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1.
近期我们对我校560名学生进行了问卷抽样调查,调查共发出问卷560份,回收560份,回收率为 100%,全部为有效问卷。为确保调查的客观性、科学性,在抽样过程中,我们充分考虑了专业特色、学制特色,其中中专生175人,占31.3%,高大专178人,占31.8%,五年制大专207人,占37%;电气系207人,占36.96%,机械系178人,占31.78%,计算机系84人,占15%,动力系50人,占8.9%;从家庭来源看,大中城市61人,占10.8%,城镇130人,占23.21%,农村368人,占65…  相似文献   

2.
姜长英,年龄与世纪同步,经历与世纪同行,一身坎坷,半世奋斗,为航空教育事业和航空史研究,呕心沥血,鞠躬尽瘁,硕果显赫,德高望重。  相似文献   

3.
胡朝德 《飞行力学》1994,12(3):59-66
主要介绍K-8飞机在鉴定试飞中的操纵性,稳定性试飞方法和结果,其中包括起飞,着陆,速度稳定性,过载稳定性,机动点,中性点的确定,同时还对纵向模态特性,横侧静稳定性,操纵性,滚转效率,横侧动态特性进行了测定,并在各特性的测定中谈了飞行体会。  相似文献   

4.
人发样品是生物类有机样品,用火焰原子吸收光谱法测定人发中Ca,Mg,Cu,Pb,Fe,Zn元素时,采用硝酸:高氯酸=4:1消解体系,电热板加热常压消解大约2小时,样品呈湿盐态,以去离子水稀释定容,测定溶液为无色,透明,分别上机测定以上各元素,本测定方法技术关键在于消解温度不得超过250℃消解完全后要赶尽高氯酸,测定Ca,Mg时,用0.1%SrCl2水溶液定容,以消除共存物的干扰,对各元素的仪器测定  相似文献   

5.
测量船是海上活动观测站,船上配有精密跟踪测量雷达和光学经纬仪等测控设备,要精确观测空间飞行器的运动轨迹或弹道,就必须精确测定船体的位置,速度,姿态和航向,我国早期测量船上的导航系统使用避限性很大,而且相当落后,已经不能满足当代海上作业的精度要求,急需更新。目前,我国GPS已全面投入运行,利用该系统测定测量船的位置和姿态,不仅精度高,实时性强,而且操作简便,设备成本低,借助差分导航,组合导航等技术还可以进一步提高其定位测姿精度,不久的将来,俄罗斯的Glonass也将投入运行,且工作性能与GPS基本一样,可作GPS的补充导航能力。  相似文献   

6.
基于神经网络的稳M数非线性控制   总被引:2,自引:1,他引:1  
介绍风洞稳M数神经网络的非线性控制,包括预测模型,动态优化和反馈校正原理,以实现速度快,精度高,低耗油的优化控制目标,试验表明,该系统不仅稳M数控制精度高,响应速度快,而且鲁棒性好,节省燃油。  相似文献   

7.
中航第二集团公司成立一周年以来,针对“三少一多”的困难,顽强拼搏,开拓进取,抓发展,抓机遇,抓改革,抓创新……,抓出了一片新局面  相似文献   

8.
微传感器最新发展   总被引:9,自引:1,他引:9  
近年来,微传感器受到国际传感技术界的广泛关注,本文介绍十多个微传感器,包括三轴加速度计,单,双轴加速度计片,表面微机械陀螺(角速度传感器),微惯性导航系统,微磁通门传感器,磁阻传感器,纳米皮拉尼压力传感器,微科氏质量流量计,毫米波图像传感器,GPS手表(1cm^3),二氧化碳传感器和微/超微角位移传感器,文事简要介绍它们的基本结构。敏感机理,特点等,从中可以看出微传感器已成为传感技术中有重要应用前景的组成部分。  相似文献   

9.
一、“九五”回顾 “九五”期间,我国民航业经历了市场经济的严峻考验。面对前所未有的困难局面,行业上下齐心协力,团结一致,通过深化管理体制改革,加强宏观调控,规范航空运输市场,强化运价管理,调整航空运输结构,加强规章制度建设等一系列强有力的措施,冲破了由卖方市场变买方市场,由高增长变低增长,由高效益变低效益的重重困境,运输生产取得了可喜的成绩。 伴随民航业的发展,“九五”期间,民航飞行学院抓住历史机遇,不断深化以教学训练为中心的各项改革,通过更新训练机型,加大基础建设投入,完善训练设施,合理调整训练…  相似文献   

10.
DSP具有速度快,精度高,价格低等特点,而惯性技术要求信号处理具有响应时间快,运算精度高,可靠性好,DSP非常适合于在惯性技术中应用,作者介绍了DSP的特点,设计方法,DSP在捷联系统中的应用,以及世界DSP厂商和产品等内容。  相似文献   

11.
This paper discusses experimental results from two different build configurations of a heated multiple rotating cavity test rig.Measurements of heat transfer from the discs and tangential velocities are presented.The test rig is a 70% full scale version of a high pressure compressor stack of an axial gas turbine engine.Of particular interest are the internal cylindrical cavities formed by adjacent discs and the interaction of these with a central axial throughflow of cooling air.Tests were carried out for a range of non-dimensional parameters representative of high pressure compressor internal air system flows(Re up to 5×106 and Rez up to 2×105).Two different builds have been tested.The most significant difference between these two build configurations is the size of the annular gap between the(non-rotating) drive shaft and the bores of the discs.The heat transfer data were obtained from thermocouple measurements of surface temperature and a conduction solution method.The velocity measurements were made using a two component,LDA system.The heat transfer results from the discs show differences between the two builds.This is attributed to the wider annular gap allowing more of the throughflow to penetrate into the cavity.There are also significant differences between the radial distributions of tangential velocity in the two builds of the test rig.For the narrow annular gap,there is an increase of non-dimensional tangential velocity V/Ωr with radial location to solid body rotation V/Ωr=1.For the wider annular gap,the non-dimensional velocities show a decrease with radial location to solid body rotation.   相似文献   

12.
The effects of Mo on the microstructure evolution, porosity and hydrogen sorption properties of Ti-Mo getters are investigated in this work. The results show that the addition of Mo prolongs the densification process of Ti-Mo getters and results in a significant amount of sintered pores. With the Mo content increasing, the porosity of getters firstly increases reaching the maximum value as it at- tains about 7.5wt.%, and then drops. At the room temperature, the hydrogen sorption property of getters increases progressively with the Mo content increasing, but the tendency is not very clear before its content lies below 2.5wt.%. When the Mo content achieves about 7.5wt.%, the hydrogen sorption property proves to be the best. The discussion is made about the above mentioned phenomena inclusive of hydrogen sorption properties of getters under different activation conditions (from 500-750 ℃).  相似文献   

13.
A new time-accurate marching scheme for unsteady flow calculations is proposed in the present work. This method is the combination of classical Successive Over-Relaxation (SOR) iteration method and Jacobian matrix diagonally dominant splitting method of LUSGS. One advantage of this algorithm is the second-order accuracy because of no factorization error. Another advantage is the low computational cost because the Jacobian matrices and fluxes are only calculated once in each physical time step. And, the SOR algorithm has better convergence property than Gauss-Seidel. To investigate its accuracy and convergency, several unsteady flow computa- tional tests are carried out by using the proposed SOR algorithm. Roe’s FDS scheme is used to discritize the inviscid flux terms. Un- steady computational results of SOR are compared with the experiment results and those of Gauss-Seidel. Results reveal that the numerical results agree well with the experimental data and the second-order accuracy can be obtained as the Gauss-Seidel for unsteady flow computations. The impact of SOR factor is investigated for unsteady computations by using different SOR factors in this algorithm to simulate each computational test. Different numbers of inner iterations are needed to converge to the same criterion for different SOR factors and optimal choice of SOR factor can improve the computational efficiency greatly.  相似文献   

14.
The slewing motion control of a truss arm driven by a V-gimbaled control-moment-gyro (CMG) is a nonlinear control problem. The V-gimbaled CMG consists of a pair of gyros that must precess synchronously. The moment of inertia of the system, the angular momentum of the gyros and the external disturbances are not exactly known. With the help of feedback linearization and recursive Lyapunov design method, an adaptive nonlinear controller is designed to deal with the unknown items. Performance of the proposed controller is verified by simulation.  相似文献   

15.
适于低轨卫星IP网络的单核共享树组播算法(英文)   总被引:1,自引:0,他引:1  
为了解决低轨卫星IP网络中现有典型源组播算法的信道资源浪费问题,本文提出了一套单核共享树组播算法,即核心群合并共享树(CCST)和加权核心群合并共享树(w-CCST)算法。CCST 算法包括动态近似中心(DAC)选核方法和核心群合并组播路径构建方法。DAC方法专为周期、规律运动的低轨卫星网络提出,不需要复杂的星上计算。在核心群合并方法中,以核节点作为初始核心群,通过核心群和剩余组成员的最短路径方法逐步扩展直至整棵组播树构建完成,从而使得组播树的树代价最小,大大提高了网络的带宽利用率和组播传输效率。w-CCST 算法中所提出的加权因子可以调整树代价和端到端传播时延之间的折衷程度,因此,可以通过调整加权因子来适度增大树代价、降低端到端传播时延以支持某些端到端时延要求苛刻的实时组播业务。最后,与低轨卫星 IP 网络中典型算法进行了性能比较,仿真结果说明,CCST 算法的平均树代价比其它算法显著降低,w-CCST 算法的平均端到端传播时延小于 CCST 算法。  相似文献   

16.
GA-Based Model Predictive Control of Semi-Active Landing Gear   总被引:1,自引:1,他引:0  
Semi-active landing gear can provide good performance of both landing impact and taxi situation, and has the ability for adapting to various ground conditions and operational conditions. A kind of Nonlinear Model Predictive Control algorithm (NMPC) for semi-active landing gears is developed in this paper. The NMPC algorithm uses Genetic Algorithm (GA) as the optimization technique and chooses damping performance of landing gear at touch down to be the optimization object. The valve's rate and magnitude limitations are also considered in the controller's design. A simulation model is built for the semi-active landing gear's damping process at touchdown. Drop tests are carried out on an experimental passive landing gear systerm to validate the parameters of the simulation model. The result of numerical simulation shows that the isolation of impact load at touchdown can be significantly improved compared to other control algorithms. The strongly nonlinear dynamics of semi-active landing gear coupled with control valve's rate and magnitude limitations are handled well with the proposed controller.  相似文献   

17.
Simulation and Analysis of Crashworthiness of Fuel Tank for Helicopters   总被引:1,自引:0,他引:1  
Crashworthiness requirement of fuel tanks is one of the important requirements in helicopter designs. The relations among the protection frame, textile layer and rubber layer of the fuel tank are introduced. Two appropriate FE models are established, one is for an uncovered helicopter fuel tank without protection frame, and the other is for fuel tank with protection frame. The dynamic responses of the two types of fuel tanks impinging on the ground with velocities of 17.3 m/s are numerically simulated for the purpose of analyzing energy-absorbing capabilities of the textile layer and protection frame. The feasibility of the current crashworthiness design of the fuel tank is examined though comparing the dynamic response behaviors of the two fuel tanks.  相似文献   

18.
Aerospace relay is one kind of electronic components which is used widely in national defense system and aerospace system. The existence of remainder particles induces the reliability declining, which has become a severe problem in the development of aerospace relay. Traditional particle impact noise detection (PIND) method for remainder detection is ineffective for small particles, due to its low precision and involvement of subjective factors. An auto-detection method for PIND output signals is proposed in this paper, which is based on direct wavelet de-noising (DWD), cross-correlation analysis (CCA) and homo-filtering (HF), the method enhances the affectiv-ity of PIND test about the small particles. In the end, some practical PIND output signals are analysed, and the validity of this new method is proved.  相似文献   

19.
20.
(高)超声速流动试验技术及研究进展   总被引:1,自引:1,他引:1  
易仕和  陈植  朱杨柱  何霖  武宇 《航空学报》2015,36(1):98-119
近年来,与高速飞行器相关的(高)超声速流动受到了极大的关注。这类流动所具有的非定常性、强梯度和可压缩性对试验方法和风洞设计技术提出了挑战。超声速纳米示踪平面激光散射(NPLS)技术是由作者所在团队研发的非接触光学测试技术。它能够以较高的空间分辨率来揭示超声速三维流场的一个瞬态剖面的时间解析的流动结构。介绍了NPLS技术以及基于NPLS开发的密度场测量、雷诺应力测量和气动光学波前测量等方法,并回顾了这些技术在超声速边界层、超声速混合层、超声速压缩拐角、激波/边界层相互作用和光学头罩绕流等流动中的应用,清晰地再现了边界层、混合层、激波等典型流场结构及其时空演化特性。另外,为了模拟和研究高空大气条件下边界层自然转捩和超声速混合层的转捩特性,介绍了高超声速静风洞、超-超混合层风洞的设计技术以及层流化喷管的设计方法。  相似文献   

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