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Aerospace Control
1006-3242
2013 Issue 3
The Design of UAV Flying Simulation System Based on Multi-Agent
YUN Chao;LI Xiaomin;ZHENG Zonggui;CHEN Naishu
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page:85-90
The Application Study on Embedded Real-Time Operation System in Launch Vehicle
SONG Zhengyu
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page:3-10
The Design and Research of Closed Loop General Testing Technique Based on BMU and LVDS Bus
ZHOU Huan;SONG Zhengyu
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page:45-49,61
The Optimal Multiple-Impulse Orbit Transfer by Using Hybrid Genetic Algorithm
FU Lei;AN Xiaomin;QIN Zhaohua;XU Min
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page:15-19
SINS Alignment with Large Azimuth Misalignment Angles
ZHAO Pengfei;QI Jianyu
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page:25-29
A Reliability Evaluation Approach for Aeronautical Products Based on Dempster-Shafer Theory
ZHOU Kuang;SHI Yimin;MA Lina
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page:91-96
A Method of Separatation Vibration Disturbance in Outfield Calibration of IMU
ZHANG Bin;LIU Jieyu;LI Cheng
..............
page:20-24,29
Research on Terminal Guidance and Control Integration for Hypersonic Vehicle
XIAO Hong;WANG Yong;GUO Haifeng;LI Wangxi;TANG Chuanlin
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page:74-80
The Evolvement Analysis of Satellite Formation under J2 Term and Atmosphere Drag Perturbation
HUANG Yong;LI Xiaojiang;WANG Zhiheng;LI Zhaoming
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page:62-68
Research on Identification Guide Stars Simulation Based on STK and Star Selection
ZHAO Hui;XIONG Zhi;WANG Rong;ZHANG Cheng;LIU Jianye
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page:55-61
Environment Modeling and Simulation for Initial Alignment on Rocking Base
LIANG Luyang;LIU Xijun;YANG Ye
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page:30-33,39
Study on MEMS-SINS in Initial Alignment with Magnetometer Assistance
GAO Yong;CAO Juanjuan;TANG Haihong;BAI Huanxu
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page:50-54
Research on Midcourse Guidance Law for Interceptor Based on Virtual Target
LI Shuang;JIANG Yong;ZHANG Yiqun;LI Junlong
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page:40-44
Study on the Ramjet Engine Control Paths
CHEN Xinmin;LI Yufei
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page:11-14,96
A Robust and Adaptive Depleted Shutdown Guidance Method of Solid Rocket
ZHOU Jun;PAN Yanpeng;HU Weijun
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page:34-39
Investigation for Overcoming Effect of Magnetic Field to High Precision North Finding with FOG
REN Lei;SHAO Chunjiang;ZHOU Lu;LIU Qingqing
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page:81-84,96
Linear Program Based on Aerosurfaces Reconfiguration Control Allocation
ZANG Xiheng;TANG Shuo
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page:69-73