测量船船摇前馈数据处理方法研究及应用

船摇前馈是航天测量船稳定性设计方法之一。实践证明,船摇前馈对改善系统误差有益,目标速度前馈特别是加速度前馈的改善效果要比船摇前馈的好。分析原因,一方面是目标相对船摇来说变化慢,低频分量多,滤波后能够比较准确地得到所要的值,前馈精度也就高;另一方面是船摇前馈值特别是加速度前馈比较难以准确获得。因此,准确地计算前馈量,是补偿测量设备伺服系统滞后造成的误差,达到高精度地跟踪目标的关键之一。本文详细给出了船摇前馈量的具体计算公式,并在卫星发射任务中进行了应用和验证。     

Solar sail formation flying on an inclined Earth orbit

The versatility of solar sail propulsion can be utilized in the exploration of Earth’s magnetotail. An inclined periodic orbit with respect to ecliptic is possible for a solar sail with its orbital plane in synchronous rotation with the sun. Solar sail evolving on such an inclined orbit is free of Earth shadow. Formation flying of a cluster of sails around such an inclined periodic orbit is investigated in this paper. The solution of the first-order approximation to the linear relative motion is used to qualitatively analyze the configurations of relative orbits. Since the relative motion is unstable, active control is necessary to keep a periodic relative motion. A typical LQR method is employed to stabilize the relative motion. The design method is validated by numerical examples.     

固体火箭发动机／导弹一体化设计

以某一两级固体地—空导弹作为算例,研究了固体火箭发动机/导弹一体化设计问题。研究以导弹起飞质量最轻和可用过载最大为目标建立了目标函数,利用优化理论完成了7个设计变量的优化设计。优化结果表明,所建立的数学模型是正确的。     

Application of Wuhan Ionospheric Oblique Backscattering Sounding System (WIOBSS) for the investigation of midlatitude ionospheric irregularities

An upgrade of Wuhan Ionospheric Backscattering Sounding System (WIOBSS) was developed in 2015. Based on the Universal Serial Bus (USB), and a high performance FPGA, the newly designed WIOBSS has a completely digital structure, which makes it portable and flexible. Two identical WIOBSSs, which were situated at Mile (24.31°N, 103.39°E) and Puer (22.74°N, 101.05°E) respectively, were used to investigate the ionospheric irregularities. The comparisons of group distance, Doppler shift and width between Mile-Puer and Puer-Mile VHF ionospheric propagation paths indicate that the reciprocity of the irregularities is satisfied at midlatitude region. The WIOBSS is robust in the detection of ionospheric irregularities.     

计算机生成兵力

介绍分布交互仿真（ＤＩＳ）环境中计算机生成兵力（ＣＧＦ）的概念,分析ＣＧＦ系统的原理、结构、特点和主要研究内容。介绍现有的ＣＧＦ系统,分析ＣＧＦ系统与人工智能以及ＣＧＦ实体与ＤＩＳ的３种仿真类型之间的关系。     

一种计算开伞动载的实用方法

依据海因里奇开伞动力理论,在计算个表充满时间的连续方程中,考虑了伞顶孔,伞顶部分大透气量织物面积,以及伞衣中、下部分织物透气量对开伞动载的影响。引用了非线性的阻力特征文化曲线［２］,计算伞衣充气过程中阻力特征的变化。并考虑了伞衣充气过程初始瞬时的阻力特征,假设在伞衣初始充气时期的一段时间中,进气口直径为常值,数值上等于［４（ＣＡ）０／Ｃ（ｓｔ）π）］（１／２）。计算实例表明,计算结果与实测数据相比较,其一致性是比较满意的。     

无控航天器与空间碎片再入的工程预测方法研究现状

无控航天器、火箭末级以及空间碎片再入地球大气层后可能未烧尽,残存的小碎片高速撞击地面,对人类安全和生态系统构成极大威胁。提前预测其再入轨迹并采取预防措施能够有效降低地面风险。文章对无控航天器和空间碎片再入工程预测模型,包括航天器模型、动力学模型、气动热模型和烧蚀解体模型的研究现状进行跟踪与总结,也介绍了国内外有公开资料的工程应用软件,并讨论若干关键问题和进一步研究方向。     

基于热管-风冷系统的新能源汽车电机热分析

针对新能源汽车电机紧凑、轻量化、高功率密度和高可靠性的要求,提出基于热管-风冷系统的新型冷却系统。设计了基于热管-风冷系统的电机结构,建立电机有限元热分析模型并验证其可行性;通过有限元模拟,研究该新型电机在额定功率和峰值功率下的温度场。结果表明:热管-风冷系统能有效地控制电机的温升。与水冷系统相比,无需水泵、节温器、水箱、管路以及其他装置,结构简单、紧凑,有利于实现新能源汽车的轻量化和高功率密度。     

Validation on MERSI/FY-3A precipitable water vapor product

The precipitable water vapor is one of the most active gases in the atmosphere which strongly affects the climate. China's second-generation polar orbit meteorological satellite FY-3A equipped with a Medium Resolution Spectral Imager (MERSI) is able to detect atmospheric water vapor. In this paper, water vapor data from AERONET, radiosonde and MODIS were used to validate the accuracy of the MERSI water vapor product in the different seasons and climatic regions of East Asia. The results show that the values of MERSI water vapor product are relatively lower than that of the other instruments and its accuracy is generally lower. The mean bias (MB) was ?0.8 to ?12.7?mm, the root mean square error (RMSE) was 2.2–17.0?mm, and the mean absolute percentage error (MAPE) varied from 31.8% to 44.1%. On the spatial variation, the accuracy of MERSI water vapor product in a descending order was from North China, West China, Japan -Korea, East China, to South China, while the seasonal variation of accuracy was the best for winter, followed by spring, then in autumn and the lowest in summer. It was found that the errors of MERSI water vapor product was mainly due to the low accuracy of radiation calibration of the MERSI absorption channel, along with the inaccurate look-up table of apparent reflectance and water vapor within the water vapor retrieved algorithm. In addition, the surface reflectance, the mixed pixels of image cloud, the humidity and temperature of atmospheric vertical profile and the haze were also found to have affected the accuracy of MERSI water vapor product.     

空间站常用元器件的霉菌敏感性研究

为研究空间站常用元器件的霉菌敏感性,选取空间站常用11大类元器件,针对霉菌对元器件的可能影响进行深入分析。基于空间站特定霉菌环境设计了加速试验方案,研究建立了基于元器件损伤程度的敏感等级分类方法,获取了不同元器件对霉菌的敏感性结果以及对应的敏感部位,为后续空间站用元器件质保工作的完善奠定基础。