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[期刊论文] 作者：Lai TENG,Zhong-he JIN,
来源：信息与电子工程前沿（英文版） 年份：2018
A spacecraft’s separation parameters directly affect its flying trace.If the parameters exceed their limits,it will be difficult to adjust the flying attitude...
[期刊论文] 作者：Sheng-chao DENG,Tao MENG,Zhong-he JIN,
来源：信息与电子工程前沿（英文版） 年份：2017
Because of their volume and power limitation, it is difficult for CubeSats to configure a traditional propulsion system. Atmospheric drag is one of the space en...
,A combined modulated feedback and temperature compensation approach to improve bias drift of a clos
[期刊论文] 作者：Ming-jun MA,Zhong-he JIN?,Hui-jie ZHU,
来源：浙江大学学报（英文版）（C辑：计算机与电子） 年份：2015
The bias drift of a micro-electro-mechanical systems (MEMS) accelerometer suffers from the 1/f noise and the tem-perature effect. For massive applications, the...
[期刊论文] 作者：Shu-jian SUN,Tao MENG,Zhong-he JIN,
来源：信息与电子工程前沿（英文版） 年份：2019
An ammonia self-managed vaporization propulsion (ASVP) system for micro-nano satellites is presented. Compared with a normal cold gas or liquefied gas propulsio...
[期刊论文] 作者：Ming-chen ZHAO,Chun-hui WANG,Zhong-he JIN,,
来源：Journal of Zhejiang University-Science C(Computers & Electro 年份：2013
The accuracy of microwave ranging is mainly limited by the frequency instability of the oscillator that generates the carrier phase signal. A dual transponder c...
[期刊论文] 作者：Sheng-chao DENG,Tao MENG,Zhong-he JIN,,
来源：Frontiers of Information Technology & Electronic Engineering 年份：2017
立方星由于体积和功率限制,难以配置传统的推进系统以实现编队飞行。而大气阻力是低轨卫星可以用于轨道调整的空间环境动力之一。本文提出一种通过大气阻力实现轨道面内沿迹...
[期刊论文] 作者：Di-qing YING,Qiang LI,Hui-lian MA,Zhong-he JIN,,
来源：Journal of Zhejiang University-Science C(Computers & Electro 年份：2014
We present how residual intensity modulation(RIM) affects the performance of a resonator fiber optic gyro(R-FOG) through a sinusoidal wave phase modulation tech...
[期刊论文] 作者：Yang REN,Zhong-he JIN,Yan CHEN,Hui-lian MA,
来源：浙江大学学报（英文版）（C辑：计算机与电子） 年份：2011
Proportional integrator (PI) is always adopted in the resonant frequency servo loop in a resonator micro optic gyro (RMOG).The oscillation phenomenon is observe...
[期刊论文] 作者：Xia ZHANG,Hao WANG,Xu-dong ZHENG,Shi-chang HU,Zhong-he JIN,
来源：浙江大学学报（英文版）（C辑：计算机与电子） 年份：2010
...
[期刊论文] 作者：Jian-wen JIANG,Wei-jun YANG,Chao-jie ZHANG,Xiao-jun JIN,Zhong-he JIN,
来源：浙江大学学报（英文版）（C辑：计算机与电子） 年份：2011
...
[期刊论文] 作者：Hao WANG,Zhi-yuan WANG,Ben-dong WANG,Zhong-he JIN,John L.CRASSIDIS,
来源：信息与电子工程前沿（英文） 年份：2021
Infrared Earth sensors are widely used in attitude-determination and control systems of satellites. The main deficiency of static infrared Earth sensors is the...
[期刊论文] 作者：Hao WANG,Zhi-yuan WANG,Ben-dong WANG,Zhuo-qun YU,Zhong-he JIN,John L.CRASSIDIS,
来源：信息与电子工程前沿（英文版） 年份：2020
An artificial intelligence enhanced star identification algorithm is proposed for star trackers in lost-in-space mode. A convolutional neural network model base...
[期刊论文] 作者：Qiao WANG,Xiao-jun JIN,Wei ZHANG,Shi-ming MO,Zhao-bin XU,Zhong-he JIN,
来源：信息与电子工程前沿（英文版） 年份：2019
To overcome the shortcomings of the traditional measurement error calibration methods for spaceflight telemetry, tracking and command (TT&C) systems, an online...
[期刊论文] 作者：Qiao WANG,Xiao-jun JIN,Wei ZHANG,Shi-ming MO,Zhao-bin XU,Zhong-he JIN,,
来源：Frontiers of Information Technology & Electronic Engineering 年份：2019
为克服传统误差标校方法的缺点,提出一种基于星地差分GPS的航天测控系统在线误差标校方法。该方法采用固定区间平滑算法,平滑前向、后向抗差自适应卡尔曼滤波结果,同时基于蚁群最优化算法固定星地差分GPS载波相位模糊度,以获取高精度星地基线测量结果。将该结果......
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