Aerospace Contrd and Application 2011 Issue 5 Vibration Modal Analysis of Flexible Plate Structure Connected by a Flexible Hinge

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Aerospace Contrd and Application
1674-1579
2011 Issue 5

Vibration Modal Analysis of Flexible Plate Structure Connected by a Flexible Hinge
QIU Zhicheng;JIANG Heng

..............page:1-7

A New Method for Improving Fidelity of Air-Suspended Platform Simulation for Relative Orbit Motion between Satellites
SUN Chengqi

..............page:42-44

Modeling and Analysis of Testability for a Typical Product of Spacecraft Based on Multi-Signal Model
ZHANG Shuai;HU Zheng

..............page:45-48

Sattelite Three-Axis Attitude Determination Method Based on Radio-Frequency Sensor
CHANG Jiansong;LI Jiajia;WU Yunli;ZENG Haibo

..............page:14-19

On-Board Robust Tracking of Guidance Trajectory for Lunar Pinpoint Soft Landing
LIANG Dong;HE Yingzi;LIU Liangdong

..............page:8-13

A Method of CRC Check Implemented by Using C Language
YANG Junchun

..............page:49-51

High-Bandwidth Measurement Based Attitude Determination
HE Shimin;TANG Liang

..............page:20-25

Software Requirements Analysis for Attitude and Orbit Control System with User Story
LIN Rongfeng;CAI Hong

..............page:52-54,58

Modeling Method of Fiber Optic Gyro Based on AR Model
ZHOU Yi;LI Yong;ZHANG Feng

..............page:55-58

A Simulation Test-Bed for Rapid Maneuver Experiment of Flexible Satellite
RAO Weidong;XU Lijia

..............page:59-62

Completely Analytical Results of a Kind of Oscillators in Pulse Width Modulators
SUN Dinghao

..............page:26-30

Embedded Operating System Research and Design for Spacecraft
qiao lei ; peng fei ; zhao zuo ; sun yue ; yang zuo ; liu bo

..............page:31-35,41

Application of Divide-and-Conquer Strategy to the Data Stream Control of Satellite
HU Yuexin;ZHANG Duzhou

..............page:36-41