共享自动驾驶汽车使用意愿模型及其影响因素

为了构建共享自动驾驶汽车(shared autonomous vehicles，SAV) 的使用意愿模型并分析其影响因素，通过使用时机和使用频率来体现公众对SAV的使用意愿；采用验证性因子分析将态度潜变量转化为潜变量得分，以此将态度潜变量引入传统的有序Logit模型；提出SAV使用意愿的有序Logit模型构建方法，并建立基于个人属性、通勤特征、态度潜变量的SAV使用意愿模型.研究发现:是否使用过滴滴拼车、工作单位停车费、自动驾驶态度对使用时机和3种价格(1，2，3元/km) 下的使用频率有显著影响；使用过滴滴拼车、工作单位收取停车费、支持自动驾驶的群体倾向于频繁地、更早地使用SAV出行；公众期望以1元/km或 2元/km即不超过目前滴滴拼车的价格使用SAV.     

论中国儒家思想中人的发展观

从狭义上讲，人的发展观是关于个体人的发展的最根本的看法。中国传统社会中儒家思想的人的发展观就是在这个意义上讨论的，它着重把人的发展的本质内容理解为人的道德修养。这种人的发展观的形成有其深刻的社会经济根源和政治基础。     

Jane Eyre,a Plain but Spectacular semi-autobiographic Portrait of Charlotte Bronte

Maybe life itself is a endured suffering. This is a story about a special and unreserved woman who has been exposed to a hostile environment but continuously and fearlessly struggling for her ideal life. It is interpreted as a symbol of the independent spirit.Through Jane Eyre,Charlotte Bronte realized her own dream and life pursuit.There she was the master of her own fate.     

The detection of structural deformation errors in attitude determination

In the determination of the attitude parameters from a multi-antenna GPS array, one of the major assumptions is that the body frame is rigid at all times. If this assumption is not true then the derived attitude parameters will be in error. It is well known that in airborne platforms the wings often experience some displacement during flight, especially during periods of initializing maneouvres, such as taking off, landing,and banking. Often it is at these points in time that it is most critical to have the most precise attitude parameters.There are a number of techniques available for the detection of modeling errors.The CUSUM algorithm has successfully been implemented in the past to detect small persistent changes. In this paper the authors investigate different methods of generating the residuals, to be tested by the CUSUM algorithm, in an effort to determine which technique is best suited for the detection of structural deformation of an airborne platform. The methods investigated include monitoring the mean of the residuals generated from the difference between the known body frame coordinates, and those calculated from the derived attitude parameters. The generated residuals are then passed to a CUSUM algorithm to detect any small persistent changes. An alternative method involves transforming the generated residuals into the frequency domain through the use of the Fast Fourier Transform. The CUSUM algorithm is then used to detect any frequency changes. The final technique investigated involves transforming the generated residuals using the Haar wavelet. The wavelet coefficients are then monitored by the CUSUM algorithm in order to detect any significant change to the rigidity of the body frame.Detecting structural deformation, and quantifying the degree of deformation, during flight will ensure that these effects can be removed from the system, thus ensuring the most precise and reliable attitude parameter solutions. This paper, through a series ofsimulations, will assess the effectiveness of the above mentioned techniques for detecting structural deformation effects on a GPS multi-antenna array. These principles are then tested with experimental data.     

浅谈我国大学生政治态度教育效果的分析研究——以江西省某四高校为例

政治态度教育是思想政治教育的重要内容,它直接影响思想政治教育的效果。当前我国大学生政治态度教育的效果如何?本文通过对江西省四所高校的调查,分析了当前大学生政治态度教育效果的现状,并认为,对大学生加强以政治态度教育为内容的思想政治教育对提高大学生的思想政治教育水平具有重要的意义。     

区域地理教育与区域可持续发展

文章论述了可持续发展的形成标志着人类、资源、环境的发展进入新的时期 ,这对建立在以人地关系研究为基础的区域地理学产生深刻的影响 .提出把可持续发展理论纳入到区域地理的教材、教法中 ,作为在区域地理教学中的内容及实现可持续发展教育的基本措施 ,指出实现地理素质教育 ,也就是培养学生的情感、态度、价值观的教育     

对社会调查中常用态度与方法的初步分析

社会调查实际上是由调查者与被调查者双方共同完成的。调查者不是“包打听”，也不是完全的“被告知者”，真实材料的获得要建立在双方相互尊重的前提下；每一种调查方法之间是一种弥补的关系：调查者对调查对象都怀有一种自觉不自觉的价值与情感取向，深刻地影响着调查者对材料的分析。     

大型舰船甲板变形测量

为测量大型舰船甲板的变形，提出了基于多个IMU数据融合的测量方法．建立了甲板变形测量模型．利用最小二乘估计对甲板的变形进行了分析．结果表明，用该方法可以实时估计未安装IMU战位点处的甲板变形，且能减少变形测量系统所需IMU的数量；变形估计精度与IMU的布置有关，当IMU的布置合理时，估计精度优于0．8arcmin．     

基于四元数的导弹反步控制及全方位算法应用

针对传统四元数适应范围小,分析误差困难问题,基于误差四元数的概念深入研究了姿态误差形式和姿态角和四元数全方位转换问题,提出了姿态角和四元数的全方位转换算法。该算法实现了姿态角和四元数的-1800到1800全空间转换,并且具有抗扰动的能力,同时将四元数与非线性反步(backstepping)方法结合,进行了导弹姿态控制。仿真表明了全角度算法的正确性,以及基于文中的四元数姿态误差方程可有效进行导弹全方位姿态控制。     

飞行器三轴姿态测量方法

介绍了到目前为止常用飞行器三轴姿态测量敏感器.详述了这些姿态敏感器的工作原理.根据这些原理分析了它们的优缺点,并比较了它们的性能指标.给出了具有指导意义的结论.