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	Space advanced technology demonstration satellite 期刊论文 OAI收割 Science China Technological Sciences, 2024, 卷号: 67, 期号: 1, 页码: 240-258 作者: Zhang, XiaoFeng; Chen, Wen; Zhu, XiaoCheng; Meng, Na; He, JunWang \| 收藏 \| 浏览/下载：45/0 \| 提交时间：2024/02/01 SATech-01 spacecraft design scientific instruments on-orbit performance
	Space advanced technology demonstration satellite 期刊论文 OAI收割 SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2023, 页码: 19 作者: Zhang, Xiaofeng; Chen, Wen; Zhu, Xiaocheng; Meng, Na; He, Junwang \| 收藏 \| 浏览/下载：24/0 \| 提交时间：2024/02/05 SATech-01 spacecraft design scientific instruments on-orbit performance
	Space advanced technology demonstration satellite 期刊论文 OAI收割 SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2023, 页码: 19 作者: Zhang, Xiaofeng; Chen, Wen; Zhu, Xiaocheng; Meng, Na; He, Junwang \| 收藏 \| 浏览/下载：40/0 \| 提交时间：2024/02/22 SATech-01 spacecraft design scientific instruments on-orbit performance
	The influence of inner material with different average thermal conductivity on the performance of whole insulation system for liquid hydrogen on orbit storage 期刊论文 OAI收割 INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2021, 卷号: 46, 期号: 18, 页码: 10913-10923 作者: Wang, Ping; Ji, Lun; Yuan, Jing; An, Zhenguo; Yan, Kaiqi \| 收藏 \| 浏览/下载：28/0 \| 提交时间：2021/04/26 Passive insulation system Inner material Multilayer insulation Thermal insulation performance Liquid hydrogen on orbit storage
	Modeling and optimization of composite thermal insulation system with HGMs and VDMLI for liquid hydrogen on orbit storage 期刊论文 OAI收割 INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2020, 卷号: 45, 期号: 11, 页码: 7088-7097 作者: Wang, Ping; Ji, Lun; Yuan, Jing; An, Zhenguo; Yan, Kaiqi \| 收藏 \| 浏览/下载：29/0 \| 提交时间：2020/05/24 Liquid hydrogen on orbit storage Hollow glass microspheres Variable density multilayer insulation Optimal configuration Thermal insulation performance
	Quasi-All-Passive Thermal Control System Design and On-Orbit Validation of Luojia 1-01 Satellite 期刊论文 OAI收割 Sensors, 2019, 卷号: 19, 期号: 4, 页码: 18 作者: L.Yang; Q.Li; L.Kong; S.Gu; L.Zhang \| 收藏 \| 浏览/下载：50/0 \| 提交时间：2020/08/24 quasi-all-passive,thermal analysis,thermal balanced test,on-orbit,performance,temperature,fluctuation,Chemistry,Engineering,Instruments & Instrumentation
	AUTONOMOUS INTEGRATED NAVIGATION USING X-RAY PULSARS AND ASTEROIDS 会议论文 OAI收割 63rd International Astronautical Congress 2012, IAC 2012, Naples, Italy, 2012 Yang Chengwei; Gao Dong; Zheng Jianhua 收藏 \| 浏览/下载：39/0 \| 提交时间：2014/04/30 To improve the navigation performance of the spacecraft during interplanetary cruise a novel integrated navigation system is proposed. For X-ray pulsar navigation (XNAV) is a hot and prospective research subject and the optical navigation using asteroids is practical in space engineering we designed an autonomous navigation system using one X-ray detector and one navigation camera. The measurement models of the XNAV based on the time difference of arrival and the optical navigation based on the images of asteroids are presented. To enhance practicality the X-ray pulsars and asteroids are observed by turns. The batch least square filter used by Deep Space I is adopted to estimate the system state. The numerical simulation results show that the integrated navigation is feasible on the interplanetary cruise orbit. Moreover compared with the XNAV and the optical navigation the integrated navigation system can provide higher navigation performance.
	Electronic system design of ultraviolet ozone vertical profile probe for aerography satellite (EI CONFERENCE) 会议论文 OAI收割 2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011, August 12, 2011 - August 14, 2011, Harbin, China Song K.; Wang S. 收藏 \| 浏览/下载：20/0 \| 提交时间：2013/03/25 The design of ultraviolet ozone vertical profile probe is illustrated and the electronic system is introduced in detail. The device is a compact high precision ultraviolet-vacuum ultraviolet spectral radiometer and is used to measure atmospheric solar backscattering spectral radiance and solar spectral irradiance. Noise of the system is analyzed and Numeric accumulation and synchronous demodulation was used to decrease the noise and the zero-drift of the instrument. The solar irradiance at altitude 830 km in 160-400 nm and the backscattering solar spectral radiance in the ultraviolet ozone absorption band at 12 wavelengths from 250 nm to 340 nm are obtained. Test results on orbit show that all the requested function is met successfully and the performance is stable. 2011 IEEE.
	Memoryless polynomial LMS adaptive filter for orbit object tracking (EI CONFERENCE) 会议论文 OAI收割 2009 International Conference on Information Engineering and Computer Science, ICIECS 2009, December 19, 2009 - December 20, 2009, Wuhan, China 作者: Wang P. 收藏 \| 浏览/下载：28/0 \| 提交时间：2013/03/25 In order to find a fast and effective solution to orbit object tracking a memoryless polynomial adaptive filter is proposed in this paper. Unlike Volterra adaptive filter the proposed filter is composed of polynomials in different orders which can fit normal orbit trajectory well. A memoryless polynomial filter (MLF) is designed first. The designed memoryless polynomial filter can be separated into a linearization filter and a FIR filter. Analogous to linear LMS adaptive filter a LMS adaptive algorithm is derived for the memoryless polynomial filter which is called Memoryless polynomial LMS adaptive filter (MLPLMS adaptive filter). Experiments show that the proposed filter has better performance than that of a normal LMS filter on orbit tracking. 2009 IEEE.