2024 | No.4 | No.3 | No.2 | No.1 | ||
2023 | No.6 | No.5 | No.4 | No.3 | No.2 | No.1 |
2022 | No.6 | No.5 | No.4 | No.3 | No.1 | No.2 |
2021 | No.6 | No.5 | No.4 | No.3 | No.2 | No.1 |
2020 | No.6 | No.5 | No.4 | No.3 | No.2 | No.1 |
2019 | No.6 | No.5 | No.4 | No.3 | No.2 | No.1 |
2018 | No.6 | No.5 | No.4 | No.3 | No.2 | No.1 |
2017 | No.6 | No.5 | No.4 | No.3 | No.2 | No.1 |
2016 | No.6 | No.5 | No.4 | No.3 | No.2 | No.1 |
2015 | No.6 | No.5 | No.4 | No.3 | No.2 | No.1 |
2014 | No.6 | No.5 | No.4 | No.3 | No.2 | No.1 |
2013 | No.6 | No.5 | No.4 | No.3 | No.2 | No.1 |
2012 | No.6 | No.5 | No.4 | No.3 | No.2 | No.1 |
2011 | No.6 | No.5 | No.4 | No.3 | No.2 | No.1 |
2010 | No.6 | No.5 | No.4 | No.3 | No.2 | No.1 |
2009 | No.6 | No.5 | No.4 | No.3 | No.2 | No.1 |
2008 | No.6 | No.5 | No.4 | No.3 | No.2 | No.1 |
Star-Tracker-Based Attitude Determination Algorithms |
Star-Tracker-Based Attitude Determination Algorithms |
. 2009 Vol. 35 (5): 61-64 |
Abstract (1751) |
A New Concept of Moon - Earth Space Transportation Platform |
LI Huifeng,LIN Zhenhai,XUE Songbai |
. 2009 Vol. 35 (5): 43-47 |
Abstract (1736) |
C-W Guidance-Based Aiming Point Correction Technique |
MA Yanhong1,2 , Hu Jun1 |
. 2009 Vol. 35 (5): 52-55 |
Abstract (1577) |
Extraction and Matching of SIFT Feature for Simulated Lunar Environment |
LIU Jialu |
. 2009 Vol. 35 (5): 48-51 |
Abstract (1564) |
Introduction to Simultaneous Maneuvers and Composite Control of |
GOU Xingyu1,2 , CHEN Yiqing1,2 , LI Tieshou1,2 , HE Yingzi1,2 , TANG Liang1,2 |
. 2009 Vol. 35 (5): 1-5 |
Abstract (1557) |
A New Modeling Method of Satellite Fault Diagnosis |
ZHANG Xiaogong, REN Zhang |
. 2009 Vol. 35 (5): 38-42 |
Abstract (1555) |
Adaptive Control Scheme for the Capture of a Tumbling Spacecraft Using Free-Floating Space Manipulators |
WANG Hanlei1,2, XIE Yongchun1,2 |
. 2009 Vol. 35 (5): 6-12 |
Abstract (1539) |
In-Orbit Identification of the Inertial Matrix of Zero Momentum Satellite |
LIN Jiawei1,2,WANG Ping1 |
. 2009 Vol. 35 (5): 26-30 |
Abstract (1524) |
An Accurate Orbit Determination Technique Using GPS Receiver |
SUN Baoxiang1,2 |
. 2009 Vol. 35 (5): 20-25 |
Abstract (1515) |
A New Method for Discriminating Moon Interference Based on CES Software |
TU Zhijun1,2,MEI Zhiwu1,2,YUAN Jun1 |
. 2009 Vol. 35 (5): 31-37 |
Abstract (1505) |
Research on Universality of Equipment Monitoring Software Framework in a Satellite Earth Station |
KE Ling,XU Jing,LI Ying |
. 2009 Vol. 35 (5): 56-60 |
Abstract (1505) |
Research on Attitude Dynamics Modeling and Control for Spin-Stabilized Micro-Satellite |
TIAN Lin, XU Shijie |
. 2009 Vol. 35 (1): 47-50 |
Abstract (1476) PDF (336KB) (1652) |
Discrete-Time Fuzzy Adaptive Control for the Hypersonic Aircraf |
GAODaoxiang 1,2,SUNZengqi 1,2,3 |
. 2009 Vol. 35 (5): 13-19 |
Abstract (1470) |
Effect of Barrel’s Thermal Deformation on Measurement Error of a Star Sensor |
LIU Haibo1;HAO Yuncai2;TAN Jichun1;TAN Wei1;LIU Yiwu2 |
. 2008 Vol. 34 (5): 22-25 |
Abstract (1460) |
Modeling and Analysis of Pressure Regulation Unit for Electric Propulsion System |
GOU Haoliang;PAN Hailin |
. 2008 Vol. 34 (5): 49-52 |
Abstract (1446) |
Fuzzy Adaptive Concerted Driving Control for Lunar Rover with Reduced Tracking Errors |
SUN Duoqing1;2;MA Xiaoying2;3;YANG Xiaojing1;YU Baiyin1;SHAO Xiangyuan1 |
. 2008 Vol. 34 (5): 12-16 |
Abstract (1444) |
Particle filter algorithm for relative navigation of space non-cooperative target |
Jin Huanghuang, Wen Qiyong, Xia Hongwei, Wang Changhong |
. 2009 Vol. 35 (4): 6-10 |
Abstract (1411) |
A Ground Test Method of Electrostatic Discharge for Infrared Earth Sensor |
QI Chunzi;LIU Xuli |
. 2008 Vol. 34 (5): 8-11 |
Abstract (1399) |
A Velocity-free Attitude Controller of Flexible Spacecraft |
CAI Jian1,2, WANG Fang1,2 , ZHANG Honghua1,2 |
. 2009 Vol. 35 (2): 18-23 |
Abstract (1394) PDF (411KB) (1798) |
A Method of Approximate Second-Order Extended Kalman Filter |
FAN Wei 1,2, LI Yong 3 |
. 2009 Vol. 35 (1): 30-35 |
Abstract (1381) PDF (419KB) (1821) |
. 2013 Vol. 39 (1): 0- |
Abstract (621) PDF (16158KB)(12562) |
Design of STK-Based Realtime Visualization Simulation System for Satellites |
DU Yaoke |
. 2009 Vol. 35 (2): 61-64 |
Abstract (1206) PDF (441KB)(3064) |
Fault Mode Analysis and Fault Tolerant Methodology for SRAM-Based FPGA on Spacecraft |
HAO Zhigang 1, YANG Mengfei 2 |
. 2009 Vol. 35 (1): 51-55 |
Abstract (1161) PDF (416KB)(1942) |
Application of Contraction Mapping Theorem in Accelerometer Calibration for Inertial Navigation System |
WANG Libin, LIU Feng, SHANG Kejun, LU Jian |
. 2009 Vol. 35 (1): 61-64 |
Abstract (1108) PDF (307KB)(1862) |
A Method of Approximate Second-Order Extended Kalman Filter |
FAN Wei 1,2, LI Yong 3 |
. 2009 Vol. 35 (1): 30-35 |
Abstract (1381) PDF (419KB)(1821) |
A Velocity-free Attitude Controller of Flexible Spacecraft |
CAI Jian1,2, WANG Fang1,2 , ZHANG Honghua1,2 |
. 2009 Vol. 35 (2): 18-23 |
Abstract (1394) PDF (411KB)(1798) |
Design of Predictor-Corrector Reenty Guidance Law for Lunar Mission Spacecraft |
LI Huifeng,ZHANG Rui |
. 2009 Vol. 35 (1): 19-24 |
Abstract (1051) PDF (416KB)(1776) |
Motion Simulators for Rendezvous Simulation Test |
ZHANG Xinbang,LIU Liangdong,LIU Shenzhao |
. 2009 Vol. 35 (2): 51-55 |
Abstract (951) PDF (346KB)(1676) |
An Autonomous Navigation Method for Spacecrafts during Orbit Maneuver |
XIONG Kai1,2, WEI Chunling1,2, LIU Liangdong1,2 |
. 2009 Vol. 35 (2): 7-12 |
Abstract (1044) PDF (447KB)(1654) |
Research on Attitude Dynamics Modeling and Control for Spin-Stabilized Micro-Satellite |
TIAN Lin, XU Shijie |
. 2009 Vol. 35 (1): 47-50 |
Abstract (1476) PDF (336KB)(1652) |
The Attitude Control of Variable Parameter Spacecraft by Using Intelligent Adaptive Control Method |
YU Xinxin 1,2, XIE Yongchun 1,2 |
. 2009 Vol. 35 (1): 36-41 |
Abstract (1282) PDF (427KB)(1645) |
Fast Simulation Platform for Mixed Programming Technique-Based AOCC Application Software |
ZHANG Yin, SUO Xu-Hua, GUO Ming-Shu- |
. 2010 Vol. 36 (1): 56-58 |
Abstract (368) PDF (1095KB)(1628) |
Effect of Gravitational Perturbations on Satellite Orbit via Different Astronomy Standards |
JIANG Fanghua, LI Junfeng, BAOYIN Hexi |
. 2009 Vol. 35 (2): 38-41 |
Abstract (1086) PDF (337KB)(1557) |
Backstepping Controller Design for Space Robot |
ZHANG Jun 1,2, HU Haixia 1.2, XING Yan 1,2 |
. 2009 Vol. 35 (1): 7-12 |
Abstract (1078) PDF (387KB)(1549) |
Safety Analysis of Angular Contact Ball Bearing in CMG under Random Vibration |
WANG Xiaowei, XU Yingxia |
. 2009 Vol. 35 (2): 29-34 |
Abstract (1068) PDF (478KB)(1522) |
Sensor Fault Identification for A Satellite Navigation System |
LIU Chunjuan1, SONG Hua1,2, QIU Hongzhuan1,LIU Changhua3 |
. 2009 Vol. 35 (2): 13-17 |
Abstract (995) PDF (458KB)(1520) |
Control Allocation and Reconfiguration of Redundant Wheels for Spacecraft Attitude Control System |
ZHAO Yang, ZHANG Da-Wei, TIAN Hao |
. 2010 Vol. 36 (1): 1-6 |
Abstract (349) PDF (1145KB)(1501) |
Moment of Inertia Unknown Non-Cooperative Target Angular Velocity Estimation |
LIU Zhi-Yong, HE Ying-Zi, LIU Tao- |
. 2010 Vol. 36 (1): 24-30 |
Abstract (421) PDF (773KB)(1500) |
Attitude Controller Design for Combined Spacecraft after Separated LIU Sai, XU Shijie |
LIU Sai, XU Shijie |
. 2009 Vol. 35 (2): 35-37 |
Abstract (1104) PDF (301KB)(1496) |
Review of Fault Diagnosis Approach Based on Qualitative Model |
GAO Wei 1,2, XING Yan 1,2, WANG Nanhua 1,2 |
. 2009 Vol. 35 (1): 25-29 |
Abstract (1135) PDF (450KB)(1486) |