碳硼复合渗研究及其应用

本文研究了２０钢和４５钢的碳硼复合渗渗层组织及耐磨性能。结果表明：复合渗可得到较强支撑作用的过渡层,从而使渗硼层耐磨性提高。饲料粉碎机锤片采用复合渗工艺处理后试用效果良好。     

一种使用Rhapsody-Simulink 工具链开发嵌入式软件的方法

描述了一种以DOORS 管理的软件需求为输入,用Rhapsody 进行软件框架建模并验证,而对部分软 件单元使用Simulink 进行详细设计、验证,然后将Simulink 模型导入Rhapsody 模型中形成完整软件配置项的 嵌入式软件开发方法。     

GRACE gravity field modeling with an investigation on correlation between nuisance parameters and gravity field coefficients

The GRACE (Gravity Recovery And Climate Experiment) monthly gravity models have been independently produced and published by several research institutions, such as Center for Space Research (CSR), GeoForschungsZentrum (GFZ), Jet Propulsion Laboratory (JPL), Centre National d’Etudes Spatiales (CNES) and Delft Institute of Earth Observation and Space Systems (DEOS). According to their processing standards, above institutions use the traditional variational approach except that the DEOS exploits the acceleration approach. The background force models employed are rather similar. The produced gravity field models generally agree with one another in the spatial pattern. However, there are some discrepancies in the gravity signal amplitude between solutions produced by different institutions. In particular, 10%–30% signal amplitude differences in some river basins can be observed. In this paper, we implemented a variant of the traditional variational approach and computed two sets of monthly gravity field solutions using the data from January 2005 to December 2006. The input data are K-band range-rates (KBRR) and kinematic orbits of GRACE satellites. The main difference in the production of our two types of models is how to deal with nuisance parameters. This type of parameters is necessary to absorb low-frequency errors in the data, which are mainly the aliasing and instrument errors. One way is to remove the nuisance parameters before estimating the geopotential coefficients, called NPARB approach in the paper. The other way is to estimate the nuisance parameters and geopotential coefficients simultaneously, called NPESS approach. These two types of solutions mainly differ in geopotential coefficients from degree 2 to 5. This can be explained by the fact that the nuisance parameters and the gravity field coefficients are highly correlated, particularly at low degrees. We compare these solutions with the official and published ones by means of spectral analysis. It is found that our solutions are, in general, consistent with others in the spatial pattern. The water storage variations of the Amazon, Chari and Ganges river basins have also been computed. The variations computed with the NPARB approach are closer to those produced by JPL and DEOS solutions, while the variations produced with the NPESS approach are in good agreement with those produced by the CSR and GFZ solutions. A simulation study is implemented with considering realistic noise and low-frequency error. The two approaches are used to recover the true model. The NPESS solution appears closer to the true one. Therefore we are inclined to estimate the nuisance parameters simultaneously with the geopential coefficients.     

类IXV飞行器初期再入制导与姿态控制方法研究

摘要： 针对类IXV飞行器无翼式升力体构型及采用RCS/尾襟翼组合控制特点,研究其初期再入段的高精度制导与姿态控制方法.设计带过程约束的数值预测 校正制导律以提高制导系统的鲁棒性及精确性;根据其执行机构配置特点,设计基于RCS的航向控制律及基于RCS/气动舵的纵、横向复合控制律,并采用鲁棒伺服LQR技术进行控制参数快速设计.通过蒙特卡洛打靶仿真来验证算法的精度及鲁棒性.     

RNSS/INS深耦合高动态导航接收机测试方法研究CSCD

卫星导航和惯性导航采用深耦合方式实现导航作为世界上最先进的导航形式,在国防中的应用越来越广泛,但其在高动态下的性能需要验证。当前针对深耦合高动态下导航接收机的测试研究较少,本文介绍了基于卫星信号模拟器的测试系统组成及测试用高动态场景,运用模拟测试原理,通过对导航接收机在高动态下定位速度和跟踪灵敏度的测试及其结果分析,验证了导航接收机的深耦合功能,对此类接收机的测试方法进行了初步探究。     

一种基于OPTICS聚类的仅测角导航目标检测算法

仅测角自主导航方法具有设备简单、复杂度低,功耗低的优点,在空间任务中具有广泛的应用前景.针对中远距离下空间目标特征少的特点,提出了一种利用基于OPTICS聚类算法的空间目标检测方法,可用于仅测角导航过程中的目标检测.对原始星图进行预处理提取星点及目标点,并结合星图识别的结果选择部分帧,使用经过改进的OPTICS聚类方法获得目标运动轨迹.最后,使用本文中的算法对软件仿真出的含有目标的高精度星图进行处理验证了算法的可行性.在卫星相对于空间目标抵近过程中,目标检测的水平误差及垂直误差小于0.15°的帧数分别占到了85.4%以及99.6%.相比AVANTI实验中的目标检测方法,减少了在轨任务中相关参数的调节,进一步提升了算法的自主性.     

《客舱服务技能》课程教学的改进与思考

《客舱服务技能》是空乘专业的一门专业必修课程。在课程改革中,如何改进《客舱服务技能》的教学效果是我们需要关注的重点。本文从目前该课程发展状况、师资、教材、实训条件、教学方法等方面对该课程的建设情况及存在的问题进行了分析与探讨。     

某型涡轮轴发动机稳态气路故障诊断方法

本文是涡轮轴发动机稳态气路故障诊断方法研究的结果。根据监控功能要求 ,应用气路参数分析法 ,确定反映部件性能参数变化的测量参数 ,建立故障诊断模型 ,探讨分别应用 6个和 4个测量参数诊断气路部件故障的方法     

双轴式涡喷发动机的转差线图确定方法的研究

转差是双轴式发动机交付验收参数之一 ,交付发动机的转差是依据该型的标准转差线图调整和确定的 ,标准转差线图确定得合适程度关系到发动机外场使用的性能、稳定性和可靠性。本文比较系统地论述了双轴式涡喷发动机的转差线图的制作和使用 ,分析了转差线图上、下限界对发动机的影响 ,提出了用工作点检查法和稳定工作裕度检查法解决转差线图上、下限界的确定问题。解决了某新机转差线图的确定依据。本方法可用于新机研制中标准的转差线图确定 ,建议二种检查方法结合使用     

不确定性系统鲁棒H∞/H2混合控制在航空发动机中的应用

将结构参数不确定性问题引入到参数化的一般 H∞ 控制器中 ,并考虑 H2 性能指标 ,提出了 1种被控系统中存在结构参数不确定性的混合 H∞ /H2 控制器的设计方法 ,给出了相应问题求解的充分必要条件 ,问题的解归结为求解 3个 Riccati方程。设计的控制器在某型双转子涡喷发动机气动热力学非线性模型上进行了仿真验证