《空間控制技術(shù)與應(yīng)用》2018年總目次

第1期

長文

剛體衛(wèi)星相平面控制閉環(huán)系統(tǒng)穩(wěn)定性分析

陳志華，解永春(1)

論文與報(bào)告

姿態(tài)異常下的星體自旋角速度確定方法

雷擁軍，李明群(15)

基于奇異值分解的單框架變速控制力矩陀螺角動量管理方法

李 煥，黨慶慶，徐世杰(21)

基于降階ESO的微小型空地導(dǎo)彈改進(jìn)LQR滾轉(zhuǎn)控制

鐘高偉，陳東生，王明光(30)

有限時(shí)間收斂的阻力加速度跟蹤進(jìn)入制導(dǎo)律

嚴(yán) 晗，何英姿(38)

基于長方體禁飛區(qū)的安全繞飛軌跡設(shè)計(jì)

梁靜靜，解永春(45)

基于區(qū)域平均燃料消耗的推力器配置問題

王 敏，王思野(51)

空間機(jī)械臂間隙影響分析

張世俊(56)

天基通信與太空射電望遠(yuǎn)鏡功能一體系統(tǒng)

吳鵬飛，祖鳳丹，付培華，胡羽行，許雯雯，張嵐昕(62)

半球諧振陀螺零偏溫度漂移的自補(bǔ)償

劉吉利，李建朋，武志忠，李 愷(69)

熱容法測量推進(jìn)劑剩余量的地面試驗(yàn)

郭 蕾，李 永，焦 焱，唐 飛，宋 濤(74)

第2期

論文與報(bào)告

面向海洋機(jī)動目標(biāo)跟蹤監(jiān)視的衛(wèi)星重構(gòu)組網(wǎng)優(yōu)化與仿真

趙程亮，張占月，李志亮，劉 瑤(1)

月地轉(zhuǎn)移軌道中應(yīng)急調(diào)整異面著陸場的軌道控制及優(yōu)化方法

馮 飛，張雅聲，張安理(8)

小展弦比有限厚度舵面顫振特性分析

秦玉靈，李曉東，張 飛，李長春，宮曉春，高志勇(14)

軌控大干擾下的系統(tǒng)角動量管理

王淑一，雷擁軍，王新民，袁 軍(19)

一種基于模糊分割的黃金分割控制器設(shè)計(jì)及其應(yīng)用

馮佳佳，李宜鵬(25)

基于事件觸發(fā)的航天器變周期控制方法研究

孫 帥，王 磊,王志文(31)

適用于時(shí)變不確定系統(tǒng)的并行模型自適應(yīng)估計(jì)

熊 凱，魏春嶺，劉良棟(36)

基于近鄰保持嵌入的衛(wèi)星姿態(tài)控制系統(tǒng)微小故障檢測

劉 敏,陸寧云,肇 剛,姜 斌(42)

衛(wèi)星導(dǎo)航系統(tǒng)失效性能分析與重構(gòu)方法研究

趙 雙，張雅聲，戴樺宇，齊 躍(49)

新一代空間交會對接光學(xué)成像敏感器

劉啟海，龔德鑄，華寶成，鐘 俊，鄭 巖，趙春暉(56)

一種改進(jìn)的投影裝置標(biāo)定方法

孫秀清,張篤周,王 立,吳奮陟(62)

脈沖等離子體推力器放電電離二維PIC建模與仿真

劉 祺,楊 磊,黃玉平,鄭再平,趙 絮(67)

一種軟件脆弱性自動分析定位的方法

王同磊，陳朝暉(73)

第3期

論文與報(bào)告

帶柔性載荷超靜平臺的模型參數(shù)在軌辨識

齊田雨，湯 亮，張科備(1)

含有多級驅(qū)動機(jī)構(gòu)衛(wèi)星的多變量頻域穩(wěn)定性分析方法

劉 磊(7)

基于虛擬目標(biāo)的導(dǎo)彈越肩發(fā)射初制導(dǎo)軌跡優(yōu)化

金一歡,雷葉紅,馮 昊,彭繼平,田 野(15)

類IXV飛行器初期再入制導(dǎo)與姿態(tài)控制方法研究

黃盤興，何英姿，楊 鳴，郭敏文(22)

再入飛行器末端能量管理段縱向剖面優(yōu)化方法

龔宇蓮，陳上上(28)

一種地外天體路標(biāo)圖像的稀疏化表征方法

胡榮海，黃翔宇(36)

高精度星相機(jī)光學(xué)系統(tǒng)像質(zhì)評價(jià)及實(shí)現(xiàn)

賈永丹, 王偉之,孫 建,王 妍,宗云花,曹桂麗，康少英(43)

平面感應(yīng)式脈沖等離子體推力器高速脈沖氣體供給閥的試驗(yàn)驗(yàn)證

郭大偉，程謀森，李小康,車碧軒(50)

短文

GEO螺旋巡游軌道的相對運(yùn)動分析和螺旋環(huán)設(shè)計(jì)

鄭樂天，周海俊(56)

控制力矩陀螺框架諧波減速驅(qū)動系統(tǒng)建模與仿真

杜 航，李 剛，魯 明(60)

基于紅外波段船載星光定向儀白晝恒星探測技術(shù)

夏夢綺，盧 欣，張春明，孫大開(67)

著陸避障中雙目立體匹配方法與仿真

劉 洋,王 立,華寶成,李 濤(73)

第4期

學(xué)術(shù)研究

遍歷理論在航天動力學(xué)領(lǐng)域的應(yīng)用

萍鄉(xiāng)春鑼曲詞生動流暢、通俗易懂，演唱常用夸張手法。曲詞句數(shù)不拘，兩句一韻，有時(shí)四句、八句一韻，換韻靈活多樣，多為七字句。有時(shí)為了增加節(jié)奏的變化，字?jǐn)?shù)可多可少，采取戲曲的“垛板”演唱。這些音調(diào)與萍鄉(xiāng)方言的音調(diào)結(jié)合緊密，具有濃厚的地方特色。萍鄉(xiāng)春鑼的最大特征就是“見贊”。如：見人贊人、見物贊物、見事贊事。無論是男女老少、茶樓藥鋪還是多多少少的段子，演繹者總能充分“贊”的優(yōu)勢。

白 雪，徐 明，姚 闖(1)

基于導(dǎo)納控制的空間精細(xì)操作半物理仿真

鄭海潮,何 俊,陳龍海(8)

徑向共線多星庫侖編隊(duì)飛行構(gòu)型保持研究

孫云龍,袁長清,李政廣(16)

基于快速響應(yīng)的導(dǎo)航星座重構(gòu)構(gòu)型設(shè)計(jì)

趙 雙 ，張雅聲，戴樺宇(26)

掠入射聚焦型脈沖星探測器的能量響應(yīng)標(biāo)定

石永強(qiáng)，席同鑫，辛優(yōu)美，陳建武，鄧樓樓，呂政欣，梅志武(34)

一種空間軸承的自適應(yīng)共振解調(diào)故障診斷方法

劉紅星，卿 濤，王 虹，何 田，張韶華(40)

基于SpaceOS2的TCP/IP網(wǎng)絡(luò)協(xié)議棧移植

袁瑞成，劉 波，喬 磊，劉健培(46)

技術(shù)交流

關(guān)于干擾作用下航天器姿態(tài)飽和控制的結(jié)果

胡錦昌,張洪華,王澤國,陳上上(56)

應(yīng)用動態(tài)流量控制的天地網(wǎng)絡(luò)數(shù)據(jù)傳輸方法

楊佳欣 ,禹 航(61)

用戶星中繼終端天線螺旋掃描算法

李 榮，龐 潔，晁 寧(66)

一種新型雙環(huán)控制并聯(lián)均流穩(wěn)壓電路

蘇少侃，彭 勃，王立偉，鄭 煒，常 濤，陳明陽(72)

第5期

論文與報(bào)告

基于加速度反饋的兩桿柔性機(jī)械臂振動控制與實(shí)驗(yàn)研究

邱志成，李 城(1)

基于六維加速度傳感器的大型機(jī)械臂柔性關(guān)節(jié)振動抑制

倪風(fēng)雷，林鵬飛，鄒 添(7)

一種動態(tài)環(huán)境下空間機(jī)器人的快速路徑規(guī)劃方法

胡曉東，黃學(xué)祥，胡天健，王峰林，梁書立(14)

一種改進(jìn)的機(jī)械臂逆運(yùn)動學(xué)阻尼最小二乘算法

王云鵬，解永春(22)

對衛(wèi)星柔性對接補(bǔ)加一體化機(jī)構(gòu)建模與設(shè)計(jì)

黃劍斌，黃龍飛，韓 旭，蒙 波，李 志，王文龍，李 文(30)

空間機(jī)器人抓捕目標(biāo)碰撞后的復(fù)合體穩(wěn)定控制

韓 冬，黃攀峰，劉習(xí)堯(38)

不確定通訊下的異構(gòu)多智能體網(wǎng)絡(luò)魯棒編隊(duì)控制

劉 淼，李忠奎(47)

基于改進(jìn)蟻群算法的多機(jī)器人任務(wù)分配

秦新立，宗 群，李曉瑜，張博淵，張秀云(55)

短文

柔性空間機(jī)械臂在軌操作仿真與分析

黎 凱，張 堯，陳余軍(60)

一種基于控制參數(shù)化的雙連桿機(jī)械臂最優(yōu)PID參數(shù)整定方法

郭小龍，郭敏華，譚 元，曹函宇，佃松宜，李 彬(70)

拒絕服務(wù)攻擊下的Euler-Lagrange系統(tǒng)的安全控制

曹 然，程 龍(76)

一類微型撲翼飛行器的滑模自適應(yīng)姿態(tài)控制

李 航，何廣平，畢富國(81)

第6期

論文與報(bào)告

僅地心矢量測量的衛(wèi)星轉(zhuǎn)對地定向姿態(tài)控制方法

雷擁軍，魏春嶺，何英姿，劉 潔(1)

一種空間機(jī)械臂無視覺在軌柔順裝配方法

鄧 雅，劉維惠，李曉輝，文 聞(8)

反作用輪主被動隔振器的復(fù)合控制研究

李林峰，張激揚(yáng)，羅睿智(13)

一種適用于星載太陽翼的驅(qū)動控制器設(shè)計(jì)

李麗嬌,石 然,嚴(yán) 丹,馬吉雨,張 俊(22)

航天器太陽能板振動單演多尺度相位測量

鄭少杰，薛斌黨，張國琪(32)

一種適應(yīng)于大負(fù)載工況的高線性度數(shù)字化比例電磁閥

張 榛，汪旭東，王代華，梁 亮，潘 斌，張 良(39)

星敏感器用4T像素CMOS圖像傳感器總劑量效應(yīng)研究

曹中祥，鐘紅軍，張運(yùn)方，李全良(45)

高精度星敏感器遮光罩柔性支撐結(jié)構(gòu)設(shè)計(jì)與分析

劉 婧，余成武，鐘紅軍，隋 杰，武延鵬(51)

基于1553B總線的航天器系統(tǒng)時(shí)間同步設(shè)計(jì)方法

李經(jīng)松，陳朝暉，黨紀(jì)紅，李昊然，董曉剛，李曉鋒(56)

短文

基于參數(shù)類型和訪問序的數(shù)據(jù)沖突靜態(tài)分析方法

董 燕，黃 晨，王小麗，虞礪琨，于 倩(62)

一種“白黑白”盒混合型航天器軟件單元測試技術(shù)

鄭小萌,高 猛,滕俊元(69)

AerospaceControlandApplicationContents(2018)

No.1

Stability Analysis of the Closed-Loop System of a Phase-Plane Controlled Rigid Satellite

CHENZhihua,XIEYongchun(1)

Spinning Angle Velocity Determination for In-Orbit Satellites with Attitude Anomaly

LEIYongjun，LIMingqun(15)

An Angular Momentum Management Method of Variable Speed Control Moment Gyroscope

Based on Singular Value Decomposition

LIHuan,DANGQingqing,XUShijie(21)

Improved LQR Roll Control of Miniature Guided Missile Based on Reduce-Order ESO

ZHONGGaowei，CHENDongsheng，WANGMingguang(30)

Drag-Tracking Guidance for Entry Vehicles with Finite Time

YANHan,HEYingzi(38)

Design Method of Safe Fly-Around Trajectory Based on Rectangular Keep-Out-Zone

LIANGJingjing，XIEYongchun(45)

Thruster Configuration Problem Based on Regional Average Fuel Consumption

WANGMin,WANGSiye(51)

Locomotion Control of Quadruped Robot Based on MIMO Characteristic Model with Input Decoupling

ZHANGShijun(56)

Space-Based Communication and Radio Telescope Functions Integrated System

WUPengfei,ZUFengdan,FUPeihua,HuYuxing,XUWenwen,ZHANGLanxin(62)

Self-Compensation of Bias Temperature Drift in Hemispherical Resonator Gyro

LIUJili,LIJianpeng,WUZhizhong,LIKai(69)

Ground Test on Thermal Propellant Gauging System

…GUOLei,LIYong,JIAOYan,TANGFei,SONGTao(74)

No.2

Satellite Reconstruction Network Optimization and Simulation for Marine Maneuvering Target Tracking

and Surveillance

ZHAOChengliang，ZHANGZhanyue，LIZhiliang，LIUYao(1)

An Orbit Control and Optimization for Switching Landing Site in Emergency in Trans-Earth Trajectory

FENGFei，ZHANGYasheng，ZHANGAnli(8)

Flutter Characteristic Analysis of Finite Thickness Rudder Surface with Low Aspect-Ratio

QINYuling,LIXiaodong,ZHANGFei,LIChangchun,GONGXiaochun,GAOZhiyong(14)

Momentum Management for a Momentum Exchange Device System with Large Disturbance Torque in

Orbit Control Process

WANGShuyi，LEIYongjun，WANGXinmin，YUANJun(19)

Design and Application: A Golden Section Controller Based on Fuzzy Segmentation

FENGJiajia,LIYipeng(25)

Aperiodic Spacecraft Control Method：An Event Triggered Approach

SUNShuai,WANGLei,WANGZhiwen(31)

Parallel-Model Adaptive Estimation for Time-Varying Uncertain Systems

XIONGKai,WEIChunling,LIULiangdong(36)

Incipient Fault Detection Method of Satellite Attitude Control System Based on

Neighborhood Preserving Embedding

LIUMin，LUNingyun，ZHAOGang，JIANGBin(42)

Failure Performance and Reconstruction Method of Satellite Navigation System

ZHAOShuang,ZHANGYasheng,DAIHuayu，QIYue(49)

New Generation Camera-Type Rendezvous and Docking Sensor

LIUQihai,GONGDezhu,HUABaocheng,ZHONGJun,ZHENGYan,ZHAOChunhui(56)

An Improved Method of Projector Calibration

SUNXiuqing，ZHANGDuzhou，WANGLi，WUFenzhi(62)

Two-Dimensional Particle-in-Cell Modeling and Numerical Simulation on the Discharge and Ionization of

Pulsed Plasma Thruster

LIUQi,YANGLei,HUANGYuping,ZHENGZaiping,ZHAOXu(67)

A Method of Analyzing and Localizing Software Vulnerability Automatically

WANGTonglei,CHENZhaohui(73)

No.3

On-Orbit Parameter Identification of Ultra-Quiet Platform with Flexible Payloads

QITianyu,TANGLiang,ZHANGKebei(1)

Multi-Variable Frequency Domain Stability Analysis for Satellites with Multi-Stage Drive Mechanisms

LIULei(7)

Guidance Law Design for Air-to-Air Missile Over-the Shoulder Based on Virtual Target

JINYihuan,LEIYehong,FENGHao,PENGJiping,TIANYe(15)

Reentry Guidance and Control Method for Class-IXV Aircraft

HUANGPanxing,HEYingzi,YANGMing,GUOMinwen(22)

TAEM Vertical Profile Optimization Algorithm for Reentry Vehicle

GONGYulian,CHENShangshang(28)

A Sparse Descriptor for Landmarks of Extraterrestrial Celestial Bodies

HURonghai,HUANGXiangyu(36)

Evaluation and Implementation of Image Quality in High-Precision Star Camera Optical System

JIAYongdan,WANGWeizhi,SUNJian,WANGYan,ZONGYunhua,CAOGuili,KANGShaoying(43)

Experiment Validation of a Novel Fast Pulsed Gas Valve for Inductive Pulsed Plasma Thruster

GUODawei,CHENGMousen,LIXiaokang,CHEBixuan(50)

Relative Motion Analysis and Helix Design of GEO Helix Tourist Orbit

ZHENGLetian,ZHOUHaijun(56)

Modeling and Simulation of CMG Gimbal System Based on Harmonic Gear

DUHang,LIGang,LUMING(60)

Daytime Star Detection Algorithm for an Infrared Shipboard Star Sensor

XIAMengqi,LUXin,ZHANGChunming,SUNDakai(67)

Stereo-Vision Matching-Techniques and Simulation for Hazard Detection During Planetary Landing

LIUYang,WANGLi,HUABaocheng,LITao(73)

No.4

The Application of Ergodic Theory in Astrodynamics

BAI Xue, XU Ming, YAO Chuang(1)

A Hardware-in-the-Loop Simulation Strategy of Space Fine Manipulation Based on Admittance Control

ZHENG Haichao, HE Jun, CHEN Longhai(8)

On Shape Remain of Radial Collinear N-Craft Coulomb Formation

SUN Yunlong，YUAN Changqing，LI Zhengguang(16)

Configuration Design of Navigation Constellation Reconfiguration Based on Quick Response

ZHAO Shuang, ZHANG Yasheng, DAI Huayu(26)

The Energy Response Calibration of FXPT

SHI Yongqiang,XI Tongxin,XIN Youmei,CHEN Jianwu,DENG loulou,LV Zhengxin,MEI Zhiwu(34)

An Adaptive Resonance Demodulation Method Based on Fault Diagnosis for Aerospace Precise Bearing

LIU Hongxing, QING Tao, WANG Hong, HE Tian, ZHANG Shaohua(40)

Network Protocol Stack Transportation Based on SpaceOS2

YUAN Ruicheng, LIU Bo, QIAO Lei, LIU Jianpei(46)

Saturated Control of Spacecraft Attitude Subject to External Disturbances

HU Jinchang,ZHANG Honghua, WANG Zeguo,CHEN Shangshang(56)

A Method of Network Data Transfer From Space to Ground Base on Dynamic Flux Control

YANG Jiaxin,YU Hang(61)

Spiral-Scanning Algorithm for User Inter-Satellite Antenna

LI Rong, PANG Jie, CHAO Ning(66)

A Novel Parallel-Output Regulation Circuit With Two Control Loops

SU Shaokan，PENG Bo，WANG Liwei , ZHANG Wei, CHANG Tao，CHEN Mingyang(72)

No.5

Experimental Research of Vibration Control on Two-Link Flexible Manipulator Based on Acceleration Feedback

QIU Zhicheng, LI Cheng(1)

Vibration Suppression Strategy for Flexible Joint of Large Manipulator Based on a Six Dimensional Accelerometer

NI Fenglei, LIN Pengfei, ZOU Tian(7)

A Fast Path Planning Method for Space Robot in Dynamic Environment

HU Xiaodong, HUANG Xuexiang, HU Tianjian, WANG Fenglin, LIANG Shuli(14)

An Improved Damped Least Squares Method for Solving Inverse Kinematics Problem of Manipulator

WANG Yunpeng, XIE Yongchun(22)

Modelling and Designing of the Flexible Docking and Fueling Mechanism for the Satellites

HUANG Jianbin, HUANG Longfei, HAN Xu, MENG bo, LI Zhi, WANG Wenlong, LI Wen(30)

Stabilization Control of Combined Spacecraft After Multiple Impacts During Space Robot Capturing the Target

HAN Dong, HUANG Panfeng, LIU Xiyao(38)

Robust Formation Control of Heterogeneous Multi-agent Systems with Uncertain Communications

LIU Miao, LI Zhongkui(47)

Task Allocation of Multi-Robot Based on Improved Ant Colony Algorithm

QIN Xinli, ZONG Qun, LI Xiaoyu, ZHANG Boyuan, ZHANG Xiuyun(55)

Simulation and Analysis of On-Orbit Operations with Flexible Space Manipulators

LI Kai, ZHANG Yao, CHEN Yujun(60)

A Control-Parametrization-Based Optimal PID Tuning Method for a Two-Link Manipulator

GUO Xiaolong, GUO Minhua, TAN Yuan, CAO Hanyu，DIAN Songyi, LI Bin(70)

Secure Control of Euler-Lagrange Systems Under Denial-of-Service Attacks

CAO Ran, CHENG Long(76)

Sliding-Mode Adaptive Attitude Controller Design for Flapping-Wing Micro Air Vehicle

LI Hang，HE Guangping，BI Fuguo(81)

No.6

Earth-Oriented Attitude Recovery Control Method of Satellites with Geocentric Vector Measurements Only

LEIYongjun,WEIChunling,HEYingzi,LIUJie(1)

Space Manipulator Compliant On-Orbit Assembly without Vision Feedback

DENGYa,LIUWeihui,LIXiaohui,WENWen(8)

Composite Control of an Active-Passive Micro-Vibration Isolator Utilized for Reaction Wheel Assembly

LILinfeng,ZHANGJiyang,LUORuizhi(13)

Design of a Drive Controller for Satellite-Borne Solar Wing

LILijiao,SHIRan,YANDan,MAJiyu,ZHANGJun(22)

Measurement of the Micro-Vibration of the Spacecraft Solar Panels Using Monogenic Multiscale Phase

ZHENGShaojie,XUEBindang，ZHANGGuoqi(32)

The Ultra-Linear Digital Proportional Solenoid Valve Designed for High Load Conditions

ZHANGZhen,

WANGXudong,WANGDaihua,LIANGLiang,PANBin,ZHANGLiang,PANBin,ZHANGLiang(39)

Total Ionizing Dose Radiation Effects of Four-Transistor CMOS Image Sensors in Star Trackers

CAOZhongxiang,ZHONGHongjun,ZHANGYunfang,LIQuanliang(45)

Design and Analysis of Flexible Supporting Structure for the Baffle of High-Accuracy Star Sensor

LIUJing，YUChengwu，ZHONGHongjun，SUNJie，WUYanpeng(51)

Time Synchronization Design Method for Spacecraft System Based on 1553B Bus

LIJingsong,CHENZhaohui,DANGJihong,LIHaoran,DONGXiaogang,LIXiaofeng(56)

Static Data Conflict Analysis Based on Parameter Type and Access Sequence

DONGYan,HUANGChen,WANGXiaoli,YULikun,YUQian(62)

A White-Black-White-Box Mixed Unit Test Technology of Spacecraft Software

ZHENGXiaomeng,GAOMeng,TENGJunyuan(69)