首页 | 本学科首页   官方微博 | 高级检索  
相似文献
 共查询到20条相似文献,搜索用时 78 毫秒
1.
介绍了多频段多目标海上测控模拟器的设计和实现方法。在硬件设计上,模拟器采用工控机和工作站架构,数字化可重组基带硬件平台技术,实现了不同频段、不同目标航天器的仿真功能。在软件设计上,采用RS422/232接口双中断驱动技术,实现了遥测和数传的同步;采用软件模块化和数据库融合设计技术,实现了多型号目标航天器的仿真需求。  相似文献   

2.
Electronics and computers have long been associated with aviation, defense and aerospace. Many aerospace advances would have been impossible without digital computers, and digital computers would not have progressed as rapidly without aerospace. In some sense you may thank aerospace for the computer on your desk and Internet in your life. DoD and NASA programs drove computer technology for the first 25 years, but in the 80s the primary thrust transitioned to the commercial sector. Aerospace computation requirements have driven the development of many electronic components such as transistors, ICs and memory technology. Advances in memory technology progressed from delay lines to electrostatic tubes to magnetic cores and now solid-state memory. As the need for number crunching grew, computers transitioned from batch processing, time-sharing, real-time computing, networking to the ubiquitous PC and Internet. How far is it from your hand-held PDA to the nano computer?  相似文献   

3.
介绍了红外成像导引系统数字图像处理计算机的硬件设计.它采用了TI公司最新推出的C64xTM系列新一代数字图像信号处理器-TMS320C6414和Xilinx公司超大规模现场可编程逻辑器件Virtex-Ⅱ系列的XC2V2000,实现一个高性能的弹载数字图像处理硬件平台,在红外焦平面成像导引系统中具有较高的实用价值和广泛的应用前景.  相似文献   

4.
智能旋翼的频域神经控制   总被引:3,自引:0,他引:3  
 频域内的神经控制方法在振动主动控制中因其允许复杂的控制算法,适合于智能旋翼的控制。在建立频域智能旋翼系统模型的基础上,提出了频域内的智能旋翼神经控制方法。采用正交设计方法选取训练样本,建立频域神经模拟器,然后按照提出的算法进行控制。仿真结果表明提出的算法有效,并且具有较好的鲁棒性。  相似文献   

5.
Science and technology advance neither steadily nor continuously. Concepts deemed obsolete and confined to oblivion find their niche in new developments. Discarded old methods revive as the key ingredients to new designs. Analog computing was the birthplace of two important technologies: Computer simulation, as applied to system design, was founded. The operational amplifier, to become the basis for modern linear circuitry, was perfected. Valuable as it was, analog simulation's quasi-hardware approach to analysis aggravated users as much as it aided them. When digital simulation languages arrived, simulation engineers readily adopted them. When the microprocessor transformed digital computers into inexpensive circuit components (more like gates, flip-flops, amplifiers, etc. than computers,) there arose unlimited prospects for digital control. But, the discrete digital and continuous analog worlds are not compatible. Timing discontinuities and variable resolution limitations create problems. Control system designs, especially microprocessor based ones, need laboratory development. For hands-on testing, the analog computer is as handy an instrument as a controls engineer could have. Its two unique and valuable functions are: Simulator of Systems to be Controlled... The electrical analogs or physical models, analog computer simulations offer predictable yet realistic representations of mechanisms and processes to be controlled. Programmable Linear Circuits Manifold... The terminal points for high quality, linear circuit devices, analog computer patch panels offer the only formal means of programing linear signal processing, interface and control circuits. This paper offers a discussion of these two analog computing uses.  相似文献   

6.
利用受控系统在频域的传递函数矩阵,直接设计频域最小阶Kx-观测器,可以避免状态空间实现这一中间环节,减少研究层次。本文利用多项式向量空间的对偶最小基和多项式矩阵的Popov阶梯形的概念,分析了频域最小阶Kx-观测器的设计问题,做了大量简化,得到一种设计算法,并附有例题说明。层次清楚,方法简便,在工程应用上是可取的。 文中对于频域Kx-观测器的可能最小阶数,也作了一些讨论,得到一些有益的结果。  相似文献   

7.
针对远程信号监测系统对测控仪器的要求,文中给出了在ISA卡上集成高精度频率计/信号源的设计原理与实现方法。该设计采用CPLD电路,对恒温晶振的输出信号和GPS的PPS信号进行自适应处理,克服了在实际应用中GPS秒脉冲信号易受干扰、晶振存在不确定漂移等因素造成的误差,将获得的高精度时钟信号和GPS秒脉冲信号作为基准信号用在测频电路和信号源中,使频率计和信号源可以长时间保持很高的精度,提高了系统的性能和可靠性。  相似文献   

8.
胡寿松  胡明华 《航空学报》1986,7(5):504-509
本文在频域范畴内,利用输出反馈方法论述了在二次型性能指标下多变量线性最优调节器的控制问题,通过把多变量系统的前馈解耦控制与最优控制结合起来,得到了最优控制解的频域形式。这种最优控制规律既可使系统的能耗和输出偏差综合最优,具有较好的抗干扰性,又可满足给定的时域性能指标。方法简单,求解方便,便于工程应用。作为例子,文中对某纵向飞行控制系统进行了最优设计。  相似文献   

9.
数字式颤振主动抑制系统的研究   总被引:4,自引:1,他引:3  
邹丛青  陈桂彬 《航空学报》1994,15(6):647-651
介绍了数字式颤振主动抑制系统的控制律综合、风洞实验及其工程特性。控制律的设计采用连续域离散化的方法。对4种不同控制律进行了风洞实验,验证了理论计算与实验设计的正确性。实验中控制律用微机和工业控制机联合实现;还根据工程应用的观点提出了颤振主动抑制系统应该具有的特性。对一个与实际飞机动力相似的机翼/外挂系统的研究表明,颤振速度提高了20%左右,并且系统的工程特性也是基本可行的。  相似文献   

10.
Nonlinear apodization for sidelobe control in SAR imagery   总被引:2,自引:0,他引:2  
Synthetic aperture radar (SAR) imagery often requires sidelobe control, or apodization, via weighting of the frequency domain aperture. This is of particular importance when imaging scenes containing objects such as ships or buildings having very large radar cross sections. Sidelobe improvement using spectral weighting is invariably at the expense of mainlobe resolution presented here is a class of nonlinear operators which significantly reduce sidelobe levels without degrading mainlobe resolution implementation is via sequential nonlinear operations applied to complex-valued (undetected) SAR imagery. SAR imaging is used to motivate the concepts developed in this work. However, these nonlinear apodization techniques have potentially broad and far-ranging applications in antenna design, sonar, digital filtering etc., i.e., whenever data can be represented as the Fourier transform of a finite-aperture signal  相似文献   

11.
郭锁凤 《航空学报》1984,5(2):178-185
 本文针对数字飞行控制系统的多速率特点,分析了等效变换的方法及变换成单速率系统的过程,并由此讨论了多速率系统的性能及其设计方法。  相似文献   

12.
黄俊钦  刘莎 《航空学报》1988,9(3):148-155
 本之将二维递归数字滤波器的时域设计转化为二维线性移不变差分模型的辨识问题。文中采用一种新的辨识方法,能确定滤波器的阶次和参数矩阵。该方法中运用了实时递推算法,使得初始信息矩阵较小,占用较少的内存空间,故比较实用。文中给出了设计实例。  相似文献   

13.
A digital autopilot design was developed for a small laser-guidedtactical missile. The multiloop design was developed in the w plane and analyzed by time domain simulation. Performance is as good or better than the current analog version, thus demonstrationg the feasibility of digital guidance technology in tactical missile applications.  相似文献   

14.
软开关组合式变换器建模与校正   总被引:2,自引:0,他引:2  
邢岩  严仰光  赵修科 《航空学报》1998,19(5):597-602
针对电流控制离散脉冲调制方式下的一种软开关组合式变换器,借助于时域仿真和付里叶变换建立系统频域模型(频率特性曲线),并在此基础上导出等效解析模型,为软开关组合式变换器系统性能分析提供了一种方便可行的方法,特别是解决了其电压调节器设计盲目性的问题。并给出了电压调节器设计及系统性能分析实例。  相似文献   

15.
The frequency domain approach to guidance system design is presented. The model of the guidance control system reflects the most important characteristics of the flight control system that combines airframe and autopilot dynamics (damping, natural frequency, time constant, and airframe zero frequency). The analytical expressions for frequency response and related expressions for missile system performance are given. The analytical results obtained can be utilized for missile system design.  相似文献   

16.
梁锋  张林昌  李春锦 《航空学报》1988,9(11):581-585
 一、概述 飞机设计的最终目的是为了获得具有良好的静、动态飞行品质,并能完成规定飞行任务的飞机。目前衡量飞行品质好坏的规范是MIL-F-8785C,该规范给出了飞行包线内飞机的静态控制品质、动态响应品质、对大气紊流的响应品质以及驾驶员的操纵要求等项规定。飞行控制系统设计者最关心的是动态响应品质。目前有多种确定飞机动态响  相似文献   

17.
随着数字化装配技术的逐渐成熟和推广应用,适应数字量传递的互换性设计对于提升飞机操纵面设计效率、稳定装配质量和降低维护成本具有显著的现实意义。以飞机操纵面的互换性设计为研究对象,针对互换性的要求分析设计要点,建立与数字化装配相协调的互换性设计流程;从操纵面的构型特征角度分析互换性设计的结构元素;提出实现操纵面互换性的技术途径,给出相应的参考指标;以某型飞机的副翼为例,对其进行互换性分析和设计,并通过实际装配进行检验。结果表明:操纵面互换性设计流程合理可行,能够满足互换性要求。  相似文献   

18.
19.
The cockpit design in the new JAS39 Gripen combat aircraft is based on an electronic computer-controlled display system. This display system EP 17, has four areas of presentation: one Head-Up Display (HUD) and three Multi-Function Displays (MFD). The HUD is equipped with a diffraction optics combiner which gives the display high visibility within a large field-of-view, and with minimal visual interference to the outside world. The Multi-Function Displays in the front panel are a Flight Data Display showing flight and system data, a Horizontal Situation Display that superimposes tactical information on a digital map and a Multi-Sensor Display with, primarily, radar information. This system is supported by a Display Processor comprising computers, graphic generators, sensor information processors and a digital map memory. It also includes an integrated video recording system for recording analog and digital sensor video, bus data and voice  相似文献   

20.
轴流压气机旋转失速DSP在线控制方法   总被引:1,自引:0,他引:1  
李琳  聂超群 《航空学报》2009,30(5):787-793
针对压气机旋转失速的在线控制新方法进行了实验研究。构造了完整的数字信号处理(DSP)控制方案,并在单级低速轴流压气机实验台上完成了实验验证。在对动态信号进行时域分析、频域分析、滤波及相关性分析的基础上,确定了旋转失速在线控制的整定值,结合叶顶微喷气扩稳方法,在不同相关系数设定的条件下,进行了旋转失速在线反馈控制的实验研究。实验结果显示该DSP控制系统与相关计算方案结合具有有效的控制效果,为压气机流动失稳控制技术发展探索一种新的方式。  相似文献   

设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号