基于CCSDS的遥科学试验台通信链路的概念研究

为了有效地利用空间站资源,提出了遥科学的概念。利用空间站的微重力环境所做的各种科学实验,需要空地间交互地进行通信,空间数据系统咨询委员会（ＣＣＳＤＳ）为这种通信键路制定了一系列标准。着重讨论了遥科学对通信链路的要求,适于遥科学实验的空间数据系统模型以及天基、地基通信系统框图。     

航天器复杂约束姿态机动的自主规划

 研究了星载设备经受动态环境的多种几何约束和动力学约束时,航天器姿态机动历程的星上规划方法。将完整姿态映射为三维姿态描述空间中的点,姿态路径的规划问题转化为中间节点的规划。随机搜索空间中的一组节点,在相邻节点间采用施加动力学约束的Euler转动姿态制导律,并考查Euler转动过程中的几何约束。用快速搜索随机树方法搜索到可行解,再利用姿态空间特性对路径加以优化。仿真显示算法能在大范围内快速得到可行解,优化措施有助缩短机动时间。离散化的节点规划保证了复杂约束情况下解的有效性,并具有概率完备性。     

Crack monitoring method based on Cu coating sensor and electrical potential technique for metal structure

Advanced crack monitoring technique is the cornerstone of aircraft structural health monitoring.To achieve real-time crack monitoring of aircraft metal structures in the course of service,a new crack monitoring method is proposed based on Cu coating sensor and electrical potential difference principle.Firstly,insulation treatment process was used to prepare a dielectric layer on structural substrate,such as an anodizing layer on 2A12-T4 aluminum alloy substrate,and then a Cu coating crack monitoring sensor was deposited on the structure fatigue critical parts by pulsed bias arc ion plating technology.Secondly,the damage consistency of the Cu coating sensor and2A12-T4 aluminum alloy substrate was investigated by static tensile experiment and fatigue test.The results show that strain values of the coating sensor and the 2A12-T4 aluminum alloy substrate measured by strain gauges are highly coincident in static tensile experiment and the sensor has excellent fatigue damage consistency with the substrate.Thirdly,the fatigue performance discrepancy between samples with the coating sensor and original samples was investigated.The result shows that there is no obvious negative influence on the fatigue performance of the 2A12-T4 aluminum alloy after preparing the Cu coating sensor on its surface.Finally,crack monitoring experiment was carried out with the Cu coating sensor.The experimental results indicate that the sensor is sensitive to crack,and crack origination and propagation can be monitored effectively through analyzing the change of electrical potential values of the coating sensor.     

Pre-correction X-ray pulsar navigation algorithm based on asynchronous overlapping observation method

In order to shorten the data update period and further improve the accuracy, a pre-correction X-ray pulsar navigation algorithm based on asynchronous overlapping observation method is proposed. The asynchronous overlapping observation method partially overlaps the two adjacent observation periods, so that the data update period depends on the minimum pulsar observation period rather than the maximum like the other algorithms. The number of sampling points is also reduced to 2, which will effectively reduce the calculation burden. The proposed pre-correction extended Kalman filter uses observation data of adjacent sampling points to achieve a two-fold correction and makes up for the problem of insufficient observations on some sampling points caused by the observation method. Finally, simulations show that the proposed algorithm reduces the position and velocity errors by 21.55% and 19.13% compared to the EKF based on asynchronous observation method when using three detectors to observe the corresponding pulsars simultaneously. At the same time, the running time of one data update calculation is only 6.6% more than that of the EKF algorithm based on synchronous observation method.     

Active vibration suppression for flexible satellites using a novel component synthesis method

This paper is devoted to developing a closed-loop vibration suppression controller for a satellite with large flexible appendages based on component synthesis vibration suppression (CSVS) method. The dynamics model of a flexible satellite is firstly established by using the Newton–Euler methodology, and the dynamics model of the flywheel is also developed. A novel CSVS method is presented based on zero-vibration differentiator (ZVD), which can guarantee multi-order vibration suppression. Combined with the proposed CSVS method, traditional closed-loop controllers such as PD or sliding mode controllers can be applied to active vibration suppression. The stability of the proposed closed-loop CSVS controller is proved by the Lyapunov theory. Subsequently, the dynamic optimal control allocation algorithm is proposed for six flywheels, and a novel nonsingular fast terminal sliding mode controller is developed to obtain practical voltage control input for the flywheel drive control system. Finally, numerical simulations are carried out to validate the effectiveness of the proposed method.     

美国深空测控通信技术动向分析

文章详细介绍了美国深空测控通信技术的发展动向,并对其未来规划进行了较为详细的综述和分析。     

一种自适应协方差矩阵旋转变换卡尔曼滤波算法及其应用

在被动方式下对目标进行跟踪 ,由于系统的可观性较弱 ,很容易引起状态误差协方差矩阵的过早跳变而导致系统发散。为此 ,本文研究了一种新的卡尔曼滤波算法 -自适应协方差矩阵旋转变换卡尔曼滤波算法 ,并将其应用于水面目标被动跟踪。由于该算法的协方差更新采用状态滤波值计算雅可比矩阵 ,因而具有更好的一致性。仿真结果表明 ,该算法可以克服观测模型线性化误差带来的不良影响 ,改善由于观测噪声的统计特性不能精确已知而导致的滤波不稳定问题 ,具有良好的鲁棒性、快速性和精确性。     

深空网干涉测量数据对嫦娥五号定轨能力分析

针对嫦娥五号探测器(CE-5)开展基于深空网测量数据的定轨能力分析.首先从测量原理分析了深空网VLBI数据的误差源,然后利用CE-5的精密轨道评估了 VLBI数据的误差,最后基于实测数据与协方差分析理论,分析UXB与VLBI数据的定轨能力.结果表明:转移阶段,单独利用深空网测量数据可以获取优于1 km的转移轨道精度,标...     

轴流压气机中喘振和旋转失速的数值模拟

基于轴流压气机逐级过失速特性，建立了多级轴流压气机过失速瞬态，包括喘振或旋转失速的分析模型。发展了分析轴流压气机过失速响应的动态滞后方法，并确定了压气机过失速响应的统一时间滞后常数。对一实验轴流压气机的过失速瞬态进行了数值模拟，与实验结果的一致性较好。     

钣料压延数值解

本文采用能量条件的硬化模式,考虑到钣料的厚向异性,导出了压延凸缘区和凹模圆角区数值解所需的理论方程以及压延拉伸失稳条件的数学表达式和压延拉伸失稳临界载荷计算公式,在此基础上,利用电子计算机求解了四种钣料(TA1—M、LY12—M、LF2—M、20钢)的压延载荷和极限压延系数。理论和实验结果取得了很好的一致性。