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Aerospace Control
1006-3242
2006 Issue 3
Modal Analysis and Model Reduction for Flexible Cantilever Plate System of Spacecraft
Qiu Zhicheng
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page:89-96
Modeling and Analyzing of a New Pneumatic Rudder-control System
Qu Xueyun;Hong Feng;Deng Xianwei
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page:84-88
Inference Engine Design for Launching Decision -making Expert System
Zhang Qingzhen;Li Qingdong;Ren Zhang
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page:81-83,96
Application of Software Reliability Metrics in Aerospace Control Software
Yuan Xincheng;Shi Zhu
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page:74-80
Development of Instrument for the Remote Sensing and Simulating of Controller
Wang Zhiqiang;Li Jihong;Zhou Jianhua;Xiao Weiping
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page:70-73
Summary of State Measure Methods of Formation Flying and Research on Feasible High Precision Measure Schemes of Intersatellite Baseline
Liu Yang;Yi Dongyun;Wang Zhengming
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page:65-69,80
Temperature Measurement and Control System for Payload Based on CAN Bus
Fang Shixiong;Li Qi
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page:61-64,80
Design of SOC System Structure Based on AMBA Bus
Jiang Penglong;Song Zhengyu;Liu Zhihua;Lv Huaibei
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page:57-60
Design of Integrated Navigation Computer on a Chip Based on PowerPC Embedded Processor Core
Liu Yun;Zhao Wei;Liu Jianye
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page:54-56,60
Simulation and Optimization of Nested PLL in TT&C Transponder
Sun Wenfeng;Yu Faxin;Jin Zhonghe;Wang Chunhui;Wang Song;Wang Yuelin
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page:48-53
Active Magnetic Attitude Control of Microsatellite Without Gyroscope
Chen Hongyu
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page:43-47,53
Gyroless Attitude Determination Algorithms of Solar Observation Satellite
Cao Yongmei;Wang Xiaolei;Huang Jiangchuan
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page:39-42,53
Orbit Maintenance for Long Life Satellites
Chen Ying;He Yingzi;Han Dong
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page:35-38
Roll/Yaw Attitude Controller Design of Biased Momentum Satellite Based on Roll Information Feedback
Li Chuanjiang;Ma Guangfu;Song Bin
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page:29-34
Reentry Attitude Double-loop SMC of the Spacecraft and Its Logic Selection
Jia Jie;Jing Quan
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page:25-28,38
Study of SINS/DGPS/Magnetometer Integrated Navigation System
Wang Zhi;Zhang Jun
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page:21-24,34
Design Study of Variable Structure Control of Rotating Missile with Moving Centroid
Bi Kaibo;Zhou Jun;Zhou Fengqi
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page:17-20
Research on Rapid Auto-aligning Method--The Method to Relieve the Influence of Heading-effect
Xiao Zhenglin;Qian Peixian
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page:13-16
Research on Attitude Law of Mass Moment Missile Based on Fuzzy Control
Guo Qing;Yang Ming;Wang Zicai
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page:7-12
Adaptive Filter of Output Signal in Optical Fiber Gyroscope
Zhang Xi;Wang Xiaxiao;Wu Zhanjun
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page:4-6,12
xin shi jue chan sheng xin chuang zao
hou xiong
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page:3