[1] |
QI Nai-Ming, ZHAO Bao-Shan, ZHAO Zhi-Gang, WANG Li-Ping.
AbsoluteErrorSelectionCriteriaofUnconstrainedModefor FlexibleManipulatorDynamicsModelDimensionReduction
[J]. Chinese Space Science and Technology, 2012, 32(2): 22-28.
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[2] |
LI Biao, LIU Zhi-Quan, CHENG Gang, DING Feng.
ConfigurationParameterAnalysisforADAM-typeArticulatedMast
[J]. Chinese Space Science and Technology, 2012, 32(2): 29-34.
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[3] |
Wang Yueyu(China Academy of Space Technology,Beijing 100094).
One Sort of Finite Element Mesh Size Criteria for Structural High-frequency Random Response Analysis
[J]. Chinese Space Science and Technology, 2005, 25(05): 62-65+71.
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[4] |
Pei Yang Song Bifeng Li Zhanke(Northwestern Polytechnical University, Xi'an 710072).
On Geometric Description Algorithm of Spacecraft Shielding or Masking
[J]. Chinese Space Science and Technology, 2004, 24(05): -.
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[5] |
Huang Bencheng Chen Jinming Qi Yan Su Wen Huang Wei (Beijing Institute of Spacecraft Environment Engineering, Beijing 100029).
Vacuum Chamber Design
[J]. Chinese Space Science and Technology, 2002, 22(03): -.
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[6] |
Han Zengyao Qu Guangji ( Beijing Institute of Spacecraft System Engineering,Beijing10 0 0 86).
Wide-band Random Vibration Response Prediction Study of the Spacecraft Structures
[J]. Chinese Space Science and Technology, 2002, 22(01): -.
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[7] |
Ma Jinhua (Shandong Architectural and Civil Engineering Institute,Jinan 250014) Song Xiangeng Wang Junqi (Shandong Technology University,Jinan 250061) He Dexin (China Aerodynamics Research and Development Center,Mianyang 621000).
The Natural Vibration Performance Analysis of Lateral Vibration for the Launch Vehicle of Strap-on Boosters
[J]. Chinese Space Science and Technology, 2000, 20(05): -.
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[8] |
Huang Tieqiu Wu Delong Yan Shaoze (Beijing Institute of Astronautical Systems Engineering,Beijing 100076).
Nonlinear Dynamic Modeling of Deployable Truss Structures With Clearances
[J]. Chinese Space Science and Technology, 1999, 19(01): -.
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[9] |
Zhang Lihua (Beijing Institute of Spacecraft System Engineering,Beijing 100086).
Application of Finite Element Method in the Thermal Analysis of Spacecraft Antenna Reflector
[J]. Chinese Space Science and Technology, 1999, 19(01): -.
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[10] |
Sun Guojiang(Beijing Institute of Spacecraft System Engineering,Beijing 100086).
COUPLED VIBRATION ANALYSIS OF LIQUID COMBUSTIBLE AND STRUCTURE IN SATELLITE
[J]. Chinese Space Science and Technology, 1996, 16(01): -.
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[11] |
Fu Danying;Sun Jiwen(Beijing Institute of Space Machine and Electricity,Beijing 100076).
RESEARCH OF LIGHTWEIGHT HONEY-COMB HOLE STRUCTURE OF SPHERICAL REFLECTOR OF SPACEBORNE SENSOR
[J]. Chinese Space Science and Technology, 1994, 14(04): -.
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[12] |
Pei Yuntian (Shanghai Institute of Technical Physics,Chinese Academia of Science)
Liu Zhengxing (Shanghai Traffic University).
STUDY ON LIGHTWEIGHT MIRROR FOR SPACE OPTICAL INSTRUMENT
[J]. Chinese Space Science and Technology, 1991, 11(06): 11-16.
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[13] |
Li Lingzhi He Zhiqin Guo Zhaozeng Ju Tao (Beijing Inst,of Satellite Information Engineering).
FINITE ELEMENT METHOD FOR GEOMETRIC DISTORTION CORRECTION OF REMOTE SENSING IMAGE
[J]. Chinese Space Science and Technology, 1989, 9(02): 24-31.
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