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Chinese Academy of Sciences Institutional Repositories Grid
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CAS IR Grid
机构
长春光学精密机械与物... [2]
新疆天文台 [2]
力学研究所 [1]
计算技术研究所 [1]
沈阳自动化研究所 [1]
合肥物质科学研究院 [1]
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OAI收割 [9]
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会议论文 [5]
期刊论文 [4]
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2024 [1]
2020 [1]
2019 [1]
2013 [1]
2012 [2]
2011 [1]
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Computer S... [1]
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Mechanical Shock Wave Suppression Structure in Hold-Down and Release Apparatus of Spacecraft
期刊论文
OAI收割
AIAA JOURNAL, 2024
作者:
Yang, Yan
;
Liu, Wei
;
Zhou, Hao
;
Yang, Jianzhong
;
Wang, Xianping
  |  
收藏
  |  
浏览/下载:10/0
  |  
提交时间:2024/11/20
Shock Waves
Spacecrafts
Cylindrical Shell Structures
Frequency Response
Satellites
Aerospace Engineering
Finite Element Method
Spacecraft Structures
Numerical Simulation
Cylindrical Coordinate System
HPC software capability landscape in China
期刊论文
OAI收割
INTERNATIONAL JOURNAL OF HIGH PERFORMANCE COMPUTING APPLICATIONS, 2020, 卷号: 34, 期号: 1, 页码: 115-153
作者:
Chen, Daobi
;
Yuan, Liang
;
Zhang, Yunquan
;
Yan, Jingfu
;
Kahaner, David
  |  
收藏
  |  
浏览/下载:58/0
  |  
提交时间:2020/12/10
Advanced materials
artificial intelligence
AI
biotechnology
biotech
earth sciences
education
energy
power
natural resources
engineering
environmental
pollution
government S&T policy
funding
high-performance computing (HPC)
hw
sw
apps
information technology
IT
manufacturing
mathematics
meteorology
modeling
simulation
physics
space
satellite
aerospace
Approach to cross-company spacecraft software defect prediction based on transfer learning
期刊论文
OAI收割
Guangxue Jingmi Gongcheng/Optics and Precision Engineering, 2019, 卷号: 27, 期号: 2, 页码: 469-478
作者:
Q.-H.Ha
;
D.-Y.Liu
;
Y.Chen
;
L.Liu
  |  
收藏
  |  
浏览/下载:116/0
  |  
提交时间:2020/08/24
Software testing,Aerospace engineering,Application programs,Classification (of information),Defects,Efficiency,Forecasting,Learning systems
Three-dimensional dynamic behavior of the flexible umbilical cable system
会议论文
OAI收割
2013 4th International Conference on Mechanical and Aerospace Engineering, ICMAE 2013, Moscow, Russia, July 20-21, 2013
作者:
Quan WC(全伟才)
;
Zhang ZY(张竺英)
;
Zhang AQ(张艾群)
;
Zhang QF(张奇峰)
收藏
  |  
浏览/下载:21/0
  |  
提交时间:2013/12/26
Aerospace engineering
Equations of motion
Ocean currents
Shear flow
Ships
Three dimensional
Lattice Boltzmann Simulations of a pitch-up and pitch-down maneuver of a span-wise flexible wing in a free stream flow Read More: http://arc.aiaa.org/doi/abs/10.2514/6.2012-300
会议论文
OAI收割
50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Nashville, TN, United states, JAN 09-12, 2012
作者:
Qi DW
;
He GW(何国威)
;
Liu YM
收藏
  |  
浏览/下载:59/0
  |  
提交时间:2013/02/26
Aerospace engineering
Deformation
Exhibitions
Flexible wings
Reynolds number
Rigidity
Vortex flow
Aerodynamic forces
Chord-based Reynolds number
Flexural rigidities
Free stream
Free-stream flow
Lattice boltzmann
Leading-edge vortices
Lift coefficient
Lift force
Particle methods
Pitch rate
Power efficiency
Reduced frequency
Three dimensional space
Time-periods
Tip edge
Trailing edges
Trailing vortex
双层星座中负载均衡路由协议研究
期刊论文
OAI收割
宇航学报, 2012, 卷号: 33, 期号: 6, 页码: 746-753
陈建州
;
王路
;
刘立祥
;
胡晓惠
收藏
  |  
浏览/下载:45/0
  |  
提交时间:2012/11/12
Aerospace engineering
Space flight
Feasibility Study of USO's Stability in Mars Exploration
会议论文
OAI收割
Beijing, PEOPLES R CHINA, MAY 05-06, 2011
作者:
Shang, K.
;
Wang, Z.
;
Ping, J. S.
;
Wang, N.
  |  
收藏
  |  
浏览/下载:28/0
  |  
提交时间:2018/03/12
Yinghuo-1
Ultra Stable Oscillator
Frequency Standard
Engineering
Aerospace
Bootstrap loader design of aerospace payload controller based on TSC695F (EI CONFERENCE)
会议论文
OAI收割
2010 2nd International Conference on Computational Intelligence and Natural Computing, CINC 2010, September 13, 2010 - September 14, 2010, Wuhan, China
Xu W.
;
Piao Y.
收藏
  |  
浏览/下载:37/0
  |  
提交时间:2013/03/25
Anti-radiation TSC695F is usually used as aerospace payload controller in tasks to ensure the aerospace payload having extremely high reliability in abominable space environment. The processor bases on SP ARC V7 architecture with parity check and EDAC
so it could design out high reliable bootstrap loader to guarantee the operation system of VxWorks and application codes loaded correctly and worked stable and high effective. First
this paper put forward the system hardware composition and boot mode which apply for aerospace payload
then it makes clear the related contents of register group initialization
stack initialization
system hardware initialization in bootstrap loader of TSC695F and give out the method to establish TRAP table. That's all through comparing different type of organize mode of program image. After that
compiling of target codes have been described and the kernel code of MakeFile had been given at the same time for reference aimed at the realization of engineering. Although this paper is based on TSC695F
but it could be extended to other embedded system based on SP ARC for bootstrap loader analysis and design
for example
the TSC697 which based on SP ARC V8 with higher performance
so this paper has extremely high engineering value. 2010 IEEE.
Autonomous navigation based on X-ray pulsar timing
会议论文
OAI收割
Wuhan, PEOPLES R CHINA, NOV 10-11, 2007
作者:
Wang, N.
;
La, D. S.
  |  
收藏
  |  
浏览/下载:29/0
  |  
提交时间:2018/03/12
X-ray Pulsar
Autonomous Navigation
Phase Measurement
Time Of Arrival
Remote Sensing
Engineering
Telecommunications
Aerospace