RTK model and positioning performance analysis using Galileo four-frequency observations

This paper proposes a real-time kinematic (RTK) model that uses one common reference satellite for the Galileo system with four frequency observations. In the proposed model, the double-differenced (DD) pseudorange and carrier phase biases among the different frequencies are estimated as unknown parameters to recover the integer features of the DD ambiguities among the different frequencies for ambiguity resolution and precise positioning. Analysis results show that the E5a, E5b, and E5 frequencies have virtually the same performance in terms of the positioning accuracy, observation residuals, and ratio values of ambiguity resolution. However, the E1 frequency performs worse than the E5a, E5b, and E5 frequencies. The RTK results for the combination of multiple frequencies are much better than those for a single-frequency observation, the coordinates’ standard deviation is improved about 20–30%, and the ambiguity fix time is improved about 10%.     

雄安新区人才队伍建设思考

人才是实现民族振兴、赢得国际竞争优势的战略资源,雄安新区建设发展离不开人才的重要支撑。本文以雄安新区人才队伍建设为研究对象,剖析这一研究的意义和现状,探究雄安新区人才队伍建设存在的问题,最后提出解决这一问题的建议。     

Wish 4-D System Successful in China——Interview with Charlie Pellerin

After Charlie Pellerin joined NASA's Goddard Space Flight Center in 1967, he received the Center's highest invention-related award for patenting a     

基于人工地标的移动机器人定位与调整技术

在飞机大型构件测量领域,针对测量设备自动化转站时存在移动机器人无法准确到达站位的问题,提出了采用基于人工地标的移动机器人定位与调整技术实现转站时的精确定位。其次,设计了一种人工地标,给出使用激光跟踪仪的地标标定工装以及标定方法,通过该方法可得到地标在全局坐标系下的坐标。同时,介绍了地标的编码与位姿的解算方法,以及移动机器人位姿调整策略。最后,试验表明,人工地标测量的位置和角度误差均较小,移动机器人通过人工地标的定位与调整后的精度可以满足自动化转站的精度要求。     

金属弹簧管性能影响因素的仿真分析

为了研究高温密封组件金属弹簧性能,本文通过对波音公司编网状弹簧管结构和Streck心脏支架结构的研究,建立了编织弹簧的几何拓扑构型和数学模型,推导了弹簧直径计算公式。采用AUTODESK3D-MAX构建了编织弹簧的仿真模型,用ANSYS仿真软件分别从编织丝直径、编织密度以及编织方法 3方面探究不同测试对弹簧性能的影响。结果表明,增加弹簧丝直径、降低弹簧管轴向方向的编织密度、提高圆周方向的编织密度、向外的弹簧管编织方式可有效提高弹簧管的回弹性能。     

基于火箭橇的无人机碰撞民用飞机试验技术研究

无人机碰撞民用飞机关键部位损伤程度的研究是民航领域关注的新型热点问题。本文首次提出采用 火箭橇试验评估无人机碰撞民用飞机的安全性。通过对碰撞速度、碰撞位置、无人机姿态、参数测量等进行研 究,设计碰撞技术方案,论述火箭橇的设计、弹道控制设计、强度校核和测试方案,并进行试验验证和仿真计算。 结果表明:本文设计的火箭橇碰撞试验方案是可行的,实现了单一弹道上的连续多点碰撞及多视角、全覆盖、高 稳定的全过程记录;可为后续开展同类碰撞试验提供必要的技术参考,所开展的多发次碰撞试验也为无人机碰 撞民用飞机的安全性评估提供了有效的试验数据。     

基于拓扑优化和形状优化的桨叶结构设计

直升机旋翼桨叶剖面结构设计是研究旋翼动力学设计的基础。提出一种联合拓扑优化和形状优化的 两级优化设计方法,可用于桨叶剖面结构的设计。第一级优化以变密度法(SIMP)作为拓扑优化的材料插值方 法,以桨叶体积最小化为设计目标,约束桨叶节点位移和应力,建立桨叶的拓扑优化求解模型;第二级优化以重 构的桨叶模型为基础开展形状优化,降低局部应力集中以及找到合理的边界节点位置。对优化后的模型进行 有限元分析,结果表明:通过拓扑优化和形状优化的两级优化,能够得到满足强度和稳定性要求的结构布局,为 桨叶结构设计提供指导方案。     

前向数据接入方式对导航星座网络通信性能的影响分析

对采用时分多址轮询建链体制的导航星座星间链路网络,为了指导星间链路网络地面前向数据接入的应用,分析了不同地面前向数据接入方式的星-星-地联合数据交互机制及其对网络通信性能的影响,并结合应用代价给出了综合评价和使用建议.以前向数据最快路径接入方式和固定节点接入方式为代表,分析了星间链路网络与地面间星-星-地联合数据交互机...     

Reliability and global sensitivity analysis for an airplane slat mechanism considering wear degradation

This paper focuses on the issue of reliability and global sensitivity analysis for an airplane slat mechanism considering the uncertainties in the wear process of mechanical components. First, the multi-body kinematic model of the slat mechanism is built in the ADAMS software. The geometrical sizes of the roller wheels after wear degradation are considered as input variables and the angle the slat should turn is considered as the output response. To accurately identify the influential roller wheels to the reliability and robustness of the slat mechanism, the failure probability based sensitivity and variance-based sensitivity indices are introduced. Comprehensive analysis of the results have shown that the reliability analysis and global sensitivity theory can help engineers find significant parts by their contributions, thus provide guidance for mechanical design and maintenance.