芳纶纤维增强复合材料的机械加工

介绍了加工芳纶纤维增强复合材料的工艺方法,包括钻孔、平板制件的切割及管件截断的方法.从刀具和切削参数等方面加以阐述,并辅以加工实例介绍了加工效果.这些刀具和工艺方法成功地应用于某型号卫星天线支架的研制中,攻克了芳纶纤维增强复合材料不易加工的难题.     

液氧煤油发动机地面试车故障监控系统研制

为了降低试车中发动机故障对产品和试车台造成的危害,提高安全性,设计了液氧煤油高压补燃发动机地面试车故障监控系统。主要介绍了系统总体实施方案、检测算法及验证情况。多次实际热试车考核和对大量热试车数据的验证表明,该系统未出现一次误报警,能够比指挥员提前检测到故障,系统简单可靠,易于实现,经济性好,对实现地面试车、箭载发动机故障检测和报警具有工程应用价值。     

CBERS-O2热红外波段绝对辐射定标及其不确定性分析

文章介绍了2004年CBERS-O2星热红外波段绝对定标工作，结合野外试验情况和数据处理过程深入进行了不确定性因素分析（包括误差分析），并从亮温反演的角度分析定标精度，进而针对如何提高在轨卫星热红外波段绝对辐射定标的精度，进行了探讨。     

Developing Space Manufacturing Industry To Serve National Economy And Promote Social Progress

Over the past 50 or more years, China's space industry has made brilliant achievements typically represented by the three milestones in China's space development history,i.e.launching the first man-made satellite into space in 1970,realizing the manned spaceflight for the first time in 2003 and sending the first lunar probe to the moon in 2007.At the same time, China's space industry has also mastered a great number of core technologies based upon its own intellectual property rights,accumulated rich exp...     

Plasma Flow and Related Phenomena in Planetary Aeronomy

Understanding the processes involved in the interaction of solar system bodies with plasma flows is fundamental to the entire field of space physics. The features of the interaction can be very different, depending upon the properties of the incident plasma as well as the nature of the obstacle. The properties of the atmosphere/ionosphere associated with the obstacle are of particular importance into understanding the plasma interaction process, especially for non-magnetized obstacle. This paper discusses in detail the roles of the atmosphere and ionosphere systems of plasma interaction around Venus, Mars, comets and some particular satellites. The coupling between magnetosphere and ionosphere is also discussed for Earth and Giant planets.     

Effects of Nb Content on Yield Strength of NiTiNb Alloys in Martensite State

Two near single-phase NiTiNb alloys—Ni₅₀Ti₄₈Nb₂ and Ni_49.5Ti_46.5Nb₄—are prepared and studied by means of scanning electron microscopy (SEM), energy dispersive spectroscopy (EDS), differential scanning calorimetry (DSC) and tensile tests in order to unearth the effects of Nb-atom solid solution in NiTi phase on the yield strength induced by self-accommodation of martensite variants. The results show that the yield strength of near single-phase NiTiNb alloys varies inversely with the amount of Nb-atoms solid-dissolved in NiTi phase. From the results out of the prior and current studies, it can be surmised that the effects of Nb content on the yield strength of NiTiNb alloys in martensite state depend on the coaction. Nb solid solution weakening mechanism and β-Nb phase composite strengthening mechanism. This inference might be a satisfactory explanation to the fact that the yield strength of (NiTi)_50–0.5xNb_x alloys in martensite state begins with decline and then rises when the Nb content increases.     

Design and implementation of a sensorless switched reluctance drivesystem

This paper presents a new sensorless switched reluctance drive system. The drive system can perform well when the system is operated in the pulse-width modulated (PWM) region. By suitably shaping an induced voltage in an inactive phase which is adjacent to an energized phase of a switched reluctance motor (SRM), the shaft position of the rotor can be easily obtained. As a result, the position sensor can be eliminated. First, the theoretical analysis of the proposed method is presented. By systematic theoretical analysis, a voltage signal which can easily estimate the shaft position of the motor is derived. This signal is only related to the input dc voltage of the converter, and the self and mutual inductances of the motor. Then, a new method to measure the self and mutual inductances of the SRM is proposed. After that, the design for a simple circuit which can synthesize the required voltage signal for rotor position estimation is presented. Next, how a 32-bit microprocessor system is used to execute the position and speed estimation, speed-loop control, and current-commands generation is shown. A closed-loop drive system is thus achieved. Several simulated and experimental results validate the theoretical analysis. A new direction in the design and implementation of a sensorless switched reluctance drive system is presented     

Nonlinear dynamics and station-keeping control of a rotating tethered satellite system in halo orbits

The dynamics of a rotating tethered satellite system （TSS） in the vicinity of libration points are highly nonlinear and inherently unstable. In order to fulfill the station-keep control of the rotating TSS along halo orbits, a nonlinear output tracking control scheme based on the θ- D technique is proposed. Compared with the popular time-variant linear quadratic regulator （LQR） controller, this approach overcomes some limitations such as on-line computations of the algebraic Riccati equation. Besides, the obtained nonlinear suboptimal controller is in a closed form and easy to implement. Numerical simulations show that the TTS trajectories track the periodic reference orbit with low energy consumption in the presence of both tether and initial injection errors. The axis of rotation can keep pointing to an inertial specific object to fulfill an observation mission. In addition, the thrusts required by the controller are in an acceptable range and can be implemented through some low-thrust propulsion devices.     

卫星光学遥感系统优化设计与像质评价探讨

介绍了卫星光学遥图像获取与图像处理一体化优化设计的思路；运用通用像质方程（GIQE）对于利用小相对孔径光学系统和调制传递函数补偿（MTFC）方法得到的图像的品质与利用相对较大相对孔径光学系统得到的图像的品质进行了对比分析。     

Virtual flight test techniques to predict a blended-wing-body aircraft in-flight departure characteristics

As one of the promising configurations of the next generation of commercial aircraft,research on departure characteristics of the Blended-Wing-Body(BWB) is of great signification to safe flight limits. A three-degree-of-freedom(3-DOF) virtual flight test in a wind tunnel has been implemented for a candidate configuration to predict the departure characteristics. The support mechanism, the test model and the control law of the virtual flight test are introduced. In order to show the relationship ...