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Aerospace Contrd and Application
1674-1579
2010 Issue 5
Characteristic Model-Based Identification and Control Of High-Order Linear Unstable System
WANG Lijiao
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page:25-31
Influence of Three-Axis Turntable Error on Calibration Accuracy of Accelerometer Error Model Coefficients
CHENG Yuan;CHEN Xijun;REN Shunqing;LI Wei
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page:58-62
Fast Shooting Method for Multi-Impulse Rendezvous in Near Circular Orbit
WANG Xiang;GONG Shengping;BAOYIN Hexi;LI Junfeng
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page:1-6
Robust Fault Detection for a Class of Nonlinear Networked Systems
HE Xiao;WANG Zidong;JI Yindong;ZHOU Donghua
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page:7-12,49
Terminal Sliding Mode Control for Multi-Target Attitude Tracking in Spacecraft Formation Flight
YUAN Changqing;LI Junfeng;ZHANG Weitai;ZHOU Hao
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page:18-24
Research on Test Design for Spacecraft
LI Bin;ZHANG Qiang;REN Kun;TANG Ning
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page:13-17
A Relative Phase-Keeping Strategy of Walker Constellation Based on Reference Orbit
HU Songjie;SHEN Jingsong;HUAN Pei
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page:45-49
Survey of Gimbal Drive Assembly Mechanism of Inter-Orbit Link Antenna for Tracking and Data Relay Satellites
CUI Chengmin;WANG Dianjun
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page:32-37
An Explicit Guidance Strategy in Halo-to-Halo Transfers
LIAN Yijun;MENG Yunhe;TANG Guojian
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page:50-53
An Adaptive PID Thermal Control of the Satellite Clock Based on RBF Neural Network
XU Bin;LIU Zhiyou;SUN Fuchun;YAO Wei;LIU Qingzhi
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page:42-44,49
An Anti-fused FPGA-Based Hardened Design for FSM
LIU Qun;FENG Dan;ZHOU Xinfa
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page:54-57,62
An Anti-Fixture Influence Handling Method for Flywheel Vibration Data
WANG Quanwu;WU Dengyun
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page:38-41