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CNKI期刊论文0611(3)
在“
Elsevier电子期刊
”中,
命中:
334
条,耗时:0.0839599 秒
在所有数据库中总计命中:
4,749
条
1.
Magnetic
attitude
control
for Earth-pointing
satellite
s in the presence of gravity gradient
作者:
Kaixing Zhou
kxing@buaa.edu.cn
;
Hai Huang
;
hhuang@buaa.edu.cn
;
Xinsheng Wang
xswang@buaa.edu.cn
;
Liang Sun
sunliang@buaa.edu.cn
关键词:
Micro
satellite
;
Earth-pointing
;
Magnetic
control
;
Sliding mode
;
Gravity gradient
刊名:Aerospace Science and Technology
出版年:2017
2.
Flexible
attitude
control
design and on-orbit performance of the ZDPS-2
satellite
作者:
Shengchao Deng
a
;
Tao Meng
b
;
mengtao@zju.edu.cn
;
Hao Wang
b
;
Chaoyu Du
a
;
Zhonghe Jin
b
关键词:
ZDPS-2
;
Nano-
satellite
;
ADCS
;
Flexible deployable mechanism
;
Three-axis stabilization
刊名:Acta Astronautica
出版年:2017
3.
A two-stage extended kalman filter method for fault estimation of
satellite
attitude
control
systems
作者:
Xueqin Chen
;
Ming Liu
;
mingliu23@hit.edu.cn
刊名:Journal of the Franklin Institute
出版年:2017
4.
Experimental research on low-cost cold gas propulsion for a space robot platform
作者:
Jan Kindracki
1
;
jkind@itc.pw.edu.pl
;
Karolina Tur
;
Przemysław Paszkiewicz
;
Łukasz Mężyk
;
Łukasz Boruc
;
Piotr Wolański
关键词:
Cold gas propulsion
;
Satellite
propulsion
;
Attitude
control
system
刊名:Aerospace Science and Technology
出版年:2017
5.
The on-orbit calibration of geometric parameters of the Tian-Hui 1 (TH-1)
satellite
作者:
Jianrong Wang
a
;
b
;
c
;
jianrongwang@sina.com
;
Renxiang Wang
a
;
b
;
Xin Hu
a
;
b
;
Zhongbo Su
c
;
d
关键词:
Satellite
photogrammetry
;
On-orbit calibration
;
LMCCD camera
;
Triangulation bundle adjustment
;
Location accuracy
;
Space resection
刊名:ISPRS Journal of Photogrammetry and Remote Sensing
出版年:2017
6.
Geolocation error tracking of ZY-3 three line cameras
作者:
Hongbo Pan
hongbopan@csu.edu.cn
关键词:
Bundle adjustment
;
ZY-3 three line camera
;
Error propagation
;
Geolocation error
;
Relative orientation
刊名:ISPRS Journal of Photogrammetry and Remote Sensing
出版年:2017
7.
Ionospheric electron density perturbations during the 7-10 March 2012 geomagnetic storm period
作者:
Anna Belehaki
a
;
belehaki@noa.gr
;
Ivan Kutiev
b
;
a
;
Pencho Marinov
c
;
Ioanna Tsagouri
a
;
Kostas Koutroumbas
a
;
Panagiotis Elias
a
关键词:
Ionospheric electron density
;
Total electron content
;
Travelling ionospheric disturbances
;
Superfountain effect
;
Sub-auroral polarization streams
;
Ionospheric topside profiler
刊名:Advances in Space Research
出版年:2017
8.
Design and analysis of a moment
control
unit for agile
satellite
with high
attitude
stability requirement
作者:
Yao Zhang
a
;
1
;
zhangyao@bit.edu.cn" class="auth_mail" title="E-mail the corresponding author
;
Mou Li
a
;
2
;
15201622364@163.com" class="auth_mail" title="E-mail the corresponding author
;
Zhuoyue Song
a
;
3
;
szhuoyue@bit.edu.cn" class="auth_mail" title="E-mail the corresponding author
;
Jinjun Shan
b
;
4
;
jjshan@yorku.ca" class="auth_mail" title="E-mail the corresponding author
;
Xin Guan
c
;
5
;
guanxin2007@tsinghua.org.cn" class="auth_mail" title="E-mail the corresponding author
;
Liang Tang
c
;
6
;
tl614@sina.com.cn" class="auth_mail" title="E-mail the corresponding author
关键词:
Control
moment unit
;
Vibration isolation
;
Control
moment gyro
;
Attitude
control
刊名:Acta Astronautica
出版年:2016
9.
Verification of Spin Magnetic
Attitude
Control
System using air-bearing-based
attitude
control
simulator
作者:
H.S. Ousaloo
a
;
hamed.oosaloo@gmail.com" class="auth_mail" title="E-mail the corresponding author
;
M.T. Nodeh
b
;
R. Mehrabian
c
关键词:
Spin magnetic
attitude
control
system
;
Spin
satellite
;
Spin stabilization
;
Verification
;
HIL
;
Simulator
;
Air-bearing
刊名:Acta Astronautica
出版年:2016
10.
Simultaneous state and actuator fault estimation for
satellite
attitude
control
systems
作者:
Yao ChengAuthor Vitae
;
Rixin Wang
;
wangrx@hit.edu.cn" class="auth_mail" title="E-mail the corresponding author
Author Vitae
;
Minqiang XuAuthor Vitae
;
Yuqing LiAuthor Vitae
关键词:
Actuator fault estimation
;
Augmented state observer
;
Fault diagnosis
;
Lipschitz nonlinear system
;
Satellite
attitude
control
system
刊名:Chinese Journal of Aeronautics
出版年:2016
1
2
3
4
5
6
7
8
9
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