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121.
航天着陆试验场指挥控制系统设计与实现 总被引:1,自引:0,他引:1
指挥控制系统是航天着陆试验场不可或缺的一部分,完成试验指挥、控制、管理、视频监控、数据分析与处理、故障判别、仿真、授时、通信等功能。文章所介绍的某航天着陆试验场指挥控制系统,由时统子系统、通信子系统、语音调度子系统、视频监控子系统、大屏幕投影显示子系统、数据处理与存储子系统、指令发控台、指显工作站、软件等组成。系统结构采用双机双网并行工作模式设计。作为数据传输核心的通信子系统,采用双网热备路径冗余设计;作为数据处理与指令发布核心的处理服务器、数据库服务器和控制计算机,设计上都采用了双机并行技术。实践证明,上述技术的运用从系统结构上避免了由于单点故障而引起的系统宕机,提高了系统的可靠性和安全性。 相似文献
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Multi-sensor image matching based on salient edges has broad prospect in applications, but it is difficult to extract salient edges of real multi-sensor images with noises fast and accurately by using common algorithms. According to the analysis of the features of salient edges, a novel salient edges detection algorithm and its rapid calculation are proposed based on possibility fuzzy C-means (PFCM) kernel clustering using two-dimensional vectors composed of the values of gray and texture. PFCM clustering can overcome the shortcomings that fuzzy C-means (FCM) cluster- ing is sensitive to noises and possibility C-means (PCM) clustering tends to find identical clusters. On this basis, a method is proposed to improve real-time performance by compressing data sets based on the idea of data reduction in the field of mathematical analysis. In addition, the idea that kernel-space is linearly separable is used to enhance robustness further. Experimental results show that this method extracts salient edges for real multi-sensor images with noises more accurately than the algorithm based on force fields and the FCM algorithm; and the proposed method is on average about 56 times faster than the PFCM algorithm in real time and has better robustness. 相似文献
124.
Due to the deficiencies in the conventional multiple-receiver localization systems based on direction of arrival(DOA) such as system complexity of interferometer or array and amplitude/phase unbalance between multiple receiving channels and constraint on antenna configuration,a new radiated source localization method using the changing rate of phase difference(CRPD)measured by a long baseline interferometer(LBI) only is studied. To solve the strictly nonlinear problem, a two-stage closed-form solution is proposed. In the first stage, the DOA and its changing rate are estimated from the CRPD of each observer by the pseudolinear least square(PLS) method,and then in the second stage, the source position and velocity are found by another PLS minimization. The bias of the algorithm caused by the correlation between the measurement matrix and the noise in the second stage is analyzed. To reduce this bias, an instrumental variable(IV) method is derived. A weighted IV estimator is given in order to reduce the estimation variance. The proposed method does not need any initial guess and the computation is small. The Cramer–Rao lower bound(CRLB) and mean square error(MSE) are also analyzed. Simulation results show that the proposed method can be close to the CRLB with moderate Gaussian measurement noise. 相似文献
125.
A system impulse response with low sidelobes is critical in synthetic aperture radar(SAR) images because sidelobes contribute to noise and interfere with nearby scatterers. However,the conventional tricks of sidelobe suppression are unable to be exactly applied to the case of spaceborne sliding spotlight SAR due to great azimuth shifts in both time and frequency domains. In this paper, an extended chirp scaling algorithm is presented for spaceborne sliding spotlight SAR data imaging. The proposed algorithm firstly uses the spectral analysis(SPECAN) technique to avoid the azimuth spectrum folding effect and then employs the chirp scaling(CS) algorithm to achieve data focusing, i.e., the so-called two-step approach. To suppress the sidelobe level, an efficient strategy for the azimuth spectral weighting which only involves matrix multiplications and short fast Fourier transformations(FFTs) is proposed, which is a post-process executed on the focused SAR image and particularly simple to be implemented. The SAR image processed by the proposed extended CS algorithm is very precise and perfectly phase-preserving. In the end, computer simulation results verify the analysis and confirm the validity of the proposed algorithm. 相似文献
126.
在转子-支承耦合结构的动力学分析过程中,结构模态参数计算结果与实验测试结果往往存在较大差异。针对此问题,应用优化算法对结构动力学模型进行修正,使计算模型能更准确地反映结构特性。建立由梁单元、盘单元、弹性支承单元组成的结构动力学有限元模型;选择优化目标函数、设计参数,并对各参数进行灵敏度分析。应用粒子群算法对选取的设计参数进行优化,得到最优模型。利用转子-滚动轴承实验器进行验证,结果表明,方法能够有效地实现转子-支承耦合结构的动力学模型修正,修正后模型更接近实际结构。 相似文献
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空客A320飞机横航向控制律采用特征结构配置方法计算闭环增益,实现了期望特征值的配置及横航向关键参数之间的解耦。基于A320横航向控制律架构,提出使用线性二次型(Linear Quadratic,简称LQ)方法,对闭环增益进行重新设计。首先根据期望的特征值引入关键参数的频域整形环节,而后通过调整二次型性能指标加权矩阵实现期望特征值的逼近及关键参数之间的解耦,并求得闭环反馈增益,最后在特征结构、稳定裕度和横航向解耦效果方面与空客设计结果作了对比分析。仿真结果表明,LQ设计可获得与特征结构配置设计相近的结果,即得到接近期望值的特征值,并实现关键变量的解耦,同时保证了闭环稳定裕度。 相似文献
129.
基于FDUC模型和Ⅲ-Ⅴ族元素共价半径不变的假设,本文出了Ⅲ-Ⅴ族固溶体中原子近邻和次近邻的键长表达式。这套键长表达式除依赖于四个Ⅲ-Ⅴ族元素的含量(x,y)外,只与四个纯化合物的晶胞参数或这四个Ⅲ-Ⅴ族元素的共价半径有关。而且也含盖了相应的伪二元固溶体的情况。本文还对其他的理论模型作了进一步的比较和讨论。 相似文献
130.
(001)SiO2衬底上LiNbO3光波导薄膜的制备 总被引:2,自引:0,他引:2
采用脉冲激光淀积技术,在(001)取向的SiO2衬底上制备了LiNbO3薄膜。为了防止淀积过程缺氧,往淀积腔内充入10~15Pa的流动氧气,淀积速度0.3~1.0nm/min,淀积时间1h,淀积结束后,充入0.6Pa的氧气,在650℃保温0.5h。采用x射线衍射和扫描电镜对LiNbO3薄膜的微观结构及表面形貌进行了检测。结果表明:LiNbO3薄膜具有(012),(024)典型的LiNbO3粉末晶体衍射峰,薄膜成分晶体结构比较纯净,而且薄膜表面光滑。利用棱镜耦合法将波长为0.638μm的激光束耦合到LiNbO3薄膜中,观察到LiNbO3薄膜具有较好的光波导性能,可望应用于非线性光学器件 相似文献