Fault rupture model of the 2008 Dangxiong (Tibet,China) Mw 6.3 earthquake from Envisat and ALOS data

On October 6, 2008, an Mw 6.3 earthquake occurred in Dangxiong county, southern Tibetan Plateau. In this study, Synthetic Aperture Radar (SAR) images from Envisat ASAR C-band descending Track 176 and ALOS PALSAR L-band ascending Track 500 are processed to generate the coseismic deformation caused by the earthquake. To estimate the source model, a downhill simplex non-linear inversion method is used to determine the fault rupture geometry, and an automatic fault discretization technique is employed to divide the fault plane to construct the optimal slip model, in which the uncertainties of the fault parameters are assessed by a Monte Carlo method. The inversion results show that the earthquake strikes almost south–north and has a normal faulting focal mechanism with rake angle and slip of −111.7° and 1.33 m, respectively. Peak slip of 2.15 m is located at a depth of 7.5 km. The estimated geodetic moment is 4.06 × 10¹⁸ N m (Mw 6.37), 71.2% of which is released in the depth range 4.5–11 km. The slip model suggests that coseismic slip also takes place at some fault patches near the earth’s surface and postseismic afterslip occurs below the coseismic rupture area after the earthquake.     

大尺寸测量系统配置中包络性与可达性分析

构建了包络性和可达性分析的原理与公式，定量判定当前测量设备空间位置是否合理，为实现在大尺寸测量方案规划阶段对测量设备的可行空间进行快速有效的规划提供依据。阐述了大尺寸测量系统总体架构与阶段任务划分，定义了包络性与可达性的输入输出关系。论述了包络性与可达性的原理与公式，包括可测量体素和外包络体的定义、数学模型和推导公式以及判定公式。最后，在CATIA环境下开发包络性和可达性分析工具，并以机翼翼肋为例，对该翼肋上待测关键特征进行包络性和可达性仿真分析。仿真结果表明，该包络性与可达性分析的原理与公式是可行的。     

力值加载校准系统误差补偿方法研究

针对飞机液压系统地面测试设备校准方法和校准装置欠缺的问题,为了提高飞机液压系统地面测试设备的测试性能和可靠性,设计了一套力值加载校准系统,该校准系统能够按着设置的参数输出精确的力值,实现对飞机液压系统地面测试设备的校准.满足了飞机液压系统地面测试设备对校准方法和校准装置的需求.     

小型飞机座舱加温系统原理及使用维护分析

以小型飞行培训教练机PA44-180双发四座飞机为例,针对其座舱加温系统从构造、工作原理以及组成等方面进行论述,重点针对近三年该系统发生的各类故障进行统计分析,并提出了该系统在日常使用维护过程中的重点注意事项。     

国外舰载飞机着舰进近适配性评估技术研究

通过对国外舰载飞机在着舰进近下滑中的操纵需求分析,提出舰载飞机着舰进近适配性的评估要求。在评估要求的基础上针对飞机在进近适配性方面相关的特性给出相应的飞行试验方法和分析方法,初步建立舰载飞机着舰进近适配性评估技术和方法。     

SJ-9A/B Satellites Conduct Key Technology Tests

On October 14, two satellites SJ-9A/B were sent into their preset orbits by a LM-2C/SMA launch vehicle, which is the first flight of a series of China’s civilian technology experimental satellites. SJ-9A and B are the first two satellites in the series of civilian technology experimental satellites designed for tests such as long lifetime and high reliability, high precision and high performance of satellite, domestically developed core components, satellite formation and     

LM-2C Used in SJ-9A/B Mission

At 11:25 a.m. on October 14, China successfully sent the SJ-9A/B satellites into their preset transfer orbits with one LM-2C launch vehicle from the Taiyuan Satellite Launch Center. The LM-2C launch vehicle used for the mission was manufactured by China Academy of Launch Vehicle Technology (CALT) of China Aerospace Science and Technology Corporation (CASC). The launch marked the 169th launch of the Long March series launch vehicle. The launch vehicle used for the mission differs not much from     

ω混沌与伪移位不变集

就紧致度量空间的连续自映射 ,研究了具有半伪移位不变集与 ω混沌的关系。证明了若 f有半伪移位不变集 ,则 f是ω混沌的且存在不可数集 S R(f ) - R(f ) ,其中 S既为 f的ω紊乱集又为 f的 L i- Yorke意义下的混沌集。进而导出一维映射 f拓扑熵大于零的充要条件是存在正整数 n,使得 fnω混沌且存在 fn 的不可数的 ω紊乱集 S R(f) - R(f)     

形态句法视角下教师话语错误分析

随着双语教学走进中国课堂,教师话语分析研究开始受到越来越多的关注.这是因为双语教学中的教师话语不仅起到信息传递和教学活动管理的作用,而且更构成了学习者的主要外语输入渠道.本文拟将通过一项工科双语开放课程的实证研究,从形态句法角度对本课程教师话语中的主要错误进行归纳整理,并在此基础之上从三大维度推导出错误诱因.