1006-3242
2010 Issue 6
The Study on Reliability Judging Method for Electronic Equipment Based on Prior Information Fusion
HUANG Jingde;DUAN Lizhao;HAO Xueliang
HUANG Jingde;DUAN Lizhao;HAO Xueliang
..............page:85-88
The Design of Missile System with Integral Sliding Mode Control
YUE Mingqiao;LEI Junwei;LI Gaopeng
YUE Mingqiao;LEI Junwei;LI Gaopeng
..............page:29-32
1553B-Bus Communication Design Based on FPGA Control
ZHANG Fei;WANG Huanyu;XU Yupeng;CAO Xuelei;CHENG Zehao;LIANG Xiaohua
ZHANG Fei;WANG Huanyu;XU Yupeng;CAO Xuelei;CHENG Zehao;LIANG Xiaohua
..............page:67-71
Attitude Control Combined with Two Type Propulsions of Heavy Launch Vehicle
ZHANG Yu;XIAO Lihong
ZHANG Yu;XIAO Lihong
..............page:18-22
Registration Algorithm for SAR and Optical Images Based on Improved SIFT
YANG Xuemei;GONG Junbin;WANG Peng;TIAN Jinwen
YANG Xuemei;GONG Junbin;WANG Peng;TIAN Jinwen
..............page:13-17,22
The On-board Orbit Propagation System Design of Large Elliptical Orbit
SHI Li;ZHANG Shijie;YE Song
SHI Li;ZHANG Shijie;YE Song
..............page:43-48,55
Design of Distributed Simulation System for Navigation and Control of Satellite Constellation
ZHAO Shuangpeng;SONG Hua;LI Kehang;QIU Hongzhuan;YANG Jing
ZHAO Shuangpeng;SONG Hua;LI Kehang;QIU Hongzhuan;YANG Jing
..............page:56-62
Design of Object-Code Testing Environment for Flight Software
QIAN Jie;LI Zhongping;XU Chunlai
QIAN Jie;LI Zhongping;XU Chunlai
..............page:63-66,76
The Confidence Level Evaluation of Fuse Test System Based on the Improved Fuzzy Synthesis Judgments
ZHOU Yuliang;HE Guangjun
ZHOU Yuliang;HE Guangjun
..............page:89-92
Research on the Standard Rules for the Module Interface of On-Orbit-Service Spacecraft
XIE Weiqi;CAI Yuanwen;LI Yan;GUO Hui
XIE Weiqi;CAI Yuanwen;LI Yan;GUO Hui
..............page:49-55
..............page:32,88
Methodology Research of Virtual Instrument Design in Simulation Training System
XU Junming;ZHAO Hongchao;LI Guolin;FAN Shaoli
XU Junming;ZHAO Hongchao;LI Guolin;FAN Shaoli
..............page:72-76
Research on Carrier Rocket Testing System Based on BIT Technology
LIANG Xiaopeng;CAI Yuanwen;BO Wei
LIANG Xiaopeng;CAI Yuanwen;BO Wei
..............page:81-84,92
Research of USB Measurement System Velocity Data Optimum Filtering Technique
YANG Ping;SUN Gang;LIU Lisheng
YANG Ping;SUN Gang;LIU Lisheng
..............page:77-80
The Kalman Filtering Algorithm of SINS/TACAN Integrated Navigation System
LIU Ruihua;LIANG Longzhang
LIU Ruihua;LIANG Longzhang
..............page:7-9,12
Research on the Application of UKF in the X-ray Pulsar-based Autonomous Navigation
GUI Xianzhou;LI Zhihao;LI Shengliang
GUI Xianzhou;LI Zhihao;LI Shengliang
..............page:33-37
The Identification of the Target Miss in Azimuth Based on Converted Measurement Adaptive Kalman Filtering Algorithm with Debasing
JIAN Jinglei;LI Jing;REN Hongbin
JIAN Jinglei;LI Jing;REN Hongbin
..............page:23-28,32
The Adaptive Information Fusion Filtering Algorithm for Multi-constellation Integrated Navigation System
WU Ling;SUN Yongrong;CHEN Chuande
WU Ling;SUN Yongrong;CHEN Chuande
..............page:38-42,62
..............page:10-12
The Analysis of Error Characteristics of Orbit-Measurement Data and Orbit-Determination Results in the Spacecraft Injection Phase
MAO Yongxing;ZHU Weikang;NI Xiaoqiu;CHEN Jiahong;HUANG Kai
MAO Yongxing;ZHU Weikang;NI Xiaoqiu;CHEN Jiahong;HUANG Kai
..............page:93-98
The Optimization Design for High-Altitude Reentry Deceleration Trajectory of Hypersonic Missile
LIU Yunpeng;LI Ling
LIU Yunpeng;LI Ling
..............page:3-6