轨道维持与调相的综合优化策略研究

在交会对接飞行任务设计研究中必须首先确定目标航天器的轨道设计策略,研究了一种将目标航天器轨道维持和调相两种任务进行综合优化的策略.轨道维持的任务是使得目标航天器轨道的形状和位置符合交会要求,调相的任务是使目标航天器在轨道中的初始相位角符合交会要求.在考虑了交会对接发射窗口、交会终端约束条件下,将目标航天器轨道设计问题转化为一个非线性规划问题,应用序列二次规划方法对其进行了求解.仿真计算表明,这种方法既能以较少变轨次数满足交会对接任务要求,又能节省燃料,为空间交会对接任务规划提供了重要参考.     

极高真空技术的发展

总结了极高真空(XHV低于10-9Pa的压力范围)获得和测量方法以及获得和测量极高真空的限制因素,描述了降低XHV系统器壁和元件(包括真空规或残余气体分析器)出气率采用的技术。     

飞机设计中的新指标—战斗恢复力

本文介绍了飞机战斗恢复力的主要特征,着重探讨了设计中提高飞机战斗恢复力的措施,旨在为以后飞机设计方案论证提供一个参考依据。     

基于超精密应用的高刚度高阻尼空气静压导轨研究

介绍了一种采用多孔质节流的新型空气静压导轨,其刚度可以达到400N/μm或者更高,具有这种刚度的空气静压导轨可以取代液体静压导轨,广泛应用于超精密机床中.     

飞机噪声预测和分析

根据中国民航规章中有关飞机适航噪声审定的要求和噪声预测原理建立了飞机噪声预测系统软件。该软件除可预测飞机适航噪声审定的起飞、进场和边线有效感觉噪声级外,还可计算巡航过程机体表面声压分布。各种噪声源的声功率在软件中均可单独计算,因此改变发动机和飞机参数可以考查这些参数对声功率的影响;对发动机和飞机设计有参考价值。通过算例计算出的起飞、进场和边线有效感觉噪声级与实测结果符合较好,能很好地满足工程应用需要。     

CBERS-02B卫星HR相机遥感影像区域网平差技术

针对CBERS-02B卫星HR相机遥感影像的几何定位精度不高,不能满足有些用户的要求,提出了基于有理多项式（Rational Polynomial Coefficient,RPC）模型的区域网平差技术,并利用多幅CBERS-02B卫星HR相机遥感影像进行了区域网平差试验,结果表明该方法能有效地提高遥感影像的几何定位精度...     

企业标准化工作与经济效益

介绍了企业从产品开发生产的相关环节入手,开展企业标准化工作与企业经济效益之间的关系,说明了企业运用标准化这一有力工具,在产品设计、制造、质量控制和企业管理等方面创造经济效益的重要作用。     

GNSS-R延迟映射接收机相关器设计

介绍基于Altera公司EP2S60 FPGA芯片的GNSS-R接收机相关器的设计与实现。根据反射信号的接收处理特点,相关器中反射通道在镜面反射点配置信息基础上滑动一定范围的码片数以及多普勒频移,以得到反射信号时延/多普勒二维相关功率。此外还重点介绍NCO模块、EMIF接口模块。试验结果表明本地码、载波生成准确,在DSP配置下相关器可正确得到反射信号相关功率。     

Sound insulation performance of plates with interconnected distributed piezoelectric patches

This paper deals with the sound insulation performance of a thin plate with intercon-nected distributed piezoelectric patches. Piezoelectric patches are periodically bonded on the sur-faces of the plate in a collocated fashion, and are interconnected via an inductive circuit network. This piezoelectric system is termed as piezo-electromechanical (PEM) plate in the paper. Homogenization methods are involved under a sub-wavelength assumption to analytically develop the dynamical equations for the PEM plate. The dispersion relationships and energy densities of the wave modes propagating in the PEM plate are studied;the sub-wavelength assumption is verified for the simulations in this paper. The coincidence frequency of the PEM plate is researched, and results show that the coincidence frequency of the PEM plate will disappear at certain circum-stances;mathematical and physical explanations are made for this phenomenon. The disappearance of the coincidence frequency is used to optimize the value of inductance, for the purpose of improv-ing the sound transmission loss of the PEM plate.     

Disturbance observer based model predictive control for accurate atmospheric entry of spacecraft

Facing the complex aerodynamic environment of Mars atmosphere, a composite atmospheric entry trajectory tracking strategy is investigated in this paper. External disturbances, initial states uncertainties and aerodynamic parameters uncertainties are the main problems. The composite strategy is designed to solve these problems and improve the accuracy of Mars atmospheric entry. This strategy includes a model predictive control for optimized trajectory tracking performance, as well as a disturbance observer based feedforward compensation for external disturbances and uncertainties attenuation. 500-run Monte Carlo simulations show that the proposed composite control scheme achieves more precise Mars atmospheric entry (3.8?km parachute deployment point distribution error) than the baseline control scheme (8.4?km) and integral control scheme (5.8?km).