可调进口导叶和叶片角向缝处理机匣相互作用的

可调进口导叶和叶片角向缝处理机匣都能扩大压气机的稳定工作范围,为了分析同时采用这两种措施对压气机稳定性的影响及二者之间相互作用的机理,在单转子轴流压气机实验台上对不同导叶弯角下实壁机匣和叶片角向缝机匣进行了详细的实验测试。同时,对导叶弯角为+10°的每一种机匣结构和导叶0°的实壁机匣结构进行了数值模拟,数值模拟结果与实验结果符合良好,相对于导叶0°的实壁机匣,实验及数值模拟结果均表明,导叶正弯角结合叶片角向缝机匣处理结构能更好地扩大压气机的稳定工作裕度。对转子流场进行对比分析可得,导叶正预旋能抑制叶背气流的分离,提高压气机的稳定工作范围,但仍然没有改变转子叶尖部诱发失速的流动现象,而叶片角向缝主要是通过对叶顶气流的抽吸作用抑制了间隙泄漏流达到扩稳效果,因此耦合时能独立发挥各自的扩稳作用,从而能获得比单独使用任何一种方法都要更大的稳定工作范围的提升。     

Effects of adiabaticity and non-adiabaticity of dust charge fluctuation on the propagation of the dust ion acoustic waves in inhomogeneous dusty plasma

A theoretical investigation has been made for adiabatic positive and negative dust charge fluctuations on the propagation of dust-ion acoustic waves (DIAWs) in a weakly inhomogeneous, collisionless, unmagnetized dusty plasmas consisting of cold positive ions, stationary positively and negatively charged dust particles and isothermal electrons. The reductive perturbation method is employed to reduce the basic set of fluid equations to the variable coefficients Korteweg–de Vries (KdV) equation. Either compressive or rarefactive solitons are shown to exist depending on the critical value of the ion density, which in turn, depends on the inhomogeneous distribution of the ion. The dissipative effects of non-adiabatic dust charge variation has been studied which cause generation of dust ion acoustic shock waves governed by KdV-Burger (KdVB) equation. The results of the present investigation may be applicable to some dusty plasma environments, such as dusty plasma existing in polar mesosphere region.     

火星卫星的冻结轨道研究

冻结轨道是一种稳定的轨道,地球、火星、月球的卫星因引力场的南北不对称,都存在冻结轨道.由于主星体引力场的不同,它们卫星的冻结轨道也有不同的特性.地球卫星的冻结执道的偏心率非常小,对卫星遥感非常有利,国内外已有相当多的近地遥感卫星采用这种轨道.月球卫星的冻结轨道偏心率随轨道倾角的不同有很大的变化,对月球卫星冻结轨道的研究...     

Needs and Tools for Future Gravity Measuring Missions

This paper compares the requirements that can be expected of gravity measuring missions with respect to the status of the instrumentation and satellite technologies. The error sources of gravity gradiometry and satellite-to-satellite tracking are analysed and the elements limiting the accuracy are identified. Proposed and approved future missions that will fly technologies of interest for gravity sensing are recalled. Areas of technical development of interest are reviewed. The article finishes with two possible conceptual missions presented as examples and with a chapter of conclusions. This revised version was published online in August 2006 with corrections to the Cover Date.     

Ocean Tides in GRACE Monthly Averaged Gravity Fields

The GRACE mission will map the Earth's gravity fields and its variations with unprecedented accuracy during its 5-year lifetime. Unless ocean tide signals and their load upon the solid earth are removed from the GRACE data, their long period aliases obscure more subtle climate signals which GRACE aims at. In this analysis the results of Knudsen and Andersen (2002) have been verified using actual post-launch orbit parameter of the GRACE mission. The current ocean tide models are not accurate enough to correct GRACE data at harmonic degrees lower than 47. The accumulated tidal errors may affect the GRACE data up to harmonic degree 60. A study of the revised alias frequencies confirm that the ocean tide errors will not cancel in the GRACE monthly averaged temporal gravity fields. The S₂ and the K₂ terms have alias frequencies much longer than 30 days, so they remain almost unreduced in the monthly averages. Those results have been verified using a simulated 30 days GRACE orbit. The results show that the magnitudes of the monthly averaged values are slightly higher than the previous values. This may be caused by insufficient sampling to fully resolve and reduce the tidal signals at short wavelengths and close to the poles. This revised version was published online in August 2006 with corrections to the Cover Date.     

变拓扑多臂航天器高效统一动力学建模

针对多臂航天器在轨操控过程中可能存在的多链、闭环、环链混合等多种拓扑构型及相应的动力学模型变化,提出基于空间算子代数理论(SOA)的高效统一动力学建模方法。首先,提出了描述多臂航天器部件连接关系的构型参数,并基于构型参数提出了多臂航天器拓扑构型描述矩阵的自主生成方法。其次,基于空间算子代数理论,将通路矩阵与空间转移算子相结合,提出了变拓扑多臂航天器统一动力学建模方法。最后,将数值仿真结果与多体动力学仿真软件的仿真结果进行比对,验证所提方法的有效性。仿真结果表明,对于不同的拓扑结构,所提出的O(n)阶统一动力学建模方法能准确描述变拓扑情况下的多臂航天器动力学响应。     

深空探测重力模拟飞行器方案设想

为解决失重环境对航天员生理健康的影响,在调研国内外重力飞行器研究现状的基础上,结合重力模拟飞行器的原理及人造重力舒适度影响因素,提出了一种通过自旋产生人造重力的深空探测飞行器方案设想。最后给出了重力模拟飞行器建设的实施规划、总体方案、在轨组装流程及技术难点。深空探测重力模拟飞行器稳定运转可为空间工作生活的航天员提供与地面无异的重力环境,将为执行深空探测任务提供必要的环境保障。     

Independent modal variable structure fuzzy active vibration control of thin plates laminated with photostrictive actuators

Photostrictive actuators can produce photodeformation strains under illumination of ultraviolet lights. They can realize non-contact micro-actuation and vibration control for elastic plate structures. Considering the switching actuation and nonlinear dynamic characteristics of photostrictive actuators, a variable structure fuzzy active control scheme is presented to control the light intensity applied to the actuators. Firstly, independent modal vibration control equations of photoelectric laminated plates are established based on modal analysis techniques. Then, the optimal light switching function is derived to increase the range of sliding modal area, and the light intensity self-adjusting fuzzy active controller is designed. Meanwhile, a continuous function is applied to replace a sign function to reduce the variable structure control (VSC) chattering. Finally, numerical simulation is carried out, and simulation results indicate that the proposed control strategy provides better performance and control effect to plate actuation and control than velocity feedback control, and suppresses vibration effectively.     

脉冲噪声下基于梯度加权平均的变步长NLMP算法

针对非高斯 α 稳定分布噪声环境下的自适应滤波问题,提出一种新的基于梯度加权平均的变步长归一化最小平均p范数(VSS-NLMP)算法。该算法基于梯度矢量能够跟踪自适应过程的均方权值偏差(MSD)这一特点,通过对梯度矢量的平滑减小梯度噪声的影响,然后利用平滑梯度矢量的欧氏范数和系统误差的分数低阶矩控制步长的变化。文中给出了新算法的迭代过程,然后对其收敛性进行简要分析,仿真结果表明,本文新算法较现有变步长NLMP算法具有更快的收敛速度和更高的稳态精度。     

一种单室双推力发动机装药Ⅱ界面粘接性能研究

根据单室双推力发动机装药的特点,对厚度绝热层、衬层的预反应及预固化衬层在真空状态下垂直存放等绝热衬层加工工艺条件对装药Ⅱ界面粘接性能的影响进行了研究,并提出了改善界面性能的技术途径。