2006-10题录英译集

上传人:j****9 文档编号:45021536 上传时间:2018-06-14 格式:DOC 页数:21 大小:244KB
返回 下载 相关 举报
2006-10题录英译集_第1页
第1页 / 共21页
2006-10题录英译集_第2页
第2页 / 共21页
2006-10题录英译集_第3页
第3页 / 共21页
2006-10题录英译集_第4页
第4页 / 共21页
2006-10题录英译集_第5页
第5页 / 共21页
点击查看更多>>
资源描述

《2006-10题录英译集》由会员分享,可在线阅读,更多相关《2006-10题录英译集(21页珍藏版)》请在金锄头文库上搜索。

1、兵工自动化 摘要英译集 2006 年第 10 期12006-10 题录英译集 *武器装备自动化 组合导航系统的加权数据融合算法潘爽,徐彬,马林立 (海军潜艇学院 研究生队,山东 青岛 266071)摘要:单一导航传感器的不确定评定分为:对不确定度大的观测值赋予小的权值,对不确定度小的观测值赋予大 的权。再根据组合不确定度最小的原则,采用拉格朗日乘数法进行加权值求解。最后,通过对双组合导航系统的加权 数据融合,证明该法具有较高的融合精度,同时也为加权数据融合法的加权因子分配提供了较好的途径。 关键词:组合导航系统;数据融合;动态不确定度;加权值Weight Data Fusion Algorit

2、hm for Combined Navigation SystemPAN Shuang, XU Bin, MA Lin-li (Brigade of Graduate, Naval Submarine Academy, Qingdao 266071, China)Abstract: The uncertainty evaluation for single navigation sensor includes giving the big uncertainty degree observation value with the small weight value and giving th

3、e small uncertainty degree observation value with the big weight value. Under the condition of minimum combined uncertainty, the weight values were calculates by the Lagrange method. At last, through the weight data fusion of combined navigation system, the simulation indicated the algorithm had a h

4、igh fusion accuracy. The algorithm also provided better method with the weight factor distribution of weight data fusion method at the same time. Keywords: Combined navigation system; Data fusion; Dynamic uncertainty degree; Weight value* 单信道相位相关干涉仪的通信测向技术李炳荣,曲长文,唐小明 (海军航空工程学院,山东 烟台,264001)摘要:单信道相位相

5、关干涉仪的通信测向技术,是将多个天线阵元接收的信号作移相合成。并按时序通过接收 机信道,进行混频、放大和检波,得到 1 组相位和幅度数据。与预存数据库进行相关,完成通信测向。并在通信测向的 同时,得到信号的其他参数值。 关键词:干涉仪;相位相关;通信测向;单信道Communication Direction Finding Technique for Single-Channel Phase Correlating Interferometer LI Bing-ron, QU Chang-wen, TANG Xiao-ming (Naval Aeronautical Engineering A

6、cademy, Yantai 264001, China)Abstract: The communication direction finding technique for single-channel phase correlating interferometer was realized by phase-shifting combination for received signals of multi-units antenna. Then, passing the receiver channel according to the time sequence, mixing,

7、amplify and demodulating, a set of data of phase and ample was obtained. After correlating with database deposited, the direction finding was realized. And the other parameters of signal were obtained at the same time. Keywords: Interferometer; Phase correlating; Direction finding; Single-channel *

8、红外/毫米波雷达双模导引末状态的目标跟踪算法王飞,万少松,袁华 (空军工程大学 导弹工程系,陕西 西安 710051)摘要:红外/毫米波雷达双模导引末状态的目标跟踪算法基于目标形心估计法。即在复合跟踪的基础上先进行空 间配准,再建立跟踪窗口,然后在窗口内逐场或逐帧计算出目标图像形心坐标相对于窗口中心的偏离量,并实时输送兵工自动化 摘要英译集 2006 年第 10 期2给复合导引头数据融合跟踪系统。该算法包括图像输入、选择灰度门限并确定跟踪窗口、计算质心及求得质心加权平 均、窗口中心的自适应调整、判断递推过程中止条件等步骤。 关键词:红外成像跟踪算法;目标形心估计;双模导引末状态;红外/毫米波雷

9、达Target Track Algorithm Based on Double-Module Guided End Appearance of Infrared/Millimeter Wave RadarWANG Fei, WAN Shao-song, YUAN Hua (Dept. of Missile Engineering, Air Force Engineering University, Xian 710051, China)Abstract: The target track algorithm of double-module guided end appearance for

10、infrared/millimeter wave radar was based on target centroid evaluation method. That is, the space registration was carried out based on, and the track window was established. Then, the shifting value of the target image centroid coordinates compared with window center was calculated by field or by f

11、rame in window; after that, the results were sent to combined head appearance data fusion track system. This algorithm includes image input, calculating the centroid and centroid weight average, the self-adjusting of window center, judging the suspending conditions of recursion process and so on. Ke

12、ywords: Infrared image track algorithm; Target centroid evaluation; Double-module guided end appearance; Infrared/millimeter wave radar* 某型导弹多功能发射车调温系统的优化控制李锦冬,李润成 (二炮装备研究院 第三研究所,北京 100085)摘要:某型导弹多功能发射车调温系统发射筒半导体致冷器的优化控制,使用四个桥臂控制工作电流换向。供 电电源则将 14 只功率场效应晶体管 MOSFET 接入电源变压器次级,两绕组的全部组合可构成 18 个不同扎数的次级。 控

13、制电路按时采集筒内、外温度并计算温差,同时采集三路电压和电流取样信号,运算后得到电源主电路中 MOSFET 管的通断开关控制量,实现半导体致冷器最佳工作电流控制。 关键词:发射车调温系统;温度控制;半导体致冷器;场效应晶体管Temperature Regulation System Optimizing Control for Multi- Function Launch Vehicle of Certain MissileLI Jin-dong, LI Run-cheng (The 3rd Institute, Second Artillery Equipment Research Inst

14、itute, Beijing 100085, China)Abstract: The temperature regulation system optimizing control for multi-function launch vehicle of certain missile adopted 4 arms to control work current commutation. The power source used 14 power file effect transistor MOSFET in power transformer second order; all the

15、 combinations of twist-coil could construct 18 different second orders. The control circuit adopted the in-barrel and out-barrels temperatures and calculated the temperature difference. At the same time the sampling signals of three-way voltage and current were adopted. After calculation, the switching switch control value of MOSFET in main

展开阅读全文
相关资源
正为您匹配相似的精品文档
相关搜索

最新文档


当前位置:首页 > 生活休闲 > 科普知识

电脑版 |金锄头文库版权所有
经营许可证:蜀ICP备13022795号 | 川公网安备 51140202000112号