基于单片机与FPGA的等精度频率计设计

根据等精度测频原理,利用单片机与FPGA结合设计等精度数字频率计。待测频率信号经过整形放大后输入到FPGA,单片机控制FPGA通过内部脉冲计数器对待测信号和标准信号源同时计数,单片机读回测频数据后,经运算处理后显示。等精度频率计测频精度高,且精度不随频率的变化而变化。单片机与FPGA结合,测频速度快,范围宽,可靠性高。     

利用最佳分频实现高精度频率测量

根据频率测量中的主要误差来源,提出利用最佳分频来实现高精度频率测量的方法。针对导弹测量的实际应用,以计数测频法中的等精度测频法为基础,利用最佳分频的2条原则,在QUARTUS平台上对设计进行仿真。仿真结果证明：该方法能继承等精度测频的优点,满足100MHz以内的频率测量,改进等精度测频需要固定的闸门选通时间的不足。     

伪码调相脉冲信号识别

提出了频谱搬移的方法,对信号进行不同精度的FFT变换,利用高精度的FFT变换来测量信号频率,再利用测得的频率对低精度的FFT变换直接进行频谱搬移,从而实现精确的下变频,提取出信号中的伪随机码。该方法避免了测频误差对下变频的影响,从而使得伪随机码的侦察识别在工程上可以实现。     

基于改进的Rife测频算法及其FPGA实现

为了提高数字接收机的测频精度,文中在分析Rife算法性能的基础上,提出了一种改进的Rife测频算法,并对该算法的原理和FPGA实现步骤进行了详细说明。仿真结果表明,在相同的信噪比条件下,该算法的测频误差小于Rife算法。同时,为了提高算法的运算速度,在利用FPGA实现时,将对数运算利用查找表方法实现,采用减法操作替代除法运算,使测频速度高达240MHz。最终实测结果验证了算法的有效性。     

相位测频法在雷达脉冲载频提取中的应用

摘要：脉内载频特征是雷达被动信号分选的关键参数,为提高雷达信号载频特征提取精度,引入相位测频法。 利用希尔伯特变换将原始信号转换为复信号,进而求取各采样点对应的相位及瞬时频率,对各点瞬时频率取均值作 为信号载频特征。将相位测频法与傅里叶变换法、计数法进行了仿真对比,结果表明：相位测频法在低载频、短脉 宽的情况下测频精确度优于傅里叶变换法和计数法。因此相位测频法应用于雷达载频特征提取,能有效提高测频精 度和稳定性,为复杂背景下雷达被动信号分选与识别提供支持与保障。     

基于分数阶傅里叶变换的标量脱靶量测量新方法

针对多普勒测量法恒幅恒频假设在脱靶量点附近会引起较大的测频误差的问题,提出了一种基于恒幅chirp信号假设的准实时标量脱靶量测量方法。通过延长多普勒频率的拟合分段时长,有效地增大了积累时间。利用分数阶傅里叶变换的快速离散算法来实现。仿真结果表明,相比基于FFT的方法,测量精度更高、鲁棒性更好,尤其是在较低信噪比的情况下,但计算复杂度略有增加。     

单脉冲雷达主动测角与被动测角的建模与仿真

文中通过对回波信号、噪声调频干扰信号、热噪声信号以及单脉冲雷达角跟踪系统各电路模块的数学建模,在Matlab下对主动测角与被动测角情况进行了仿真和比较,得出被动测角误差大于主动测角误差的结论.该结论为进一步提高单脉冲雷达跟踪噪声源测角精度提供依据.     

一种基于伪码测距的高度表实现方案

针对高度表测高范围大,测距精度高的要求,文中给出了一种基于伪码测距高度表的实现方案,应用伪码时延的码元整周期数进行粗测距,将收端伪码信号进行锁相提纯及采用差频测相技术对伪码时钟信号相移精确测量以达到精测距.这一方案,在计时时钟频率仅为50MHz的条件下,测高精度优于0.3m,量化误差小于0.2m.     

不同信道条件下的跳频信号时差估计方法

时差估计是跳频信号跟踪定位系统中的关键组成部分。针对平坦衰落信道和频率选择性衰落信道2种情况分别研究了跳频信号的时差估计方法。结论表明信道模型对跳频信号时差估计精度影响较大。在平坦衰落信道条件下,多跳信号能同时实现观测时间和带宽上的积累,从而可以获得远高于频率选择性衰落信道的时差估计精度。但在频率选择性衰落信道条件下,多跳信号只能实现观测时间的积累而不能实现带宽上的相参积累。     

伪码脉冲引信m序列的相位校正二阶差分识别

应用FFT测脉冲初始相位并计算相位序列的二阶差分来识别伪码脉冲引信信号m序列,在信号环境复杂、信噪比较低的情况下,存在误差较大、识别正确率低的问题。为此,提出在测脉冲初始相位的同时,通过检测测频误差来对消测相误差,对相位序列二阶差分进行校正的相位校正二阶差分方法来识别信号m序列。在不同信噪比条件下,仿真结果显示相位校正二阶差分识别算法能取得更好的识别效果。     

Open Rule-setting System Applied to Conceptual Design of Engines

Open rule-setting method advanced in this paper concentrates on providing designers of engines with a convenient way to express their design innovations and develop the expected prototypes in the early CAD stage, and constitute effective models for the following analysis process of CAE and CAPP. The problems arisen in the process of conceptual design with the traditional experience-based development method are analyzed. Based on those analyses, open rule-setting method is presented and some associated technical problems are discussed. The functional framework of open rule-setting system was built as software engineering methods. The speciality of the engine product as a kind of complex product and the requirement of the engine product based on its structural particularity to rule-setting system are considered carefully. A demonstration is supplied to illustrate how the open rule-setting method enhances the efficiency and quality of the engine conceptual design.     

Research on Linux Network Device Driver

By analyzing the working principle of Linux network device driver, discussing the Linux network driver structure and its key technologies, the general network driver structure and its design methodologies in Linux system are summarized. Through modifying the network device driver of Linux device driver 3rd version snull, c and improving the COW technology, the Zero-Copy technology in Linux （kernel version 2.6.11 ） is implemented. In the end, the success test tells us that the thorough analysis of network device driver is the foundation of many applications, and it also provides a certain improvement to a lot of real applications, even to military application development.     

Algorithm for Multi-laser-target Tracking Based on Clustering Fusion

Multi-laser-target tracking is an important subject in the field of signal processing of laser warners. A clustering method is applied to the measurement of laser warner, and the space-time fusion for measurements in the same cluster is accomplished. Real-time tracking of multi-laser-target and real-time picking of multi-laser-signal are introduced using data fusion of the measurements. A prototype device of the algorithm is built up. The results of experiments show that the algorithm is very effective.     

Influence of Installing Error on the Surface Shape Precision of the Axial Symmetry Aspheric Workpiece in Lapping

A method to calculate the surface shape error, which is caused by the installing error between the workpiece and the lapping tool in the process of form lapping, is proposed. The mathematical model which the installing translation error influences on the workpiece surface shape error is established. The changing rule of the error is simulated through the calculating example of the paraboloid workpiece. The results indicate that the surface shape error of the workpiece is increasing with the increase of the installing translation error, it is also increasing gradually along the center point of the curve surface to the edge, and the influence is severer to the curve surface with great curvature than that of the small curvature when the translation error is the same.     

Experimental Research on Output Performances of Giant Magnetostrictive Actuator

The paper introduces the performances of magnetostrictive actuators and its applications, discusses the design methods for the structure and internal magnetic circuit of a giant magnetostrictive actuator, and makes tests on the output displacement and force characteristics for an actuator using homemade magnetostrictive material. The experimental result shows that the actuator has satisfactory output precisions and ranges in transient and stable states, and can be used in lowfrequency vibration control system of precise equipment.     

Overview of Anti-tank Mines

First the different anti-tank mines laying possibilities are shortly summarized： hand emplaced, with mine layers, ground or helicopter relatively topographical well defined, and with cluster systems of projectiles, rockets and aircraft dispensers. Then examples of the three generations of anti-tank mines are presented：Ⅰ generation： detonating only beneath the track; Ⅱ generation： detonating beneath the track and belly; Ⅲ generation： mines with off-route actions. Weight and cost comparisons are strongly favoring the off-route Ⅲ-generation mines.     

A Finite Element Analysis on Static Strength of a Complex Section

A static finite element analysis （FEA） of an impulsive controller section is presented. The boundary condition and a part of the loads are applied. Considering the grades of the stress around the holes being large, the dense grids are adjusted accordingly. Four cases with different loads are compared, thus the influences of different loads on the section are analyzed. Numerical results show that the maximum stress of the section is lower than the strength limit of the material, and the section will not be broken with the static loads.     

Discussion on Mechanism of Breech-Blow Caused by Propellant Charge

From the view point of launch safety caused by fracture of propellant charge, this paper points out that the safety criterion of pressure wave is inadequate to evaluate the launch safety of propellant charge based on the initial negative differential pressure and sensitivity tests. Generally, the maximum barrel pressure does not depend upon the intensity of pressure wave correspondingly. The pressure wave intensity can not describe the fracture degree of propellant charge in chamber and reflect the mechanical environment of propellant charge fracturing exactly and wholly. The evaluation criterion for launch safety of propellant charge should be built on the basis of depicting the fracture degree of propellant bed.     

Experimental Studies of Toxicity on HNIW and Its Intermediates

The polycyclic nitramine hexanitrohexaazaisowurtane（HNIW） is a compound of high energy density. HNIW can replace 1, 3, 5-trinitro-1, 3, 5-triazacyclohexane（RDX） or HMX, hut its toxicity is unknown. In this paper, HNIW, hexabenzylhexaazaisowurtzitane （HBIW）, tetraacetyldibenzulhexaazaisowurtzitane （TADBIW）, tetraacetyldiformylhexaazaisowurtzitane（TADFIW） and tetraacetylhexaazaisowurtzitane（TAIW）, which are intermediates of the synthesis of the HNIW, were selected as the tested objects in acute toxicity test, acute eye stimulation test and skin irritation test according to the standards of ＂chemical product testing method-401 ： acute oral toxicity test＂, ＂chemical product testing means-405： acute eye irritation/corrosion test＂ and ＂chemical product testing means-404： acute dermal irritation/corrosion test＂ of National Circumstance Protect Bureau. The results show that all of the five objects have no toxicity, no stimulation to eye and skin under the tested conditions.     

Dynamic Simulation for Missile Erection System

In order to study the dynamic characteristics of the missile erection system, it can be considered as a rigid-flexible coupling multi-body system. Firstly, the actual system is abstracted as an equal and simplified one and then the forces applied to it are analyzed. Secondly, the rigid-flexible coupling dynamic simulation for erection system is accomplished by use of the system simulation software, for example Pro/E, ADAMS, ANSYS, MATLAB/Simulink, etc. Finally, having the aid of simulation results, the kinetic and dynamic characteristics of the flexible bodies in erection system are analyzed.The simulation considering the erection system as a rigid-flexible coupling system can provide valuable results to the research of its kinetic, dynamic and vibrational characteristics.