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22 October 2011, Volume 37 Issue 5
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Vibration Modal Analysis of Flexible Plate Structure Connected by a Flexible Hinge
Qiu-Zhi-Cheng-； Jiang-Heng
2011, 37(5): 1-7.
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394
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On-Board Robust Tracking of Guidance Trajectory for Lunar Pinpoint Soft Landing
Liang-Dong-； He-Ying-Zi-； Liu-Liang-Dong
2011, 37(5): 8-13.
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367
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Sattelite Three-Axis Attitude Determination Method Based on Radio-Frequency Sensor
Chang-Jian-Song-； Li-Jia-Jia-； Wu-Yun-Li-； Zeng-Hai-Bo
2011, 37(5): 14-19.
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364
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High-Bandwidth Measurement Based Attitude Determination
He-Shi-Min-； Tang-Liang-；
2011, 37(5): 20-25.
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350
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Completely Analytical Results of a Kind of Oscillators in Pulse Width Modulators
Sun-Ding-Hao
2011, 37(5): 26-30.
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319
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Embedded Operating System Research and Design for Spacecraft
Qiao-Lei-； Peng-Fei-； Zhao-Wei-； Sun-Yue-； Yang-Hua-； Liu-Bo-；
2011, 37(5): 31-35.
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356
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Application of Divide-and-Conquer Strategy to the Data Stream Control of Satellite
Hu-Yue-Xin-； Zhang-Du-Zhou-；
2011, 37(5): 36-41.
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351
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A New Method for Improving Fidelity of Air-Suspended Platform Simulation for Relative Orbit Motion between Satellites
Sun-Cheng-Qi-；
2011, 37(5): 42-44.
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351
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Modeling and Analysis of Testability for a Typical Product of Spacecraft Based on Multi-Signal Model
Zhang-Shuai-； Hu-Zheng
2011, 37(5): 45-48.
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338
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A Method of CRC Check Implemented by Using C Language
Yang-Jun-Chun-；
2011, 37(5): 49-51.
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439
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Software Requirements Analysis for Attitude and Orbit Control System with User Story
Lin-Rong-Feng-； Cai-Hong-；
2011, 37(5): 52-54.
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411
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Modeling Method of Fiber Optic Gyro Based on AR Model
Zhou-Yi-； Li-Yong-； Zhang-Feng
2011, 37(5): 55-58.
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431
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A Simulation Test-Bed for Rapid Maneuver Experiment of Flexible Satellite
Rao-Wei-Dong-； Xu-Li-Jia
2011, 37(5): 59-62.
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361
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Table of Content
Table of Content
