术研究

天基对地打击动能武器(SGKW)用于从太空对地面高价值战略目标进行快速、准确的打击.针对作战实时性要求,探讨了SGKW的轨道在线生成技术.首先,利用庞特里亚金极大值原理将时间最短打击轨道的最优控制问题转化为两点边值问题.由于约束条件中存在优化参数,一种基于"遗传算法+序列二次规划"的组合优化算法被用于求解伴随变量初值和再入点参数.为了提高轨道生成的速度,在大量离线优化数据的基础上建立了BP神经网络预测模型,其预测值通过序列二次规划算法稍加修正,即可满足相应任务的落点精度要求.仿真结果验证了上述方案的有效性.     

机载液压系统设计原则与发展趋势

通过总结几种典型的机载液压系统的设计特点,归纳出未来机载液压系统的基本设计原则以及发展趋势。     

高职校园文化的内涵与特征分析

诠释高职校园文化的内涵，从文化存在的形态着眼，将高职校园文化划分为物质文化、制度文化、行为文化、精神文化四个层面；分析高职校园文化的特征，包括稳定性、应用性、时代性、实践性、技术独特性；指出建设高品质高职校园文化应该坚持时代性与独特性相结合、开放性与封闭性相结合、创新性与继承性相结合的原则。     

浅谈在编译原理教学中促进学生的学习迁移

学习迁移规律是指导教育和学习的一种实用理论,根据对迁移的不同类型及其特点和影响学习迁移的各种要素的分析,结合编译原理课程的特点,按照促进学习迁移的教学原则,在编译原理教学中促进积极学习迁移,有助于培养学生的创新思维和解决问题的能力,有利于培养学生的良好学习品德.     

基于惯性定位定向的高铁轨检仪分析研究

根据高铁轨道静态检测的测量需求,设计了一种利用定位定向技术的0级轨检仪,并详细阐述了其构成和工作原理,介绍了其特点。通过对比性分析论证,优选了一种测量精度高、操作方法简单且可大幅度提高测量效率的设计方案。理论仿真表明该系统测量精度能够达到优于1.3mm/km的水平。根据理论仿真结果搭建了原理简易验证设备,结合高铁测控网的测量基准,在一段高铁的弯道铁轨上进行了验证测试,测试结果表明采用定位定向技术的0级轨检仪具备实际工程化的潜力,以及提高测量效率和精度的能力。     

基于Agent的卫星自主控制体系结构

介绍了Agent的一般概念,分析了DS-1型、ST7型、混合型、基于结构分解型,以及基于功能分解等典型卫星自主控制体系结构的组成和实现过程,并在此基础上提出了卫星自主控制体系结构设计应遵循的若干原则。     

费用效能分析的准则探讨

分析通常费用效能分析准则的缺陷，提出了费用效能模糊准则。最后通过一个可靠性优化的例子来说明费用效能模糊准则的应用情况。     

基于解耦和动态补偿的卫星控制系统设计

针对带大型挠性单翼太阳帆板和偏置动量的三轴稳定卫星,研究如何消除星内外干扰对姿态控制精度影响的卫星控制系统的设计问题。首先对星内外干扰进行了数值分析,进而阐明了在经典控制方案中干扰力矩对姿态控制精度的影响,指出经典控制在克服干扰力矩对姿态控制精度影响方面存在的不足之处。然后根据卫星的动力学特点,提出并论证了在设定角动量交换系统标称值条件下基于解耦和动态补偿的卫星控制系统的设计方案。最后深入分析了在该方案下太阳帆板挠性模态的稳定性。     

What next for China in space after Shenzhou?

This article discusses China's ambitions in space now that it seems set to pursue human spaceflight. It suggests that, after sending its astronauts into space, completing orbital rendezvous-docking operations and placing a space lab in orbit, China will focus on the Moon with its Chang’e project. As an emerging space power, China will play a more active role in the international space community through collaboration in areas such as lunar exploration, science operations on the International Space Station, the Galileo Global Navigation Satellite System and the International Geosphere–Biosphere Program (IGBP). In particular, China will vigorously explore new opportunities to expand its cooperation with Russia and ESA to counteract Washington's attempt at containment. Meanwhile, Beijing will continue to follow its self-reliance principle to go its own way in space.