天宫一号大气密度探测数据与模式的比较分析

利用天宫一号的轨道大气环境探测器在2012年12月7日至2013年1月4日,地磁活动平静下的大气密度探测数据,与NRLMSISE-00和JB2008模式进行比较。与实测数据相比,NRLMSISE4）0模式整体高估11．6％,而JB2008整体低估9．8％。JB2008模式在逐日变化趋势方面与实测结果更吻合,更好地反映了太阳辐射对热层大气的影响;而NRLMSISE-00在平静期间地磁活动影响大气密度的变化特征上,比JB2008更符合实测结果。实测结果显示冬季半球日峰值出现时间比夏季半球早,JB2008与实测相符,NRLMSISE-00则与实测相反。整体而言,在天宫一号轨道高度、地磁平静期,JB2008模式优于NRLMSISE-00模式。     

The variability of eta Car: A tool for the LBV phenomenon

We discuss the historical light curve of the most peculiar superluminous star Car, and the spectroscopic variations during the last 100 y. After the nova-like spectral evolution following the 1889 light maximum, the star underwent many shell episodes which were characterized by a large fading of the higher ionization emission lines. We describe the most recent 1992 event when the Hei and [Nii] emission lines nearly faded out, and a broad P Cygni absorption appeared in the Hi and Hei lines. A recurrence time of about 5 years is suggested from the times of the spectroscopic episodes and the IR light curve. The results are discussed in the light of possible models.     

基于S3C44b0X服装绘图仪液晶显示开发

服装绘图仪的控制核心采用SAMSUNG公司S3C44b0X处理器,S3C44b0X为一般应用提供了高性价比和高性能的微控制器解决方案。介绍了将S3C44b0X内置LCD控制器进行重新配置,使其能驱动YXD-12864A液晶显示模块,并给出了该控制器与LCD硬件接口方法,经实验验证此方法的正确性。     

基于CCS的DSP软件开发方法

主要介绍了利用CCS进行DSP软件开发的过程和程序调试方法,概括说明CCS集成开发环境的基本功能和使用方法,对主要的和不容易掌握的命令做了重点说明,并指出程序调试中应该注意的一些问题.熟练掌握调试开发工具对于加快DSP产品的开发速度是十分重要的.     

全相参雷达信标

为缩短雷达的研制周期、节约经费，研制了一种全相参雷达信标，用于对全相参宽频带自适应频率捷变脉冲压缩雷达进行测试。介绍了全相参雷达信标的关键技术及其实现方法。外场试验表明，该信标设备的设计原理是可行的，效果也是明显的。     

Production of high fidelity lunar agglutinate simulant

As space faring nations consider manned and unmanned missions to the Moon, there is a growing need to develop high fidelity lunar regolith simulants that can accurately reproduce the properties and behavior of lunar regolith. Such simulants will be employed to verify the performance of equipment, mechanisms, structures and processes to be used on the lunar surface. One of the significant limitations of current terrestrial-based simulants, such as the popular mare simulant, JSC-1A, is the lack of agglutinates. This paper investigates the production of a lunar mare agglutinate simulant based on JSC-1A. A modified plasma processing technique was used to expose the JSC-1A regolith simulant to high temperatures and transform it to predominantly a glassy phase. Detailed characterization results are presented to confirm that the agglutinate simulant material produced during this investigation reasonably satisfies the primary requirements of an agglutinate simulant such as amorphous/crystalline content, particle size, morphology, vesicular structure, chemistry, and presence of nanophase elemental Fe.     

Comparing ionospheric models with mid-latitude ionosonde observations

The purpose of this research work is to validate the ionospheric models (IRI and CHIU) to assess its suitability and usefulness as an operational tool. The ionospheric model is a computer model designed to predict the state of the global ionosphere for 24 h. The scope was limited to conduct comparisons between the predicted F₂ layer critical frequencies (f₀F₂) against observed ionosonde data. The ionospheric prediction model (IPM) was designed to predict by using monthly median sunspot number, while the observation data are taken from two digital ionospheric sounding stations (Okinawa, 26.28N, 127.8E and Wakkanai, 45.38N, 141.66E) which lies within the mid-latitude region of the globe. Analysis of the f₀F₂ data from stations for year (2001) with high solar activity and year (2004) with low solar activity, four months (March, June, September and December) chosen based primarily on data availability. From results it seen that the ratio between monthly median predicted and observed f₀F₂ values for each model used in this research work and for the chosen months was nonlinear with local time, so the empirical formula for applying correction factors were determined, these formula can be used to correct the error occurred in predicted f₀F₂ value.     

会议筹备优化设计

根据代表回执的住房要求数据,通过曲线拟合估计出本届与会代表人数,定义了距离数量指标和代表满意数量指标,并对指标赋予权重,再利用线性规划,建立优化模型,得到应预定的宾馆及每个宾馆应预定的房间;对会议室的租借问题,将各分组会议分为三个级别,并根据其重要性赋予相应的权重,再结合与会代表总人数,求得各级别会议的与会代表人数,选定会议室;对租车方案,以租车总费用最少为目标函数,以租借三种类型作为约束条件,建立优化模型,利用Lingo软件编程求解。     

Adaptive Square-Root Cubature–Quadrature Kalman Particle Filter for satellite attitude determination using vector observations

A novel algorithm is presented in this study for estimation of spacecraft?s attitudes and angular rates from vector observations. In this regard, a new cubature–quadrature particle filter (CQPF) is initially developed that uses the Square-Root Cubature–Quadrature Kalman Filter (SR-CQKF) to generate the importance proposal distribution. The developed CQPF scheme avoids the basic limitation of particle filter (PF) with regards to counting the new measurements. Subsequently, CQPF is enhanced to adjust the sample size at every time step utilizing the idea of confidence intervals, thus improving the efficiency and accuracy of the newly proposed adaptive CQPF (ACQPF). In addition, application of the q-method for filter initialization has intensified the computation burden as well. The current study also applies ACQPF to the problem of attitude estimation of a low Earth orbit (LEO) satellite. For this purpose, the undertaken satellite is equipped with a three-axis magnetometer (TAM) as well as a sun sensor pack that provide noisy geomagnetic field data and Sun direction measurements, respectively. The results and performance of the proposed filter are investigated and compared with those of the extended Kalman filter (EKF) and the standard particle filter (PF) utilizing a Monte Carlo simulation. The comparison demonstrates the viability and the accuracy of the proposed nonlinear estimator.     

一种用于实时轨道确定的NPF-SRCKF滤波算法

针对航天器实时轨道确定中建模复杂、计算量大、估计精度低的问题,设计了一种考虑地球J 2 摄动影响的基于NPF-SRCKF的实时轨道确定算法,该算法采用非线性预测滤波(NPF)对模型误差进行补偿修正,利用平方根容积卡尔曼滤波(SRCKF)算法对修正模型误差后的系统进行状态估计。针对单测站、双测站跟踪测量设计了不同的实时轨道确定算法。实验结果显示,将非线性预测滤波和平方根容积卡尔曼滤波结合在一起,运用于简化的实时轨道确定模型,能有效降低计算复杂度,改进数值运算的稳定性,提高状态估计的精度。