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Current Issue
2016, Vol.37 No.12
Published date:15 December 2016
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Numerical Simulation of Three Dimensional Large Amplitude Liquid Sloshing in Spherical Containers
YUE Bao zeng, TANG Yong
Journal of Astronautics. 2016, 37 (12): 1405-1410.
DOI:
10.3873/j.issn.1000-1328.2016.12.001
Abstract (
207
)
PDF (2447KB) (
657
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Dynamic Parameter Identification of Free Floating Space Robots after Capturing Targets
LUO Jian jun, XUE Shuang shuang, MA Wei hua, WANG Ming ming
Journal of Astronautics. 2016, 37 (12): 1411-1418.
DOI:
10.3873/j.issn.1000-1328.2016.12.002
Abstract (
324
)
PDF (2408KB) (
1308
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Stress Wave Force Balance for Use in Hypersonic Impulse Facilities
LIU Shi ran, YANG Yun xiu, HU Shou chao, HUANG Jun
Journal of Astronautics. 2016, 37 (12): 1419-1424.
DOI:
10.3873/j.issn.1000-1328.2016.12.003
Abstract (
139
)
PDF (2314KB) (
549
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Study of Fluctuating Pressure Spatial Correlation Characteristics of Instrument Cabin Model in a Rotated Body
LIU Zhen hao, REN Fang, WANG Xiao feng, QIN Zhao hong, JIA Zhou xia
Journal of Astronautics. 2016, 37 (12): 1425-1431.
DOI:
10.3873/j.issn.1000-1328.2016.12.004
Abstract (
148
)
PDF (1978KB) (
557
)
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A Cooperative Guidance Law for Multiple Missiles to Intercept Maneuvering Target
SONG Jun hong, SONG Shen min, XU Sheng li
Journal of Astronautics. 2016, 37 (12): 1432-1440.
DOI:
10.3873/j.issn.1000-1328.2016.12.005
Abstract (
207
)
PDF (3098KB) (
893
)
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Integrated Control of Position and Attitude for Terminal Guidance of Leader Follower Anti Ship Missiles
WU Yun jie, ZHANG Cong
Journal of Astronautics. 2016, 37 (12): 1441-1448.
DOI:
10.3873/j.issn.1000-1328.2016.12.006
Abstract (
172
)
PDF (2786KB) (
545
)
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A Method of Angular Acceleration Trajectory Planning to Suppress Residual Vibrations of Flexible Satellite
GENG Yun hai, HOU Zhi li, HUANG Si meng
Journal of Astronautics. 2016, 37 (12): 1449-1456.
DOI:
10.3873/j.issn.1000-1328.2016.12.007
Abstract (
195
)
PDF (1423KB) (
621
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Fault Tolerant Control Method for Active Pointing of Ultra Quiet Platform
WANG You yi, TANG Liang, HE Ying zi
Journal of Astronautics. 2016, 37 (12): 1457-1465.
DOI:
10.3873/j.issn.1000-1328.2016.12.008
Abstract (
207
)
PDF (3046KB) (
641
)
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Nonlinear Method for Multiple Impulse Hovering Control of Spacecraft
CHENG Bo, YUAN Jian ping, MA Wei hua
Journal of Astronautics. 2016, 37 (12): 1466-1472.
DOI:
10.3873/j.issn.1000-1328.2016.12.009
Abstract (
177
)
PDF (1465KB) (
589
)
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Design of a Screw Cone Drill for Lunar Regolith Drilling Mission
ZHANG Wei wei, JIANG Sheng yuan, LI Peng, SHEN Yi, DENG Zong quan, TANG De wei
Journal of Astronautics. 2016, 37 (12): 1473-1481.
DOI:
10.3873/j.issn.1000-1328.2016.12.010
Abstract (
140
)
PDF (2269KB) (
638
)
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Characteristic Analysis of the Hypervelocity Impact Acoustic Emission S2 Mode in Aluminum Plate
LIU Yuan, PANG Bao jun, CHI Run qiang, CAO Wu xiong
Journal of Astronautics. 2016, 37 (12): 1482-1490.
DOI:
10.3873/j.issn.1000-1328.2016.12.011
Abstract (
211
)
PDF (2410KB) (
580
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Three Degree of Freedom Spherical Magnetic Bearing with Low Interference Torque
MIAO Cun xiao, ZHAO Hang, HAN Tian, FAN Ya hong, XU Guo feng
Journal of Astronautics. 2016, 37 (12): 1491-1499.
DOI:
10.3873/j.issn.1000-1328.2016.12.012
Abstract (
124
)
PDF (2617KB) (
449
)
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Effect of Metamorphic UDMH Propellant on Steady State Performance of Liquid Rocket Engine
ZHA Bai lin, MA Yun teng, XU Zhi gao, TIAN Gan, MA Lan
Journal of Astronautics. 2016, 37 (12): 1500-1506.
DOI:
10.3873/j.issn.1000-1328.2016.12.013
Abstract (
197
)
PDF (2659KB) (
609
)
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Analysis on Utilization of Cooling Capacity for Ground Loading System of Cryogenic Propellants
XIE Fu shou, LEI Gang, WANG Lei, LI Yan zhong
Journal of Astronautics. 2016, 37 (12): 1507-1512.
DOI:
10.3873/j.issn.1000-1328.2016.12.014
Abstract (
146
)
PDF (1893KB) (
674
)
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