?

《空間控制技術(shù)與應(yīng)用》2015年總目次

第1期

專家約稿

低功率氮?dú)浠旌衔镫娀〖訜岚l(fā)動(dòng)機(jī)模擬研究

魏延明，耿金越，何青松，王海興(1)

學(xué)術(shù)研究

撓性航天器退步自適應(yīng)姿態(tài)機(jī)動(dòng)及主動(dòng)振動(dòng)控制

劉 敏，楊 軍，李學(xué)林，徐世杰(9)

基于描述函數(shù)法的相平面噴氣姿態(tài)控制的穩(wěn)定性分析

張國琪，劉 潔，董文強(qiáng)，何英姿(15)

超靜敏捷衛(wèi)星隔振與控制的動(dòng)力學(xué)耦合及協(xié)同設(shè)計(jì)方法

關(guān) 新，陳守磊，崔穎慧，湯 亮，鄭鋼鐵(21)

一種用于納型衛(wèi)星在軌分離釋放裝置的設(shè)計(jì)

周 偉,楊 萱,楊 華(26)

技術(shù)交流

電推進(jìn)靜止軌道轉(zhuǎn)移與空間環(huán)境分析

馬 雪，韓 冬，湯 亮(31)

一體化太陽敏感器熱分析與驗(yàn)證方法

莫亞男，張 寧，劉庭偉，崔 堅(jiān)，陳 然，趙 媛(36)

預(yù)載對(duì)飛輪用軸承組件振動(dòng)特性的影響研究

王 虹，卿 濤，周 剛，周寧寧(41)

陰影區(qū)較遠(yuǎn)距離手動(dòng)交會(huì)對(duì)接目標(biāo)識(shí)別方法

高 偉，任 焜，劉宗玉，李志宇，王 敏(46)

BIT技術(shù)在星載電子設(shè)備的應(yīng)用

蘭 超，王婧瓊(50)

DC/DC變換器中的瞬態(tài)特性分析

劉艷麗，井元良，柳新軍(55)

星敏感器調(diào)焦方法研究

劉 達(dá)，鐘紅軍，李春江，盧 欣(59)

第2期

專家約稿

資源三號(hào)衛(wèi)星控制系統(tǒng)概述及在軌驗(yàn)證

王淑一，劉 祥，陳 超(1)

學(xué)術(shù)研究

大橢圓軌道衛(wèi)星交會(huì)高軌目標(biāo)的高精度視線跟蹤控制

徐 帷，武海雷，盧 山，劉付成(6)

遙感衛(wèi)星動(dòng)力學(xué)頻譜規(guī)劃

呂 旺，向明江，沈毅力，曾 擎(12)

應(yīng)用于MEMS_SINS/GPS組合導(dǎo)航系統(tǒng)的H∞容錯(cuò)濾波算法

石 靜，楊建華，劉慧英(18)

基于Krylov子空間法的柔性航天器降階研究

李 莉，劉鑄永，洪嘉振(24)

技術(shù)交流

空間機(jī)器人協(xié)調(diào)控制全物理仿真設(shè)計(jì)與驗(yàn)證

王 穎，韓 冬，劉 濤(30)

一種地面模擬太陽電池陣開關(guān)分流方法研究

張 猛，于國慶，劉繼奎，崔赪旻，王友平(36)

一種一階延遲慣性環(huán)節(jié)溫控系統(tǒng)優(yōu)化設(shè)計(jì)方法

馮士偉，李 勇，武志忠，張沛勇(41)

控制力矩陀螺力學(xué)試驗(yàn)后的微振動(dòng)特性變化

王曉偉，翟百臣，羅睿智，關(guān) 新(46)

CAN總線并發(fā)通信時(shí)下位機(jī)應(yīng)用軟件設(shè)計(jì)

謝曉兵，董 筠，周新發(fā)，李 鶴(51)

面向軟件源程序的模型檢驗(yàn)技術(shù)

李聲濤，陳 睿，顧 斌(57)

第3期

專家約稿

航天器交會(huì)對(duì)接中液體燃料晃動(dòng)等效模型研究

王天舒，苗 楠，李俊峰(1)

學(xué)術(shù)研究

基于幾何特征的非合作目標(biāo)相對(duì)位置和姿態(tài)估計(jì)

李宜鵬,趙春暉,王 立(8)

航天器軌道交會(huì)迭代制導(dǎo)算法

李學(xué)鋒，李超兵，王志剛(14)

RTS平滑濾波在事后姿態(tài)確定中的應(yīng)用

鮑雨波,宗 紅，張春青(18)

基于星間測距的編隊(duì)衛(wèi)星一致性導(dǎo)航算法

張 艾，李 勇(23)

一種帶大撓性附件衛(wèi)星的低階魯棒控制方法

胡 萌，湯 亮(28)

技術(shù)交流

資源三號(hào)衛(wèi)星高精度控制分系統(tǒng)地面試驗(yàn)驗(yàn)證系統(tǒng)

丁建釗，劉 祥，劉 彤，傅秀濤，陳琳娜，王晉鵬，王淑一，陳 超(33)

基于視線矢量測量的火星接近段自主導(dǎo)航算法

唐青原，王曉磊(38)

星間測距對(duì)小衛(wèi)星編隊(duì)相對(duì)軌道狀態(tài)的修正

張曉磊，鄭建華，高 東，錢 航(42)

一種面向星載計(jì)算機(jī)的功能級(jí)功耗估計(jì)方法

姜 宏，楊孟飛，于廣良，魏夢捷(48)

永磁無刷直流陀螺電機(jī)鎖相穩(wěn)速控制研究

朱夢如，陳小娟，馬官營(53)

基于ZigBee的星內(nèi)無線通信網(wǎng)絡(luò)研究與設(shè)計(jì)

孫赫婕，華更新，吳 軍，梁潔玫(58)

第4期

專家約稿

基于云計(jì)算的航天器控制系統(tǒng)自組織體系結(jié)構(gòu)

王 磊，梁 俊，劉淑芬，劉鴻瑾(1)

學(xué)術(shù)研究

自適應(yīng)混合信息濾波算法及其在相對(duì)導(dǎo)航中的應(yīng)用

李明明,王 丹(7)

剛體航天器大角度姿態(tài)機(jī)動(dòng)控制算法

李偉明，申景詩，康旭輝(14)

大偏心率軌道星上快速計(jì)算方法

胡少春，黃翔宇(20)

一種帆板驅(qū)動(dòng)機(jī)構(gòu)用永磁同步電機(jī)微步控制方法

郭超勇，張 猛，梁驕雁，王友平，于國慶(24)

技術(shù)交流

空間光通信激光相干組束技術(shù)研究

李沼云，覃 波，付 益，張 昕，覃良標(biāo)，黃 芳，張明宇(30)

小型一體化編碼式太陽敏感器信號(hào)處理技術(shù)

莫亞男，趙 媛，劉 鑫(36)

基于回歸分析的飛輪泄漏預(yù)測模型構(gòu)建研究

張紹衛(wèi)，夏 旎，馮洪偉，齊 明，楊 磊(40)

基于Eclipse的航天嵌入式軟件集成開發(fā)環(huán)境設(shè)計(jì)與實(shí)現(xiàn)

郝王松，彭 飛，喬 磊，吳一帆，劉 波，吳 軍(44)

一種用數(shù)字集成電路FPGA實(shí)現(xiàn)的偽速率調(diào)制器

彭 坤(49)

航天嵌入式軟件浮點(diǎn)運(yùn)算誤差分析與控制

傅秀濤，綦艷霞，陳朝暉(54)

航天器C51語言軟件中斷資源沖突分析方法

侯成杰(58)

第5期

專家約稿

基于經(jīng)驗(yàn)學(xué)習(xí)的空間機(jī)器人精細(xì)抓捕方法

孫富春，劉春芳(1)

學(xué)術(shù)研究

基于雙目視覺的非合作目標(biāo)逼近控制系統(tǒng)設(shè)計(jì)與仿真

郭延寧，韓 旭，郭增千，張 瑤，馬廣富(6)

串并混聯(lián)空間機(jī)械臂全自由度軌跡規(guī)劃算法

王 勇，唐 強(qiáng)，徐拴鋒，朱志斌，何英姿，魏春嶺(13)

基于Smith預(yù)測控制的空間機(jī)器人遙操作研究

劉冬雨，劉 宏，黃龍飛(19)

一種基于串聯(lián)解耦的陀螺飛輪擺角控制方法

章曉明，李海軍(23)

月球上升段PEG參數(shù)自適應(yīng)估計(jì)

王志文，張洪華(28)

技術(shù)交流

太陽帆板驅(qū)動(dòng)機(jī)構(gòu)微振動(dòng)建模及摩擦補(bǔ)償研究

張可墨,張 強(qiáng),程俊波(33)

一種二浮陀螺儀熱仿真分析及試驗(yàn)驗(yàn)證

張沛勇，孫 麗，武麗花(39)

基于多面體模型的數(shù)據(jù)依賴分析方法

李 川，陳朝暉(43)

基于變延時(shí)自換向保護(hù)的大型磁力矩器控制電路設(shè)計(jì)

徐勤超(48)

執(zhí)行機(jī)構(gòu)驅(qū)動(dòng)單元軟件的設(shè)計(jì)與分析

趙性頌，董曉剛，楊曉龍，牛和明，高 猛(53)

CAST968平臺(tái)小衛(wèi)星在軌故障分析和建議

呂高見(57)

第6期

專家約稿

基于PSF相關(guān)的星點(diǎn)定位算法

郝云彩，賈瑞明，馬曉蕾(1)

學(xué)術(shù)研究

基于自適應(yīng)濾波的脈沖星導(dǎo)航方法研究

褚永輝，李茂登，黃翔宇，王大軼(8)

非合作機(jī)動(dòng)目標(biāo)交會(huì)的相對(duì)位置控制

徐李佳，胡 勇(13)

基于混合執(zhí)行機(jī)構(gòu)的敏捷衛(wèi)星姿態(tài)機(jī)動(dòng)控制

王煥杰，金 磊，賈英宏(19)

圓錐掃描地球敏感器前置放大電路穩(wěn)定性分析

涂智軍，張 燚，梅志武(25)

多剛體衛(wèi)星轉(zhuǎn)動(dòng)慣量在軌辨識(shí)

許 瑩，呂 旺，李云端，張大偉(31)

技術(shù)交流

旋轉(zhuǎn)盤片式空間相機(jī)快門的設(shè)計(jì)與研制

張 鑫，周惠坤，李保權(quán)，白超平，史春艷(37)

基于迭代學(xué)習(xí)算法的控制力矩陀螺框架擾動(dòng)抑制策略研究

來 林，周大寧，武登云(42)

基于BP神經(jīng)網(wǎng)絡(luò)的高精度陀螺恒流源補(bǔ)償方法

王健康，王雪濤，嚴(yán) 嶸，陳 斌，王春元(47)

壓力對(duì)離心式噴注器霧化特性影響的試驗(yàn)研究

石召新，毛曉芳(52)

一種星載計(jì)算機(jī)自穩(wěn)定容錯(cuò)時(shí)間同步算法

馮 丹，江耿豐，劉 波，衣學(xué)慧，劉超偉(58)

Aerospace Control and Application Contents (2015)

No.1

Simulation Analysis on the Low-Power Nitrogen/Hydrogen Mixtures Arcjets

WEIYanming，GENGJinyue,HEQingsong,WANGHaixing(1)

Backstepping Adaptive Attitude Maneuver and Active Vibration Control of Flexible Spacecraft

LIUMin,YANGJun,LIXuelin,XUShijie(9)

Stability Analysis of Phase-Plane Jet Attitudes Control System Using the Describing Function Method

ZHANGGuoqi,LIUJie,DONGWenqiang,HEYingzi(15)

Dynamics Coupling and Integrated Design in Vibration Isolation and Attitude Control Design of Ultra-Quiet

Agile Satellites

GUANXin,CHENShoulei,CUIYinghui,TANGLiang,ZHENGGangtie(21)

Design of System for Nanosatellite on-Orbit Release and Separation

ZHOUWei,YANGXuan,YANGHua(26)

On the Electric-Propulsion-Based Geostationary Transfer and Space Environmental Analysis

MAXue,HANDong,TANGLiang(31)

Thermal Analysis and Verification for an Integrative Sun Sensor

MOYanan,ZHANGNing，LIUTingwei，CUIJian,CHENRan,ZHAOYuan(36)

Effects of Preload on the Micro-Vibration Properties of Bearing Assemblies in FlyWheels

WANGHong，QINGTao，ZHOUGang，ZHOUNingning(41)

The Object Identification Methods for Manual Controlled Rendezvous and Docking in Shadow and

Remoter Region

GAOWei,RENKun,LIUZongyu,LIZhiyu,WANGMin(46)

Applications of BIT Technology in Satellite Electronic Equipment

LANChao，WANGJingqiong(50)

The Analysis of DC/DC Convertor’s Transient Responses

LIUYanli,JINGYuanliang,LIUXinjun(55)

Focusing Methods of Star Sensor

LIUDa，ZHONGHongjun，LIChunjiang，LUXin(59)

No.2

Overview of Control System and on-Orbit Test for ZY-3 Satellite

WANGShuyi,LIUXiang，CHENChao(1)

A High Precision Attitude Tracking Control Method for Highly Eccentric Orbit Spacecraft Rendezvous

with a HEO Target

XUWei，WUHailei，LUShan，LIUFucheng(6)

Dynamic Frequency Spectrum Planning of Remote Sensing Satellite

LYUWang,XIANGMingjiang,SHENYili,ZENGQing(12)

An H∞Fault-Tolerant Filter and Its Application in MEMS_SINS/GPS Integrated Navigation Systems

SHIJing,YANGJianhua,LIUHuiying(18)

Model Order Reduction of Flexible Spacecraft Based on Krylov Subspace Method

LILi,LIUZhuyong,HONGJiazhen(24)

The Design and Verification of Experiment System for Cooperative Control of Space Robot

WANGYing,HANDong,LIUTao(30)

Switching Shunt Simulation Mehtod in Ground Testing of Solar Array

ZHANGMeng，YUGuoqing，LIUJikui，CUIChengmin，WANGYouping(36)

An Optimization Design Method for Temperature Control System with a First-Order Delay Inertial Link

FENGShiwei，LIYong，WUZhizhong，ZHANGPeiyong(41)

Microvibration Characteristics Variation of Control Moment Gyroscope Subjected to Mechanical Tests

WANGXiaowei,ZHAIBaichen,LUORuizhi,GUANXin(46)

Design for Communication of CAN Bus of Lower Application Software in Concurrent Communication

XIEXiaobing,DONGJun,ZHOUXinfa,LIHe(51)

Source-Oriented Software Model Checking Technology

LIShengtao,CHENRui,GUBin(57)

No.3

Liquid Sloshing Equivalent Mechanical Model during Rendezvous and Docking

WANGTianshu,MIAONan,LIJunfeng(1)

Relative Position and Attitude Estimation of Non-Cooperative Spacecraft Based on Geometric Features

LIYipeng,ZHAOChunhui,WANGLi(8)

Iterative Guidance Algorithm for Spacecraft Orbit Rendezvous

LIXuefeng,LIChaobing,WANGZhigang(14)

The Application of RTS Smooth Filter Algorithm in Post Attitude Determination

BAOYubo,ZONGHong,ZHANGChunqing(18)

A Consensus Navigation Algorithm for Spacecraft Formation Based on Distance Ranging

ZHANGAi,LIYong(23)

Low-Order Robust Control for Satellite with Large Flexible Appendages

HUMeng,TANGLiang(28)

A Ground Testing Verification System for the High Precision Control System of the ZY-3 Satellite

DINGJianzhao,LIUXiang,LIUTong,FUXiutao,CHENLinna,

WANGJinpeng,WANGShuyi,CHENChao(33)

Autonomous Navigation Algorithm during the Phase of Approaching Mars Based on Light-of-Sight

Vector Measurement

TANGQingyuan,WANGXiaolei(38)

Correction of the Relative Orbit States Based on Inter-Satellite Ranging for Micro-Satellites Formation

ZHANGXiaolei,ZHENGJianhua,GAODong,QianHang(42)

An Approach for Functional Level Power Estimation of On-Board Computer

JIANGHong,YANGMengfei,YUGuangliang,WEIMengjie(48)

Phase-Locked Loop Steady-Speed Control of Permanent Magnet Brushless DC Gyro Motor

ZHUMengru，CHENXiaojuan，MAGuanying(53)

Research and Design of ZigBee-Based Intra-Satellite Wireless Communication

SUNHejie，HUAGengxin，WUJun，LIANGJiemei(58)

No.4

The Cloud-Computing-Based Self-Organizing Architecture for Spacecraft Control System

WANGLei,LIANGJun，LIUShufen，LIUHongjin(1)

Adaptive Hybrid Information Filtering and Its Application in Relative Navigation

LIMingming，WANGDan(7)

Large Angle Attitude Maneuver Control Algorithm for Rigid Spacecraft

LIWeiming，SHENJingshi，KANGXuhui(14)

Fast on-Orbit Prediction Algorithm for High Eccentricity Orbit

HUShaochun，HUANGXiangyu(20)

A Permanent-Magnet Synchronous-Motor Micro-Step Control Method for Solar Array Drive Assembly

GUOChaoyong,ZHANGMeng,LIANGJiaoyan,WANGYouping,YUGuoqing(24)

On Laser Coherent Beams Combining Technology for Space Optical Communication

LIZhaoyun，QINBo，F(xiàn)UYi，ZHANGXin，QINLiangbiao，HUANGFang，ZHANGMingyu(30)

The Signal Processing Technique for Integrative Encoded Sun Sensor

MOYanan，ZHAOYuan，LIUXin(36)

A Model for Predicting Flywheel Leak Based on Linear Regression Analysis

ZHANGShaowei,XIANi,FENGHongwei,QIMing,YANGLei(40)

Design and Implementation of Embedded Integrated Development Environment for Spacecraft Software

Based on Eclipse

HAOWangsong,PENGFei,QIAOLei,WUYifan,LIUBo,WUJun(44)

One Kind of Pseudo-Rate Modulator Based on Digital Integrated FPGA

PENGKun(49)

Analysis and Control of Floating-Point Operational Errors from Space Embedded Software

FUXiutao，QIYanxia，CHENZhaohui(54)

Interrupt Resource Conflict Analysis for Spacecraft C51 Language Software

HOUChengjie(58)

No.5

Space Robot Precise Manipulation Based on Experience Learning

SUNFuchun，LIUChunfang(1)

Control System Design and Simulation of Binocular Vision-Based Non-Cooperative Target Proximity Mission

GUOYanning,HANXu,GUOZengqian,ZHANGYao,MAGuangfu(6)

Trajectory-Planning Algorithm for Series-Parallel Space Manipulator Based on the Full DOFs

WANGYong,TANGQiang,XUShuanfeng,ZHUZhibin,HEYingzi,WEIChunling(13)

Space Manipulator Based on Smith Predictive Control

LIUDongyu，LIUHong，HUANGLongfei(19)

A Control Method of Gyrowheel’s Swing Angle Based on Series Decoupling

ZHANGXiaoming，LIHaijun(23)

Adaptive Estimation of PEG Parameters During Lunar Ascent

WANGZhiwen，ZHANGHonghua(28)

Micro-Vibration Modeling of SADA and Friction Compensation for the Control of PMSM

ZHANGKemo,ZHANGQiang,CHENGJunbo(33)

Thermal Simulation Analysis and Experiment Verification for a Type of Floated Gyro

ZHANGPeiyong,SUNLi，WULihua(39)

Data-Dependence Analysis Method Based on Polyhedral Model

LIChuan,CHENZhaohui(43)

Design of Control Circuit of a Large Magnetic Torquer with Protection of Variable Reverse-Self Delay

XUQinchao(48)

Design and Analysis of ADU Software

ZHAOXingsong,DONGXiaogang,YANGXiaolong,NIUHeming,GAOMeng(53)

On-Orbit Failure Statistical Analysis and Suggestions for Small Satellites of CAST968 Platform

LVGaojian(57)

No.6

Star Locating Algorithm Based on PSF Correlation

HAOYuncai,JIARuimin,MAXiaolei(1)

Adaptive Filter of X-Ray Pulsar-Based Navigation

CHUYonghui,LIMaodeng,HUANGXiangyu,WANGDayi(8)

Control for Relative Position of Spacecraft Rendezvous with a Non-Cooperative Maneuver Target

XULijia,HUYong(13)

Agile Satellite Attitude Maneuver Control Using Hybrid Actuators

WANGHuanjie,JINLei,JIAYinghong(19)

Analysis on Preamplifier Circuit Stability of the Conical Scanning Earth Sensor

TUZhijun，ZHANGYi，MEIZhiwu(25)

Identification of Rotary Inertia for Multi-Body Satellite

XUYing,LVWang,LIYunduan,ZHANGDawei(31)

Design and Manufacture of Rotary-Disc Shutter of Space Imager

ZHANGXin，ZHOUHuikun,LIBaoquan,BAIChaoping，SHIChunyan(37)

Disturbance Torque Minimization Strategy for Control Moment Gyroscopes Based on Iterative

Learning Algorithm

LAILin，ZHOUDaning，WUDengyun(42)

The Design of Precise Gyro Constant-Current Source Based on BP Neural Network Compensation

WANGJiankang，WANGXuetao，YANRong,CHENBin，WANGChunyuan(47)

Experimental Investigations on Atomization Characteristics of Bi-Centrifugal Pressure Swirl Injector

SHIZhaoxin，MAOXiaofang(52)

A Self-Stabilization Fault-Tolerant Time-Synchronization Algorithm for an On-Board Computer

FENGDan,JIANGGengfeng,LIUBo,YIXuehui,LIUChaowei(58)