Positioning error compensation for parallel mechanism with two kinematic calibration methods

Compared with serial mechanisms, the parallel mechanism (PM) theoretically exhibited higher positioning accuracy, dynamic performance, strength-to-weight ratio, and lower manufacturing cost, but they had not been widely used in the practical application. One key issue, positioning accuracy, which directly affected their performance and was greatly influenced by the errors of kinematic structure parameters was analyzed. To effectively enhance the positioning precision of PMs, a novel modeless kinematic calibration method, namely the split calibration, was presented and its compensation effect of the positioning error was comprehensively compared with that of an integrated method on two different types of PMs. A strange phenomenon-correct and incorrect identified results were derived from two different PMs by the same integrated method, respectively-which had not been reported yet was discovered, and the origin of it was revealed utilizing numerical simulations. Finally, respective merits and drawbacks of these two methods obtained in this paper provided underlying insights to guide the practical application of the kinematic calibration for PMs.     

A deployable mast for solar sails in the range of 100–1000 m

The purpose of this paper is to introduce a new deployable mast design that may provide a means to scale up solar sails to very large dimensions. The paper describes the basic analytical approach for truss beams, compares this new design with the state-of-art truss used in NASA’s solar sail development work, and provides analyses of novel applications enabled by the mast design.     

飞机结构完整性及损伤类型的探究

特定区域的结构完整性监管不仅贯穿于飞机的整个服役阶段,同时也为适航性安全提供了保障.文中主要讨论了非裂纹损伤形式与传统裂纹损伤的关键性区别,说明了非裂纹损伤形式对现有的结构完整性设计方法提出的挑战.此种损伤类型不同于目前广泛研究的传统裂纹损伤,易造成预料之外及早期的机组结构破坏,给飞机维护及结构的完整性带来了威胁.最后对现有的结构完整性设计和管理方法提出了参考意见,并对未来可能面临的挑战提出建议,对实施和完善现有的飞机结构完整性管理方法有一定的参考价值.     

空间探测磁强计安装部件的力学特性分析

对某深空探测器中的有效载荷-高精度磁强计的安装部件进行了有限元分析,分别获取了磁强计安装部件在升空过程中承受40g加速度冲击载荷以及-180～75℃的极限温度情况下,在x,y,z方向上的最大应力和最大位移,给出了由于磁强计安装部件的变形而导致的三个探头在x,y,z方向上的偏转角度,采用扫频实验法分析了磁强计安装部件的频谱特性,为空间探测磁强计的设计提供了依据.     

新型充气展开遮光罩设计方案研究和仿真分析

设计一种充气展开遮光罩结构,实现径向和轴向依次展开.提出遮光罩的结构方案、折叠方式和结构中各组件合适的材料,使得结构展开状态和折叠状态分别能够达到一定的尺寸要求.文章还对充气展开遮光罩进行静力分析和展开过程仿真,仿真分析结果表明,遮光罩能够顺利展开,遮光罩壁保持理想的工作表面.     

半硬式平流层飞艇龙骨结构设计与有限元分析

文章基于内部带有龙骨的半硬式平流层飞艇的结构设计,应用ANSYS有限元分析软件建立了龙骨的计算模型。对约束条件以及结构单元参数进行了分析,得到了龙骨结构在重力载荷作用下的应力和变形。计算结果符合结构设计规范的要求,可以为半硬式平流层飞艇的结构设计提供参考。     

片梭织机散件装配结构流程图的绘制及应用

介绍了片梭织机的结构，并应用系统原理绘制出片梭织机散件装配结构流程图。从而解决了在没有零件装配图的情况下，装配散件片梭织机的问题。     

开发教学管理网络系统实现现代化教学管理

该教学管理网络系统根据教学管理内容和科学、规范、高效等现代化管理要求进行研发，采用信息技术使教学管理达到高效、快速、安全、可靠、开放、共享、交互、协调等现代化管理要求；系统由先进的开发工具进行开发。体系结构采用客户机／服务器（C／S）和浏览器／服务器（B／S）相结合的三层体系结构。     

基于VPX架构的遥测采集平台设计

当今世界各航天大国都在大力发展航天测控通信技术,但现有测控设备间连接关系复杂,不利于系统小型化、低功耗设计,很难满足新型飞行器的设计需要。针对现阶段测控通信系统提出的一体化、小型化,高可靠性等要求,对VPX总线架构进行研究,并应用于遥测采集平台设计。提出了基于VPX架构的遥测采集平台设计方案,经试验验证,可满足目前测控通信系统提出的小体积、高速率以及高可靠性共存的设计需求,在航天领域具有广阔的发展前景。     

Mars Express/ASPERA-3/NPI and IMAGE/LENA observations of energetic neutral atoms in Earth and Mars orbit

The low energy neutral atom imagers on Mars Express and IMAGE have revealed that the neutral atom populations in interplanetary space come from a variety of sources and challenge our current understanding of heliospheric physics. For example, both in cruise phase and at Mars, the neutral particle instrument NPD on Mars Express observed “unexplained neutral beams” unrelated to Mars which appear to be either of heliospheric or solar wind origin. Likewise, the NPI instrument on Mars Express has revealed streams of neutral atoms with different properties than those observed by NPD. Independently, IMAGE/LENA has reported neutral atom observations that may be interpreted as a “secondary stream” having different characteristics and flowing from a higher ecliptic longitude than the nominal upstream direction. Both sets of observations do not appear to fit in easily with the neutral atom environment from 1.0 to 1.57 AU as it is currently understood. In this paper, we examine some highly suggestive similarities in the IMAGE/LENA and Mars Express/ASPERA-3/NPI data to try to determine potential origins for the observed signal.