InSight Mars Lander Robotics Instrument Deployment System

The InSight Mars Lander is equipped with an Instrument Deployment System (IDS) and science payload with accompanying auxiliary peripherals mounted on the Lander. The InSight science payload includes a seismometer (SEIS) and Wind and Thermal Shield (WTS), heat flow probe (Heat Flow and Physical Properties Package, HP³) and a precision tracking system (RISE) to measure the size and state of the core, mantle and crust of Mars. The InSight flight system is a close copy of the Mars Phoenix Lander and comprises a Lander, cruise stage, heatshield and backshell. The IDS comprises an Instrument Deployment Arm (IDA), scoop, five finger “claw” grapple, motor controller, arm-mounted Instrument Deployment Camera (IDC), lander-mounted Instrument Context Camera (ICC), and control software. IDS is responsible for the first precision robotic instrument placement and release of SEIS and HP³ on a planetary surface that will enable scientists to perform the first comprehensive surface-based geophysical investigation of Mars’ interior structure. This paper describes the design and operations of the Instrument Deployment Systems (IDS), a critical subsystem of the InSight Mars Lander necessary to achieve the primary scientific goals of the mission including robotic arm geology and physical properties (soil mechanics) investigations at the Landing site. In addition, we present test results of flight IDS Verification and Validation activities including thermal characterization and InSight 2017 Assembly, Test, and Launch Operations (ATLO), Deployment Scenario Test at Lockheed Martin, Denver, where all the flight payloads were successfully deployed with a balloon gravity offload fixture to compensate for Mars to Earth gravity.     

新时期高校大学生美术意识的培养

在美育教育教学过程中提高学生的美术意识,是培养具有创新意识和创新能力的新型美术人才的关键环节,在美育教育过程中,通过改善教学条件与教学手段,促进学生的创新意识以及利用现代科学技术等措施来提高学生的意识水平。     

文学话语的蕴藉及审美效果

为了弥补在文学语言中的不足,形成了以象寓意的话语蕴藉现象。本文运用了列举、分析等方式诠释话语蕴藉与文学词语、文学修辞、标点符号及文章结构之间的联系,揭示出文学话语蕴藉带给读者的丰富想象和再创造的审美空间。     

六点炉温追踪仪在涂装线上的应用

六点炉温追踪仪（ＢＹＫＯ－ＴＲＡＣＫ）能准确、科学的测试各种不同结构烘房的温度曲线。本文介绍了该仪器在烘房的工艺设计、工件烘烤质量及涂料选材等方面的应用。     

小展弦比飞翼布局作战飞机可控性设计方法

 飞翼布局飞机取消了常规布局飞机采用的安定面和操纵面,由此引起其可控性设计的诸多新问题。以某小展弦比飞翼布局作战飞机为例,利用风洞试验结果研究了几种典型新型操纵面的操纵新机理及不同飞行条件下的操纵效能等。基于可控性设计的要求,估算了该飞翼构型作战使用所需的三轴最大控制力矩系数。通过引进舵容量的概念提出了新型操纵面的参数化设计方法,最后对这一新布局方案进行了可控性评估,为飞翼布局飞机概念设计阶段的新型操纵面布置和设计提供了一种实用的方法。     

旋转对小间隙篦齿-蜂窝结构封严特性的影响

在不同旋转速度,气动参数及衬套结构下,对两种齿型的篦齿结构的封严特性进行了实验研究,篦齿实验件的旋转速度变化范围为0～2718 r/min,上游气体压力变化范围为0.2～0.71 MPa.结果表明:篦齿-蜂窝封严结构的封严特性与普通篦齿结构相似,即增加篦齿前后腔压比,泄漏系数逐渐增加但增加幅度趋于平缓;当节流间隙很小时,相对普通篦齿封严结构而言,采用蜂窝衬套后泄漏量有所增加;齿尖周向速度在低于27.13 m/s时,齿间压力及泄漏量基本不发生变化.     

Quantifying lunar soil composition with partial least squares modeling of reflectance

Retrieval of lunar soil composition is commonly achieved through optical remote sensing in which spectral characteristics of returned lunar samples are related to their constituents. Partial least squares (PLS) and principal component regression (PCR) were applied to the dataset characterized by the Lunar Soil Characterization Consortium (LSCC) to estimate the content of FeO, Al₂O₃ and TiO₂ in the soils. The goal of this study was to test whether the conversion of reflectance to single scattering albedo (SSA) via Hapke’s radiative transfer model is able to improve the performance of PLS and PCR. Results from PLS and PCR modeling of SSA spectra indicate that the conversion does not necessarily improve the performance of PLS and PCR, and this depends on the chemical considered, the way to select the number of optimal factors, and how the data were pretreated. The conversion failed to accommodate the large deviation of highland samples with low FeO, TiO₂ and high Al₂O₃.     

基于灰色模型的捷联惯组历次测试数据分析

捷联惯组历次测试数据反映了捷联惯组的逐次通电稳定性,它是引起制导工具误差的主要影响因素。本文采用建立捷联惯组历次测试数据灰色模型的方法对其逐次通电稳定性的变化趋势进行预测。通过仿真计算,验证了利用该方法进行短期预测的有效性。     

二茂铁功能化SBA-15的制备及其对AP／HTPB固体复合推进剂燃烧催化作用研究

二茂铁(Fc)及其衍生物是AP/HTPB固体复合推进剂的有效燃速催化剂,但在推进剂中的迁移始终是其应用的最大障碍。将二茂铁通过缩合反应接枝到介孔材料SBA-15的表面,制备了一种低迁移催化剂Fc-SBA-15。X射线衍射和N2吸附-脱附实验表明,Fc均匀致密地固定在了SBA-15的内外表面,Fc的负载没有对SBA-15的介孔结构造成破坏。改进的迁移性实验表明,制备的Fc-SBA-15复合材料是一种低迁移的催化剂。Fc-SBA-15对AP的热分解与AP/HTPB推进剂的燃烧具有较好的催化效果,添加2%的Fc-SBA-15使AP的高温热分解峰温度降低64℃,使AP/HTPB固体复合推进剂的燃速提高43%,压强指数下降30%。