图像三要素与MTF的分析研究

中低分辨率在轨运行卫星遥感器的调制传递函数（Modulation Transfer Function，MTF）的监测一直是研究的难题。现提出的方法解决了中低分辨率在轨运行卫星遥感器MTF监测的关键技术。考虑到卫星遥感器的最终产物是遥感图像，从图像信息理解的三要素出发，即灰度、纹理和边缘，分析图像三要素与遥感器MTF的关系。在分析过程中，应用主成分分析方法，不仅对多组原始数据进行了简化，而且对图像参数进行了降维。通过与其它方法的比较，进一步验证了使用主成分分析方法降维的有效性；同时实验结果亦表明了主成分分析方法的可靠性。最后建立了图像单个综合参数与MTF的关系模型，拟合结果说明，此模型能较好地表达图像参数与MTF之间的关系，这将为在轨运行条件下的建模提供十分重要的技术支持。     

飞机结构腐蚀疲劳寿命预估工程方法研究

简要地说明了飞机结构在腐蚀环境中的破坏模式、腐蚀破坏的分析预估方法和结构服役日历年限预估方法。通过算例说明了分析过程。     

线结构光传感器的数学模型及其测试方法

研究了线结构光传感器的数学模型，并给出了齐次坐标系下的表达形式。根据线结构光传感器的特点，提出了一种用简单的齿形靶及一个一维工作台实现求光平面在摄像机坐标系的位置参数的高准确度的测试方法，解决了对抽象光平面的瞄准问题。通过实验验证，证实了这种测试方法的可行性。     

一种氧杂蒽酮类海洋抗污损天然产物振动光谱的理论研究

基于 Gaussian 09W软件包,采用 DFT-B3LYP方法,研究了 1种来源于红树林未知真菌的海洋抗污损天然产物——6,8-di-O-methyl versiconol。先用 3-21G基组,再用 6-311G基组计算了分子的最稳定构型及其前线分子轨道分布。分析稳定构型发现,以蒽二酮为主体的分子是 1个三维非平面的结构,并且分子内部形成了 1个大的 π共轭体系。在最稳定构型的基础上,用同样的理论方法和 6-311G基组计算了该分子的红外振动频率及拉曼光谱频率,根据红外和拉曼光谱的振动频率特点,将红外光谱和拉曼光谱分成 3个区域,讨论了 2种光谱在各区域的特征峰的位置、振动特点、振动模式等,为氧杂蒽酮类海洋抗污损天然产物分子的振动光谱检测和分子结构的鉴定,提供了光谱解析方面的理论依据。     

一种负升力超高声速临近空间突击飞行概念

提出一种飞行高度70 km以上的超高速临近空间飞行概念,旨在通过火箭发动机克服大气阻力作用,通过负升力达到"增加"地球引力常数的等效效果,实现高于地球环绕速度的突击飞行,具有速度快、航程远的特点.分析了等高度巡航过程的受力情况,对气动参数选取、能量需求等问题进行了分析,给出了这类飞行器可能运行的空间区域.分析表明,该飞行方式可以实现在40 min内全球到达.     

Reliability and Sensitivity Analysis of Transonic Flutter Using Improved Line Sampling Technique

The improved line sampling (LS) technique, an effective numerical simulation method, is employed to analyze the probabilistic characteristics and reliability sensitivity of flutter with random structural parameter in transonic flow. The improved LS technique is a novel methodology for reliability and sensitivity analysis of high dimensionality and low probability problem with implicit limit state function, and it does not require any approximating surrogate of the implicit limit state equation. The improved LS is used to estimate the flutter reliability and the sensitivity of a two-dimensional wing, in which some structural properties, such as frequency, parameters of gravity center and mass ratio, are considered as random variables. Computational fluid dynamics (CFD) based unsteady aerodynamic reduced order model (ROM) method is used to construct the aerodynamic state equations. Coupling structural state equations with aerodynamic state equations, the safety margin of flutter is founded by using the critical velocity of flutter. The results show that the improved LS technique can effectively decrease the computational cost in the random uncertainty analysis of flutter. The reliability sensitivity, defined by the partial derivative of the failure probability with respect to the distribution parameter of random variable, can help to identify the important parameters and guide the structural optimization design.     

Failure Analysis for Fatigue Crack of Fuel-oil Cooler of a Certain Type of A/C

针对某型教练机燃滑油散热器产生裂纹导致燃油泄漏的故障现象,进行了地面开车试验,同时,对燃油系统和燃滑油散热器的压力、温度、流量等进行了测量,根据测量数据分析,找出了燃滑油散热器产生疲劳裂纹的原因.     

形状及旋转角度对非球铝颗粒受力的影响分析

固体火箭发动机内铝金属颗粒在运动过程中会发生变形和旋转。针对所产生的非球颗粒受力问题,采用数值模拟方法,对初始半径为100μm的铝颗粒,处于不同形状和旋转角度情况下的受力情况进行了分析计算。结果表明,外形严重偏离球体时,颗粒表面所受到的压差阻力系数与粘性阻力系数均大于当量直径下的计算值,其总阻力系数与经验公式计算所得的结果大不相同,需对其进行相应修正。在平行于来流的方向上,旋转角度改变时,颗粒所受阻力系数差值最大为5%,其中粘性阻力系数最大相差达18.9%。在垂直于来流方向上,颗粒的升力系数很小,最大值不足平行于来流方向上阻力系数的20%。     

Design and experiment of onboard laser time transfer in Chinese Beidou navigation satellites

High-precision time synchronization between satellites and ground stations plays the vital role in satellite navigation system. Laser time transfer (LTT) technology is widely recognized as the highest accuracy way to achieve time synchronization derived from satellite laser ranging (SLR) technology. Onboard LTT payload has been designed and developed by Shanghai Astronomical Observatory, and successfully applied to Chinese Beidou navigation satellites. By using the SLR system, with strictly controlling laser firing time and developing LTT data processing system on ground, the high precise onboard laser time transfer experiment has been first performed for satellite navigation system in the world. The clock difference and relative frequency difference between the ground hydrogen maser and space rubidium clocks have been obtained, with the precision of approximately 300 ps and relative frequency stability of 10E−14. This article describes the development of onboard LTT payload, introduces the principle, system composition, applications and LTT measuring results for Chinese satellite navigation system.