現(xiàn)代控制理論及其應(yīng)用

神經(jīng)網(wǎng)絡(luò)專家系統(tǒng)在電源系統(tǒng)診斷中的應(yīng)用*………………………………………安若銘 王 均(3 －88)

分?jǐn)?shù)階控制器實(shí)現(xiàn)方法研究 ………………………………………………鄺 鈺 吳 潤 李 巖(4 － 3)

基于RBF 神經(jīng)網(wǎng)絡(luò)及Luenberger 觀測(cè)器的反演設(shè)計(jì)……………………………………………………王林旭 張勝修 曹立佳 馮福沁 趙 煒(5 － 3)

導(dǎo)彈、運(yùn)載器制導(dǎo)與控制技術(shù)

一種寬頻被動(dòng)雷達(dá)制導(dǎo)信號(hào)的魯棒濾波方法 ………………………………………程雪梅 楊俊鵬(1 － 3)

一種基于速度傾角的閉路制導(dǎo)方法 ………………………………………馬瑞萍 肖 凡 張 濤(1 － 6)

基于SAR 景象不變特征點(diǎn)的匹配定位技術(shù)研究 …………………………唐 波 張 輝 劉 彥(1 －10)

北斗系統(tǒng)格網(wǎng)電離層延遲算法研究*………………………………………詹先龍 劉瑞華 楊兆寧(1 －15)

應(yīng)用模糊控制方法的擾動(dòng)引力計(jì)算 ……………………………………………………………王激揚(yáng)(1 －20)

基于H－矩陣/QFT 的魯棒解耦多變量控制在SRLV 姿態(tài)控制中的應(yīng)用…………………………………………………………………………趙志芳 肖利紅 倪少波(2 － 3)

基于彈道制導(dǎo)一體化的巡航飛行器末制導(dǎo)方案研究… …穆育強(qiáng) 王丹曄 孫曉松 黃興李 陳新民(2 － 7)

基于魯棒狀態(tài)觀測(cè)器的運(yùn)載火箭姿態(tài)控制系統(tǒng)設(shè)計(jì) ……………………周 軍 水尊師 葛致磊(2 －11)

灰色層次分析法在導(dǎo)彈武器系統(tǒng)生存能力評(píng)估中的應(yīng)用研究 ……………………邱令存 惠 軼(2 －17)

合成孔徑雷達(dá)子孔徑數(shù)據(jù)改進(jìn)ECS 成像算法 ……………………………楊立波 陸和平 高 磊(2 －22)

基于角速率和速度增量的捷聯(lián)慣性導(dǎo)航算法研究 ………………………王偉鵬 楊 博 李 方(3 － 3)

迭代制導(dǎo)情況下姿態(tài)控制系統(tǒng)穩(wěn)定性分析方法研究 ………………………………王 輝 張 宇(3 － 7)

基于擴(kuò)展卡爾曼濾波的機(jī)動(dòng)目標(biāo)跟蹤研究*…………………………………………張 蕊 史麗楠(3 －12)

基于動(dòng)態(tài)逆的高超聲速飛行器高度控制方法 …………………………………………………王 健(3 －19)

基于不對(duì)稱再入體的移動(dòng)質(zhì)心滾動(dòng)控制方法 ………………………………………李自行 李高風(fēng)(3 －23)

高超聲速飛行器制導(dǎo)與控制性能評(píng)估方法 ……………………………………………………馬衛(wèi)華(4 － 7)

小型無人機(jī)在簡(jiǎn)化傳感器配置下的自主回收控制系統(tǒng)設(shè)計(jì) …………………………………王航宇(4 －13)

基于hp 自適應(yīng)偽譜法的固體運(yùn)載火箭軌跡優(yōu)化 ……………………………………洪 蓓 辛萬青(4 －18)

光纖通道在航天運(yùn)輸系統(tǒng)的應(yīng)用分析 ……………………………………江云秋 張 瑋 蔣彭龍(4 －23)

BTT 導(dǎo)彈動(dòng)態(tài)逆－PID 控制律設(shè)計(jì)*………………………………………張維剛 雷虎民 劉 君(4 －27)

高超聲速飛行器Terminal 滑?？刂葡到y(tǒng)設(shè)計(jì)*……………………………王 鵬 劉魯華 吳 杰(5 － 9)

小型空天飛行器制導(dǎo)導(dǎo)航與控制系統(tǒng)方案*………………………………晁 濤 王松艷 楊 明(5 －15)

陀螺隨機(jī)游走對(duì)導(dǎo)彈自瞄準(zhǔn)精度的影響 ……………………………………………楊俊峰 司文杰(5 －21)

地空導(dǎo)彈武器系統(tǒng)網(wǎng)絡(luò)化作戰(zhàn)模式分析研究 ………………………………………王 希 李建勛(5 －25)

基于改進(jìn)速度增益的中段變軌制導(dǎo)方法研究…………………………………………張 俊 董文杰 訾乃全 李 剛 林金永 李雙喜(5 －30)

大氣層內(nèi)飛行器風(fēng)速在線辨識(shí)方法 …………………………………………………孫 友 楊廣慧(6 － 3)

再入飛行器偏離穩(wěn)定判據(jù)的研究與應(yīng)用 …………………………………曹玉騰 王曉東 倪少波(6 － 7)

面向控制的可變形乘波體概念設(shè)計(jì)與分析*………………………………鄧 俊 劉燕斌 張 勇(6 －13)

基于某無人機(jī)操縱面故障重構(gòu)控制方法研究 ………………………………………鄭友勝 江 維(6 －20)

空間飛行器制導(dǎo)、導(dǎo)航與控制技術(shù)

基于浮空器的新型應(yīng)急通信監(jiān)測(cè)系統(tǒng) ………………………………………………費(fèi)東年 趙攀峰(1 －23)

翼傘系統(tǒng)雀降性能及控制研究 ………………………………………………………張興會(huì) 朱二琳(1 －29)

星光折射導(dǎo)航星的改進(jìn)三角識(shí)別捕獲 ………………………………………李旻珺 楊 博 胡 靜(1 －33)

基于遺傳算法的空間自由漂浮機(jī)械臂系統(tǒng)運(yùn)動(dòng)規(guī)劃*………………………………李 巖 蔡遠(yuǎn)文(1 －40)

亞軌道飛行器返回軌跡快速優(yōu)化 ………………………………………………………………王文虎(2 －28)

基于Gauss 偽譜法的高超聲速飛行器多約束三維再入軌跡優(yōu)化 …………………姚寅偉 李華濱(2 －33)

質(zhì)量矩控制飛行器的壓心不確定性問題研究*……………………………魏鵬鑫 高長生 荊武興(2 －39)

一種天基光學(xué)GEO 目標(biāo)定位方法及初軌算法觀測(cè)幾何評(píng)價(jià) ……………王雪瑩 李 駿 安 瑋(2 －46)

非開普勒軌道下衛(wèi)星交會(huì)變軌決策研究 …………………………………張 拓 高曉光 樊 昊(2 －51)

基于借力飛行技術(shù)的星際多目標(biāo)交會(huì)轉(zhuǎn)移軌道設(shè)計(jì) …………………………………………胡青龍(2 －57)

基于X 射線脈沖星的“夸父A”衛(wèi)星自主導(dǎo)航和軌道控制 ……趙露華 費(fèi)?？?肖 昱 姚國政(3 －29)

基于擴(kuò)展卡爾曼濾波器的航天器姿控飛輪故障診斷 ………………………………吳紅芳 王 志(3 －34)

基于輸入受限的軌控期間撓性衛(wèi)星容錯(cuò)控制研究*………………………傅艷萍 程月華 姜 斌(3 －38)

基于擬歐拉角描述的上面級(jí)姿態(tài)控制律設(shè)計(jì) ……………………………夏喜旺 劉漢兵 杜 涵(3 －45)

基于飛輪控制的空間機(jī)器人質(zhì)量參數(shù)辨識(shí) ………………………………王 超 杜小平 高永明(3 －51)

地球同步帶SBV 監(jiān)視系統(tǒng)誤差分析與觀測(cè)數(shù)據(jù)仿真 ……………………唐 毅 吳美平 付曉鋒(3 －56)

空天飛行器迭代制導(dǎo)初值生成方法研究 ………………………朱建文 劉魯華 湯國建 徐明亮(3 －61)

基于視覺和MEMS-IMU 融合的火星車導(dǎo)航定向技術(shù)*………………………………………婁 路(4 －32)

基于羅格里斯參數(shù)的航天器遞歸線性姿態(tài)估計(jì)算法……………………………………………………羅宇陽 龔德仁 陳筠力 段登平 邵曉巍(4 －37)

基于Lawden 改進(jìn)型方程的編隊(duì)Unscented Kalman Filter 濾波估計(jì)………………………………………………………………溫 洲 邵曉巍 陶久亮 龔德仁(4 －42)

用四元數(shù)描述飛行器姿態(tài)時(shí)的幾個(gè)基本問題 …………………………………………………范奎武(4 －49)

空間多目標(biāo)攔截交會(huì)平臺(tái)停泊軌道設(shè)計(jì)優(yōu)化 ………………………………………吳蓓蓓 黃 海(4 －54)

一種基于光學(xué)成像敏感器多目標(biāo)視線角測(cè)量的相對(duì)導(dǎo)航方法………………………………………………………………劉 濤 胡海霞 王 穎 王大軼(5 －35)

一種無陀螺無推力器的衛(wèi)星姿態(tài)安全控制方案研究 ………………………………李明群 宗 紅(5 －42)

基于最優(yōu)推力錐的級(jí)聯(lián)推力分配算法*………………………………………………朱孟萍 徐世杰(5 －48)

基于改進(jìn)擬歐拉角的飛行器姿態(tài)控制律設(shè)計(jì) ……………………………夏喜旺 劉漢兵 杜 涵(5 －55)

帶轉(zhuǎn)動(dòng)部件航天器的RBF 神經(jīng)網(wǎng)絡(luò)滑模姿態(tài)控制*……………………杜小平 郝剛濤 高永明(5 －61)

基于GEO 帶觀測(cè)的天基光學(xué)監(jiān)視系統(tǒng)設(shè)計(jì) …………………………………………刁華飛 李 智(5 －66)

基于雙曲線B 平面參數(shù)的快速微分修正月地返回軌道精確設(shè)計(jì) …………………周 亮 胡 軍(6 －27)

基于狀態(tài)觀測(cè)器的高超音速飛行器動(dòng)態(tài)面反步控制*…………王首斌 王新民 姚從潮 謝 蓉(6 －32)

Galileo 系統(tǒng)完好性參數(shù)SISMA 的影響因素分析*………………………張雪輝 貝 超 王 芳(6 －38)

再入飛行器可達(dá)區(qū)域近似算法及地面覆蓋研究 …………………………馮必鳴 聶萬勝 李 柯(6 －43)

衛(wèi)星姿態(tài)采樣系統(tǒng)的魯棒H∞控制 …………………………………………劉善伍 張 銳 張 靜(6 －50)

基于模型預(yù)測(cè)控制的近空間飛行器容錯(cuò)跟蹤控制*………………………賀 娜 姜 斌 齊瑞云(6 －54)

計(jì)算機(jī)技術(shù)與仿真技術(shù)

電子控制器PCB 板電磁兼容性仿真與試驗(yàn)研究 ………………張 寅 葉志鋒 徐建國 曹志潔(1 －49)

基于UML 的任務(wù)空間概念模型動(dòng)態(tài)行為驗(yàn)證研究*………………………………高江林 吳曉燕(1 －54)

1553B 多功能RT IP 核的設(shè)計(jì)與實(shí)現(xiàn) … ……………………………………李 輝 張敬波 張 磊(1 －59)

含無序量測(cè)的多傳感器目標(biāo)跟蹤濾波算法 ……………………………………………………蔣春蕾(2 －63)

近空間高超聲速飛行器慣性導(dǎo)航系統(tǒng)Simulink 仿真研究*……彭 惠 熊 智 劉建業(yè) 王 融(2 －69)

基于Orbiter 的航天器升力式再入特性仿真*……………………………董彥非 譚釗勝 陳曉飛(2 －75)

CFDP 協(xié)議中延遲NAK 文件傳輸時(shí)間分析與仿真 ……………………………………………梁迎春(2 －80)

一種基于MiniGUI 的多任務(wù)嵌入式軟件設(shè)計(jì) ………………………………………靳曉園 馬穎勁(3 －65)

基于修正條件判定覆蓋的軟件測(cè)試技術(shù)研究和方法應(yīng)用 …………………………岳 海 任慧敏(3 －69)

臨近空間飛行器多物理場(chǎng)耦合建模的網(wǎng)格映射方法……………………………………………………劉 璟 王 玲 胡東飛 鐵 鳴 吳旭生(3 －73)

天地信息一體化的飛行控制系統(tǒng)綜合集成技術(shù)研究……………………………………………………董文杰 張春俠 訾乃全 周春梅 張 俊(3 －78)

CFDP 協(xié)議中延遲NAK 模式的一種改進(jìn)建議*…………………………………………………梁迎春(4 －60)

實(shí)現(xiàn)紅外導(dǎo)引頭系統(tǒng)仿真自動(dòng)化技術(shù)研究 …………………………………………喬曉慧 董云峰(4 －64)

航天產(chǎn)品試驗(yàn)數(shù)據(jù)分析與管理系統(tǒng)設(shè)計(jì)研究 ………………………………………王曉斌 古 偉(4 －68)

基于改進(jìn)PSO 算法的岸基導(dǎo)彈火力分配研究*………………王光源 汲萬峰 孫鈞正 章堯卿(5 －71)

基于DoDAF 的體系結(jié)構(gòu)信息一致性的修改方法 ………………閆 梁 杜小平 趙繼廣 李 轅(6 －59)

CFDP 中延遲NAK 雙重傳方案的驗(yàn)證與分析*…………………………………………………吳海濤(6 －65)

測(cè)試、發(fā)射和控制技術(shù)

運(yùn)載火箭大容量CPCI 集成數(shù)據(jù)采集與測(cè)試系統(tǒng)設(shè)計(jì) ………………………………趙 娜 張 磊(1 －66)

混合總線測(cè)試技術(shù)靶場(chǎng)應(yīng)用研究 ………………………………………………………………高政民(1 －71)

1553B 總線故障注入測(cè)試方法研究 …………………………………………………連 盟 李學(xué)鋒(2 －84)

基于硬解題的PLC 設(shè)計(jì)及其在測(cè)發(fā)控系統(tǒng)中的應(yīng)用 ………………………………宋征宇 劉亮亮(5 －78)

運(yùn)載火箭測(cè)試發(fā)射控制通信網(wǎng)絡(luò)監(jiān)控與管理系統(tǒng)的設(shè)計(jì)與實(shí)現(xiàn) ………陳 放 田建宇 孫兆牛(5 －83)

全數(shù)字仿真測(cè)試環(huán)境在星載嵌入式軟件測(cè)試中的應(yīng)用 …………………郭 華 武占峰 吳 瑾(6 －70)

基于目標(biāo)特征模型配置的面向?qū)ο髾z測(cè)方法研究 ………………………蔡華杰 龔俊斌 田金文(6 －73)

可靠性、安全性和維修性

航天發(fā)射場(chǎng)加注系統(tǒng)風(fēng)險(xiǎn)評(píng)估技術(shù)研究*…………………………………宋建軍 杜小平 趙繼廣(1 －76)

基于橋接模式的雙網(wǎng)絡(luò)重復(fù)使用運(yùn)載器控制系統(tǒng)冗余技術(shù) ……………漆光平 孫 鵬 李光杰(2 －89)

基于相似電子產(chǎn)品信息的可靠性評(píng)估方法 …………張立波 王宏力 陳 聰 崔祥祥 朱天文(3 －84)

液體火箭發(fā)動(dòng)機(jī)傳感器故障檢測(cè)與數(shù)據(jù)恢復(fù)算法研究*…………………黃 強(qiáng) 劉洪剛 吳建軍(4 －73)

新型截尾試驗(yàn)下航天器電源系統(tǒng)的可靠性評(píng)估*……………………………………孫天宇 師義民(5 －88)

在保障過程中的某型導(dǎo)彈故障診斷專家系統(tǒng) …………………………………………………張嘉展(6 －78)

多分類SVDD 混疊域識(shí)別新方法與故障診斷應(yīng)用*…………………………………蔡金燕 杜敏杰(6 －83)

光機(jī)電一體化

基于Fluent 計(jì)算的火箭離軌姿態(tài)運(yùn)動(dòng)仿真與分析 …………………………………關(guān) 宏 徐世杰(3 －93)

基于“筆”輸入模式的產(chǎn)品結(jié)構(gòu)草圖快速設(shè)計(jì)系統(tǒng)研究 ………………………………………訾乃全(4 －77)

STSS 紅外傳感器探測(cè)性能分析 ………………………………………………………佘二永 彭 灝(4 －81)

一種高可靠大容量信息記錄儀設(shè)計(jì)方案研究 ………………………………………吳瑞峰 張宏波(6 －89)

綜述

彈道式飛行器慣性制導(dǎo)機(jī)電式方法的研究歷史 ………………………………………范奎武 崔鑫水(1 －81)

末端導(dǎo)引律綜述*……………………………………………………………孫 勝 張華明 周 荻(1 －86)

航空中的力反饋技術(shù)*…………………………………………………………………潘 祥 葉永強(qiáng)(4 －84)

宇宙空間電磁波傳播 ……………………………………………………………………………白臨武(4 －91)

國外光學(xué)捷聯(lián)慣導(dǎo)系統(tǒng)的技術(shù)現(xiàn)狀和捷聯(lián)慣導(dǎo)發(fā)展趨勢(shì) …………………………劉智平 韓宗虎(5 －94)

《AEROSPACE CONTROL》

CLASSIFICATION CONTENTS(2012)

Modern Control Theory and Its Application

The Neural Network Expert System Applied to Power System Diagnosis ……AN Ruoming WANG Jun(3 －88)

Research of Fractional-Order Controller Realization ……………………KUANG Yu WU Run LI Yan(4 － 3)

The Controller Design by Using RBF Neural Network and A Luenberger form Observer……………………………………………………WANG Linxu ZHANG Shengxiu CAO Lijia FENG Fuqin ZHAO Wei(5 － 3)

Guidance and Control Technology of Missile and Launch Vehicle

The Robust Filter Design for the Guidance Signal of Wide-band Passive Radar Guided Weapon………………………………………………………………………………………CHENG Xuemei YANG Junpeng(1 － 3)

A Close-Loop Guidance Method Based on Velocity Dip Angle……………………………………………………………………………………………………………………MA Ruiping XIAO Fan ZHANG Tao(1 － 6)

The Research of SAR Image Match Guide Method Based on SIFT…………………………………………………………………………………………………………………TANG Bo ZHANG Hui LIU Yan(1 －10)

A Study on the Grid Ionospheric Delay Algorithm in Beidou……………………………………………………………………………………………………………ZHAN Xianlong LIU Ruihua YANG Zhaoning(1 －15)

The Application of Fuzzy Control Method to the Disturbing Gravitation Calculation ………WANG Jiyang(1 －20)

The Multivariable Decoupling Control Based on H-Matrices and QFT for SRLV……………………………………………………………………………………………ZHAO Zhifang XIAO Lihong NI Shaobo(2 － 3)

The Project Design of Terminal Guidance System for Cruise Vehicle Based on Integrating of Trajectory and Guidance………………………MU Yuqiang WANG Danye SUN Xiaosong HUANG Xingli CHEN Xinmin(2 － 7)

Attitude Control for Launchers Based on Robust State Observers…………………………………………………………………………………………………………………ZHOU Jun SHUI Zunshi GE Zhilei(2 －11)

The Study of Grey Analytic Hierarchy Process in the Survivability Application of Missile Weapon System…………………………………………………………………………………………QIU Lingcun HUI Yi(2 －17)

An Improved ECS Algorithm for SAR with Sub-Aperture Data ……YANG Libo LU Heping GAO Lei(2 －22)

The New Algorithm for Strap-down Inertial Navigation System……………………………………………………………………………………………………………………WANG Weipeng YANG Bo LI Fang(3 － 3)

The Research on Stability Analysis of Attitude Control System in the Case of Iterative Guidance……………………………………………………………………………………………WANH Hui ZHANG Yu(3 － 7)

Tracking of Maneuvering Target Based on Extended Kalman Filter …………ZHANG Rui SHI Linan(3 －12)

The Dynamic Inverse Method of Altitude Control for Hypersonic Vehicle …………………WANG Jian(3 －19)

The Moving Mass Roll Control Method Based on Asymmetric Reentry Vehicle………………………………………………………………………………………………………………………LI Zixing LI Gaofeng(3 －23)

Research on Evaluation Method of Guidance and Control Performance for Hypersonic Vehicle………………………………………………………………………………………………………………MA Weihua(4 － 7)

Design of Auto-Recovery System for SUAV in Simple Sensor Combination ……………WANG Hangyu(4 －13)

Trajectory Optimization of Solid Launch Vehicle Based on Hp-Adaptive Pseudospectral Method………………………………………………………………………………………………HONG Bei XIN Wanqing(4 －18)

The Application Analysis of Fiber Channel in Space Transportation System……………………………………………………………………………………………JIANG Yunqiu ZHANG Wei JIANG Penglong(4 －23)

The Dynamic Inversion PID Controller Design of BTT Missile…………………………………………………………………………………………………………………ZHANG Weigang LEI Humin LIU Jun(4 －27)

The Terminal Sliding Mode Control System Design for Hypersonic Flight Vehicle…………………………………………………………………………………………………WANG Peng LIU Luhua WU Jie(5 － 9)

The Design of Aerospace Plane Guidance Navigation and Control System……………………………………………………………………………………………………CHAO Tao WANG Songyan YANG Ming(5 －15)

The Effect of Gyro Random Walk during the Process of Initial Alignment of Missile…………………………………………………………………………………………………………YANG Junfeng SI Wenjie(5 －21)

The Analysis on the Networked Operational Patterns of Surface-Based Air Defense Missile System………………………………………………………………………………………………WANG Xi LI Jianxun(5 －25)

The Guidance Method on Midcourse Orbit Transfer Based on Improved Velocity Augmentation……………………………………ZHANG Jun DONG Wenjie ZI Naiquan LI Gang LIN Jinyong LI Shuangxi(5 －30)

A Method of On-line Wind Identification in the Field of Guided Aerocraft…………………………………………………………………………………………………………………SUN You YANG Guanghui(6 － 3)

The Research and Application of Re-entry Aerocraft Departure Susceptibility Criteria………………………………………………………………………………………CAO Yuteng WANG Xiaodong NI Shaobo(6 － 7)

The Control-Oriented Design and Analysis for Morphing Wave-rider……………………………………………………………………………………………………………DENG Jun LIU Yanbin ZHANG Yong(6 －13)

The Research on Reconfigurable Control Method for Certain UCA Control Surface Fault…………………………………………………………………………………………………ZHENG Yousheng JIANG Wei(6 －20)

Guidance Navigation and Control Technology of Spacecraft

A Novel Communication and Monitoring System for Emergency Based on Aerostat………………………………………………………………………………………………………FEI Dongnian ZHAO Panfeng(1 －23)

The Study of the Flare-Landing Performance and Control of Parafoil System…………………………………………………………………………………………………………………ZHANG Xinghui ZHU Erlin(1 －29)

The Capture of Grazing Star Based on the Modified Triangle Identification Algorithm…………………………………………………………………………………………………LI Minjun YANG Bo HU Jing(1 －33)

The Motion Planning for Free Flying Space Manipulator Based on Genetic Algorithm……………………………………………………………………………………………………………LI Yan CAI Yuanwen(1 －40)

The Rapid Optimization of Entry Trajectory for Suborbital Launch Vehicle ………………WANG Wenhu(2 －28)

The Generation of Three-dimensional Constrained Entry Trajectories for Hypersonic Vehicle Based on the Gauss Pseudospectral Method …………………………………………………………YAO Yinwei LI Huabin(2 －33)

The Research on the Uncertainty of Pressure Center for Moving Mass Actuated Vehicle………………………………………………………………………………WEI Pengxin GAO Changsheng JING Wuxing(2 －39)

A Novel Method of Locating GEO Objects with Space-Based Optical Short Arcs Observation and the Geometric of Precision for Initial Orbit Determination ……………………………WANG Xueying LI Jun AN Wei(2 －46)

The Study on Decision-making of the Maneuver in Satellite Orbits Based on Non-Keplerian…………………………………………………………………………………ZHANG Tuo GAO Xiaoguang FAN Hao(2 －51)

Transfer Trajectory Design of Interplanetary Multiple Objects Encounter Based on the Gravity-Assisted Technology……………………………………………………………………………………………HU Qinglong(2 －57)

The Navigation and Orbit Control of Kuafu-A Satellite Based on XNAV………………………………………………………………………………………ZHAO Luhua FEI Baojun XIAO Yu YAO Guozheng(3 －29)

The Fault Diagnosis of Spacecraft Attitude Control Flywheel Based on Extended Kalman Filter………………………………………………………………………………………………WU Hongfang WANG Zhi(3 －34)

Fault-tolerant Control Under Constrained Input for Flexible Satellite Attitude Control System during Orbit Control…………………………………………………………FU Yanping CHENG Yuehua JIANG Bin(3 －38)

The Attitude Control Law Design Based on Qausi-Euler-Angle Scheme in the Upper Stage………………………………………………………………………………………XIA Xiwang LIU Hanbing DU Han(3 －45)

Identification of Inertia Properties of Space Robot Based on Wheel Control………………………………………………………………………………………………WANG Chao DU Xiaoping GAO Yongming(3 －51)

Error Analysis and Observation Data Simulation for Geosynchronous Belt SBV Surveillance System……………………………………………………………………………TANG Yi WU Meiping FU Xiaofeng(3 －56)

Research on Initial Values of Newton Iterative Guidance for Aerospace Vehicles…………………………………………………………………………ZHU Jianwen LIU Luhua TANG Guojian XU Mingliang(3 －61)

An Approach of Attitude Estimation by Using Vision-Aided IMU for Mars Rover ………………LOU Lu(4 －32)

The Recursive Linear Attitude Estimator for Spacecraft Based on Rodriguez Parameters………………………………………………LUO Yuyang GONG Deren CHEN Junli DUAN Dengping SHAO Xiaowei(4 －37)

The Unscented Kalman Filter Estimation of Spacecraft Formation Flying Based on Improved Lawden Equation……………………………………………WEN Zhou SHAO Xiaowei TAO Jiuliang GONG Deren(4 －42)

The Key Problems of Describing Rigid-Body Attitude by Using Quaternion …………………FAN Kuiwu(4 －49)

The Design and Optimization of the Parking Orbit of Space Multiple-targets Rendezvous or Interception Platform……………………………………………………………………………WU Beibei HUANG Hai(4 －54)

A Novel Relative Navigation Method Using Angles Observations from Vision Sensor………………………………………………………………………………LIU Tao HU Haixia WANG Ying WANG Dayi(5 －35)

Satellite Safe Attitude Control Scheme Without Gyros and Thrusters ………LI Mingqun ZONG Hong(5 －42)

A Cascaded Thruster Allocation Algorithm Based on Optimal Thruster Cone……………………………………………………………………………………………………………………ZHU Mengping XU Shijie(5 －48)

The Modified Quasi-Euler-Angles-Based Attitude Control Law for Spacecraft……………………………………………………………………………………………………XIA Xiwang LIU Hanbing DU Han(5 －55)

RBFNN Siding Mode Attitude Control Method of Spacecraft with Mobile Bodies…………………………………………………………………………………………DU Xiaoping HAO Gangtao GAO Yongming(5 －61)

The System Design of the Space-Based Visible Surveillance System for GEO Belt Observation……………………………………………………………………………………………………DIAO Huafei LI Zhi(5 －66)

Moon-Earth Return Trajectory Precise Design of Fast Differential Correction Based on B-Plane Parameters of Hyper bola ………………………………………………………………………………ZHOU Liang HU Jun(6 －27)

The Dynamic Surface Backstepping Control Based on State Observer for a Hypersonic Vehicle………………………………………………………WANG Shoubin WANG Xinmin YAO Congchao XIE Rong(6 －32)

Analysis of Factor of Integrity Parameter SISMA in Galileo System…………………………………………………………………………………………………………ZHANG Xuehui BEI Chao WANG Fang(6 －38)

Research on Closest-Aproach of Footprint and Coverage for Reentry Vehicle……………………………………………………………………………………………………FENG Biming NIE Wansheng LI Ke(6 －43)

Robust H∞Control of a Class Sample-Data System for Satellite Attitude Control with Structured Uncertainty………………………………………………………………LIU Shanwu ZHANG Rui ZHANG Jing(6 －50)

The Fault Tolerant Tracking Control for Near Space Vehicle Based on Model Predictive Control………………………………………………………………………………………HE Na JIANG Bin QI Ruiyun(6 －54)

Computer Technology and Simulation Technology

The Simulation and Experimental Study on the EMC of the PCB for the Electronic Controller……………………………………………………………………ZHANG Yin YE Zhifeng XU Jianguo CAO Zhijie(1 －49)

The Validation of CMMS Dynamic Behavior Based on UML ………………GAO Jianglin WU Xiaoyan(1 －54)

The Design and Implementation of 1553B Multifunctional RT IP Core……………………………………………………………………………………………………………LI Hui ZHANG Jingbo ZHANG Lei(1 －59)

A Filter Algorithm of Multi-Sensor Target Tracking Based on Out of Sequence Measurement………………………………………………………………………………………………………………JIANG Chunlei(2 －63)

The Simulink Simulation of the INS on the Near Space Hypersonic Vehicle………………………PENG Hui XIONG Zhi LIU Jianye WANG Rong(2 －69)

The Simulation of Lifting Reentry Dynamic Properties Based on Orbiter Simulator……………………………………………………………………………………DONG Yanfei TAN Zhaosheng CHEN Xiaofei(2 －75)

The Analysis and Simulation on File Delivery Time of Deferred NAK in CFDP Protocol…………………………………………………………………………………………………………………LIANG Yingchun(2 －80)

The Design of Embedded Software Based on MiniGUI and Multitask ………JIN Xiaoyuan MA Yingjin(3 －65)

The Research on the Method of Software Testing Based on MC/DC …………YUE Hai REN Huimin(3 －69)

Grid Mapping Method of Multi-physics Coupled Modeling for Near Space Vehicle……………………………………………………………………LIU Jing WANG Ling HU Dongfei TIE Ming WU Xusheng(3 －73)

The Research on Meta-Synthesis Technology of Flying Control System in the Space and Ground Information Integra tion …………………DONG Wenjie ZHANG Chunxia ZI Naiquan ZHOU Chunmei ZHANG Jun(3 －78)

An Improved Proposal to Deferred NAK Mode in CFDP Protocol ……………………LIANG Yingchun(4 －60)

The Study of Automation of Infrared Ray Seeker Simulation System …QIAO Xiaohui DONG Yunfeng(4 －64)

The Design and Research of the Test Data Analysis and Management System for the Aerospace Product……………………………………………………………………………………WANG Xiaobin GU Wei(4 －68)

The Fire Distribution for Shore-Based Missiles Based on Improved Particle Swarm Optimization…………………………………………………WANG Guangyuan JI Wanfeng SUN Junzheng ZHANG Yaoqing(5 －71)

An Approach to Modify System Architecture and Maintain Information Consistency Based on DoDAF……………………………………………………………YAN Liang DU Xiaoping ZHAO Jiguang LI Yuan(6 －59)

The Validation and Analysis of Double Retransmission Scheme to Deferred NAK in CFDP Protocol…………………………………………………………………………………………………………WU Haitao(6 －65)

Test Launch and Control Technology

The Design of Large-Capacity Integrated Data Acquisition and Testing System of Rocket Based on CPCI Bus…………………………………………………………………………………ZHAO Na ZHANG Lei(1 －66)

Range Application Research of Mixed-bus Test Technology ……………………………GAO Zhengmin(1 －71)

The Design and Research of Fault Injection on 1553B Bus …………………LIAN Meng LI Xuefeng(2 －84)

The Design of PLC Based on Hardware Logic Solver and Its Application in Test and Launch Control System…………………………………………………………………………SONG Zhengyu LIU Liangliang(5 －78)

The Design and Implementation of Monitoring and Management System for the Network of Test and Launch Control System ………………………………………………………CHEN Fang TIAN Jianyu SUN Zhaoniu(5 －83)

The Application of All-Digital Simulation Test Environment in Embedded Software Test……………………………………………………………………………………………GUO Hua WU Zhanfeng WU Jin(6 －70)

The Research of Object-Oriented Detection Method Based on Technique of Configurable Target Feature Model……………………………………………………………CAI Huajie GONG Junbin TIAN Jinwen(6 －73)

Reliability Safety and Maintainability

Research on Risk Evaluation in Filling System of Space Launch Site……………………………………………………………………………………………………SONG Jianjun DU Xiaoping ZHAO Jiguang(1 －76)

The Redundant Technology Based on Bridge-Control-Double-Networks for Reusable Launch Vehicle Control System…………………………………………………………………QI Guangping SUN Peng LI Guangjie (2 －89)

The Method of Reliability Assessment for Electronic Products Based on Multiple Similar Samples……………………………………ZHANG Libo WANG Hongli CHEN Cong CUI Xiangxiang ZHU Tianwen(3 －84)

Research of Failure Detection and Data Accommodation Algorithm of Sensor for Liquid-Propellant Rocket Engine………………………………………………………HUANG Qiang LIU Honggang WU Jianjun(4 －73)

The Reliability Evaluation for Aerospace Power Supply in a New Type of Censoring Test………………………………………………………………………………………………………SUN Tianyu SHI Yimin(5 －88)

Security in the Process of a Certain Type of Missile Fault Diagnosis Expert System for Shallow Layer…………………………………………………………………………………………………ZHANG Jiazhan(6 －78)

A Novel Approach to Discriminate the Overlap Region of Multi-class Classification SVDD and Fault Diagnosis Ap plication …………………………………………………………………………CAI Jinyan DU Minjie(6 －83)

Photoelectric and Electromechanical Integration Technology

The Analysis and Simulation of Attitude Motion for a De-orbit Rocket Based on Fluent Flow Field Calculation…………………………………………………………………………………GUAN Hong XU Shijie(3 －93)

The Study on Structural Sketch Fast Design System of Engineering Products Based on Original Pen Input Pattern……………………………………………………………………………………………ZI Naiquan(4 －77)

The Analysis of Detection Performance for STSS IR Sensor …………………SHE Eryong PENG Hao(4 －81)

Research on the Design of Mass Storage Information Recorder with High Reliability……………………………………………………………………………………………………WU Ruifeng ZHANG Hongbo(6 －89)

Summary

The History of Inertia Guidance Electromechanical Method for Ballistic Aircraft………………………………………………………………………………………………………………FAN Kuiwu CUI Xinshui(1 －81)

A Survey of Terminal Guidance Law ………………………SUN Sheng ZHANG Huaming ZHOU Di(1 －86)

Force Feedback Technologies in Aviation …………………………………PAN Xiang YE Yongqiang(4 －84)

The Electromagnetic Wace Propagation of the Observable Universe …………………………BAI Linwu(4 －91)

The Technical Situation and Development Tendency of Foreign Optical Strapdown Inertial Navigation System………………………………………………………………………………LIU Zhiping HAN Zonghu(5 －94)