中国科学院机构知识库网格系统: 检索

浏览/检索结果: 共9条，第1-9条

帮助

条数/页：排序方式：
	Development and Space Experiment Verification of Annular Liquid Flow Payload for China Space Station 期刊论文 OAI收割 SYMMETRY-BASEL, 2024, 卷号: 16, 期号: 11, 页码: 21 作者: Wang J(王佳); Chen Y(陈一); Wu D(吴笛); Hu L(胡良); Ye ZJ(叶致君) \| 收藏 \| 浏览/下载：14/0 \| 提交时间：2025/01/06 space experiment annular liquid flow payload development thermocapillary convection oscillatory instability
	Design, integration, and test of the scientific payloads on-board the HERMES constellation and the SpIRIT mission 期刊论文 OAI收割 SPACE TELESCOPES AND INSTRUMENTATION 2022: ULTRAVIOLET TO GAMMA RAY, 2022, 卷号: 12181, 页码: 121811G 作者: HERMES Collaboration \| 收藏 \| 浏览/下载：21/0 \| 提交时间：2023/11/09 High Energy Astrophysics HERMES SpIRIT CubeSat Payload Space 4.0 Silicon Drift Detectors GAGG ASIC Gamma-ray Bursts
	The Payload Development and the Experiments for Studying Thermocapillary Convection in TG-2 Liquid Bridge 期刊论文 OAI收割 MICROGRAVITY SCIENCE AND TECHNOLOGY, 2021, 卷号: 33, 期号: 1, 页码: 14 作者: Duan L(段俐); Kang Q(康琦); Zhang, Jianquan; Li, Xiang; Hu L(胡良) \| 收藏 \| 浏览/下载：31/0 \| 提交时间：2021/03/30 Liquid bridge Payload development Experiment verification Space experiment
	Payload parameter identification method of flexible space manipulator 期刊论文 OAI收割 Aircraft Engineering and Aerospace Technology, 2020, 卷号: 92, 期号: 6, 页码: ‏ 925-938 作者: Ni ZY(倪智宇); Zhang, Yewei; Shen XH(沈昕慧); Wu SN(邬树楠); Wu ZG(吴志刚) \| 收藏 \| 浏览/下载：21/0 \| 提交时间：2020/05/30 Endpoint payload Modal frequency Parameter identification Subspace method Space manipulator Singular value decomposition
	Space Life Science of China in 2015 期刊论文 OAI收割 Chinese Journal of Space Science, 2016, 卷号: 36, 页码: 788-804 作者: Li Yujuan; Sui Li; Li Qiang;; Wang Rui;; Wang Rui \| 收藏 \| 浏览/下载：32/0 \| 提交时间：2018/12/12 Space Life Sciences Space Payload Simulated Microgravity Ionizing Radiation
	Experimental Study of Gravitation Effects on Liquid Crystal Phase Transitions in Polydisperse Aqueous Suspensions of Mg Al-2 Layered Double Hydroxide 期刊论文 OAI收割 MICROGRAVITY SCIENCE AND TECHNOLOGY, 2016, 卷号: 28, 期号: 2, 页码: 95-100 作者: Chen Y; Zhang L; Sun DJ; Sun ZW(孙址伟); Xu SH(徐升华) 收藏 \| 浏览/下载：51/0 \| 提交时间：2016/09/14 Thermocapillary convection Cylindrical annulus Payload Space experiment Microgravity fluid physics
	The research of the high precision universal stable reconnaissance platform in near space 会议论文 OAI收割 nternational symposium on photoelectronic detection and imaging 2011: space exploration technologies and applications, beijing, china, may 24, 2011 - may 26, 2015 YangHong-Tao; CaoJian-Zhong; FanZhe-Yuan; ChenWei-Ning 收藏 \| 浏览/下载：42/0 \| 提交时间：2012/07/09 Near space Stable platform Payload Light-weight design stabilization accuracy
	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：40/0 \| 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.
	An intelligent method for early design and decision of space payload (EI CONFERENCE) 会议论文 OAI收割 2010 1st IEEE International Conference on Progress in Informatics and Computing, PIC 2010, December 10, 2010 - December 12, 2010, Shanghai, China 作者: Han C.-S.; Wen M. 收藏 \| 浏览/下载：27/0 \| 提交时间：2013/03/25 This paper is concerned with the design and decision method of space payload in the early design phase. The objective is to develop a generalized intelligent framework to assist designers in designing space payload. A multi-level method is introduced which is based on the combination of case-based reasoning (CBR) multicriteria rough sets theory (MRST) and kernel-based self-organizing maps (KSOM). The first is CBR module which aims to help designers to obtain some similar cases of the new situation. The second is MRST module which can extract the decision rules of configuration seletion. The third is KSOM module which can reduce the variable range and design space of the space payload. The results demonstrate the effectiveness of the proposed design method. 2010 IEEE.