Very low thrust station-keeping for low Earth orbiting satellites

Traditional station-keeping for Earth observation satellites with chemical thrusters generally involves maneuvers every couple months that are able to change significantly the semi-major axis and the inclination. These strategies do not scale down to very low thrust level (a few hundreds of μN) electrical thrusters. This paper presents both in-plane and out-of-plane strategies that spread corrections over very long arcs and discretize them to tiny maneuvers every couple orbits, taking into account mission-constraints on maneuvers locations. These strategies scale up to medium thrust strategies, filling the gap between propulsion technologies. The out-of-plane strategy although features a new no-deadband property and controls the full orbital momentum. All strategies allow control very close to the reference (a few hundreds meters in osculating parameters) and very low cost.     

Improving the low orbit satellite tracking ability using nonlinear model predictive controller and Genetic Algorithm

The satellite motion on the reference orbit (RO) with less energy consumption has always persuaded researchers to design optimal control systems. The nonlinear nature and time-varying equations of motion make this quest more challenging. The present study proposes a novel control system for satellite motion on the RO by considering a comprehensive model of its dynamics in orbit and a Nonlinear Model Predictive Controller (NMPC). The NMPC calculates the sub-optimal control inputs of satellite motion reference on the elliptic orbit by minimizing a convex cost function at each stage. Moreover, all weighting parameters of the cost function are optimized by the Genetic Algorithm (GA) to produce less perturbation and guarantee the best NMPC performance. Finally, the implemented NMPC has been compared to a Linear MPC (LMPC). The results show that not only can the NMPC resist against larger errors and perturbations, but it can also compensate for those errors by returning the satellite to its main orbit and maintaining it.     

一种测量航空发动机T_4温度的新方法

采用热电偶信号放大集成电路AD595结合镍铬─镍铝热电偶温度传感器 ,设计了航空发动机T 4 温度热电偶测温电路 ,实现了冷端自动补偿、热电偶断线报警信号输出功能。实测数据分析表明 :输出幅值大 ,误差小 ,重复性好。测量电路简单 ,具有较强的实用性。     

基于功率取样的光纤光源平均波长控制技术

为提高宽谱光纤光源温度稳定性,对平均波长温度稳定性进行了分析;对不同泵浦功率下输出光的平均波长与输出功率的变化进行了仿真和实验研究,揭示了宽谱光纤光源平均波长与输出功率的相关性;提出并实现了一种基于数学模型的平均波长控制技术.从光源输出取出小部分功率作为反馈信号,通过调整泵浦激光器电流实现了中心波长的精确控制.对研制的样机进行了实际测试,结果表明控制方案是可行的,在－45~70℃的温度范围内,宽谱光纤光源的平均波长稳定性达到0.3×10^-6℃^-1.     

Improved interpretation of solar wind ion measurements via high-resolution magnetic field data

The Wind   spacecraft’s Faraday cups (FC) continue to produce high-quality, in situ observations of thermal protons (i.e., ionized hydrogen) and α$\alpha$-particles (i.e., fully ionized helium) in the solar wind. By fitting a Wind/FC ion spectrum with a model velocity distribution function (VDF) for each particle species, values for density, bulk velocity, and temperature can be inferred. Incorporating measurements of the background magnetic field from the Wind Magnetic Field Investigation (MFI) allows perpendicular and parallel temperature components to be separated. Prior implementations of this analysis averaged the higher-cadence Wind/MFI measurements to match that of the Wind/FC ion spectra. However, this article summarizes recent and extensive revisions to the analysis software that, among other things, eliminate such averaging and thereby account for variations in the direction of the magnetic field over the time taken to measure the ions. A statistical comparison reveals that the old version consistently underestimates the temperature anisotropy of ion VDF’s: averaging over fluctuations in the magnetic field essentially blurs the perpendicular and parallel temperature components, which makes the plasma seem artificially more isotropic. The new version not only provides a more accurate dataset of ion parameters (which is well suited to the study of microkinetic phenomena), it also demonstrates a novel technique for jointly processing particle and field data. Such methods are crucial to heliophysics as wave-particle interactions are increasingly seen as playing an important role in the dynamics of the solar wind and similar space plasmas.     

工质温度对二次喷射推力矢量性能的影响

为了研究二次流温度对推力矢量的影响规律,本文基于二次喷射的基本原理,利用计算流体力学(CFD)软件,对不同温度的二次流进行了模拟仿真分析。结果表明,在相同喷射压强和喷射流量下,二次流温度越高,在扩张段影响的范围就越大,但产生的侧向力和温度并不是简单的正变关系。在此分析的基础上,提出了一种合理利用二次流温度的工程方案。
     

基于DS18B20的数字温度测量仪

介绍了DS18B20-线式数字温度传感器的功能特性和结构特点,分析了其工作时序,结合AT89S51给出了数字式温度测量装置的系统结构、硬件接口电路和软件设计方法。     

模糊温度控制系统在橡塑制品硫化工艺中的应用

根据橡塑制品的特点,以PLC为中心,在温度控制系统中应用PID 模糊抑制超调技术,研制一套平板硫化机模糊温度控制系统,提高硫化温度的精度,试验结果表明,所研制的系统能够全自动进行橡塑产品的硫化,操作方便,控制简单。     

双层钙钛矿(Sr2-xBax)FeMoO6的结构和电磁性能研究

利用X射线粉末衍射、Rietveld结构精修技术及电、磁测试等手段分别对（Sr2-xBax）FeMoO6（0≤x≤2）的晶体结构及电磁性质进行了研究。研究结果表明：对于掺杂含量x≤1．6的（Sr2-xBax）FeMoO6样品,其电阻率温度关系呈金属性,而对于掺杂含量x≥1．7的样品,其电阻率温度关系呈半导体性。居里温度Tc在x=0．4处出现极大值。     

硅溶胶对钙基膨润土性能影响

对硅溶胶改性钙基膨润土的研究结果表明:硅溶胶/膨润土(质量比)小于1/8时,膨润土的吸附性和悬浮性随着硅溶胶加入量的增加而提高,进一步增加硅溶胶的加入量反而下降,膨胀性持续降低;pH值对硅溶胶改性效果影响不大;随焙烧温度的升高,膨润土的吸附性和膨胀性呈先上升后下降的趋势,悬浮性提高,500℃焙烧土综合性能最佳;硅溶胶改性500℃焙烧后膨润土的性能更好。差热分析表明,600~700℃焙烧膨润土失去晶格羟基,综合性能降低;扫描电镜观察说明,硅溶胶改性后膨润土颗粒分散性较好;X-射线衍射和透射电镜分析证实了带负电的硅溶胶主要结合在蒙脱石端面上。