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CNKI期刊论文0611(3)
知网期刊论文(3643)
在“
Elsevier电子期刊
”中,
命中:
415
条,耗时:0.0779636 秒
在所有数据库中总计命中:
5,270
条
1.
MPC on manifolds with an application to the
control
of
spacecraft
attitude
on SO(3)
作者:
Uro&scaron
;
V. Kalabić
a
;
1
;
kalabic@umich.edu
Author Vitae
;
Rohit Gupta
a
;
rohitgpt@umich.edu
Author Vitae
;
Stefano Di Cairano
b
;
dicairano@ieee.org
Author Vitae
;
Anthony M. Bloch
c
;
abloch@umich.edu
Author Vitae
;
Ilya V. Kolmanovsky
a
;
ilya@umich.edu
Author Vitae
关键词:
Model predictive
control
;
Geometric
control
;
Manifolds
;
Lie groups
;
Spacecraft
attitude
刊名:Automatica
出版年:2017
2.
Singularity-free integral-augmented sliding mode
control
for combined energy and
attitude
control
system
作者:
Samira Eshghi
;
saeshghi@yahoo.com
;
Renuganth Varatharajoo
renu99@gmx.de
关键词:
Spacecraft
guidance and
control
;
CEACS
;
Flywheels
;
Low Earth orbit satellites
;
Sliding mode
control
;
Synergism
刊名:Advances in Space Research
出版年:2017
3.
Fault Tolerant
Attitude
Control
for
spacecraft
with SGCMGs under actuator partial failure and actuator saturation
作者:
Fuzhen Zhang
;
Lei Jin
;
jinleibuaa@163.com
;
Shijie Xu
关键词:
Spacecraft
;
Fault tolerant
control
method
;
Single gimbal
control
moment gyros
;
Gimbal rate saturation
;
Sliding mode
control
刊名:Acta Astronautica
出版年:2017
4.
Attitude
coordination of multiple
spacecraft
for space debris surveillance
作者:
Leonard Felicetti
a
;
leonard.felicetti@ltu.se
;
M. Reza Emami
a
;
b
;
reza.emami@ltu.se
;
reza.emami@utoronto.ca
关键词:
Space debris surveillance
;
Spacecraft
formation
;
Attitude
coordination
;
Attitude
control
刊名:Advances in Space Research
出版年:2017
5.
Attitude
control
of an underactuated
spacecraft
using quaternion feedback regulator and tube-based MPC
作者:
M. Mirshams
;
M. Khosrojerdi
;
mkhosrojerdi@mail.kntu.ac.ir
关键词:
Underactuated
spacecraft
;
Tube-based MPC
;
Quaternion feedback regulator
;
Fault tolerant
control
;
Spacecraft
detumbling
刊名:Acta Astronautica
出版年:2017
6.
Line-of-sight based
spacecraft
attitude
and position tracking
control
作者:
Rakesh R. Warier
;
rakeshwarier@sc.iitb.ac.in" class="auth_mail" title="E-mail the corresponding author
;
Arpita Sinha
asinha@sc.iitb.ac.in" class="auth_mail" title="E-mail the corresponding author
;
Srikant Sukumar
srikant@sc.iitb.ac.in" class="auth_mail" title="E-mail the corresponding author
关键词:
Line-of-sight based
control
;
Spacecraft
attitude
control
;
Spacecraft
formation flying
;
Coordinate-free
attitude
control
刊名:European Journal of
Control
出版年:2016
7.
Attitude
tracking
control
for
spacecraft
with robust adaptive RBFNN augmenting sliding mode
control
作者:
Yao Zou
a
;
b
;
zouyao20@126.com" class="auth_mail" title="E-mail the corresponding author
关键词:
Spacecraft
control
;
Attitude
tracking
;
Sliding mode
control
;
Robust adaption
;
Radial basis function neural network (RBFNN)
;
Switching function
刊名:Aerospace Science and Technology
出版年:2016
8.
Attitude
control
of an underactuated
spacecraft
using tube-based MPC approach
作者:
M. Mirshams
;
M. Khosrojerdi
mkhosrojerdi@mail.kntu.ac.ir" class="auth_mail" title="E-mail the corresponding author
关键词:
Underactuated
spacecraft
;
Spacecraft
attitude
control
;
Tube-based MPC
;
Fault tolerant
control
刊名:Aerospace Science and Technology
出版年:2016
9.
Attitude
takeover
control
for post-capture of target
spacecraft
using space robot
作者:
Panfeng Huang
a
;
b
;
pfhuang@nwpu.edu.cn" class="auth_mail" title="E-mail the corresponding author
;
Ming Wang
a
;
b
;
c
;
Zhongjie Meng
a
;
b
;
Fan Zhang
a
;
b
;
Zhengxiong Liu
a
;
b
关键词:
Attitude
control
;
Takeover
control
;
Post-capture
;
Space robot
;
Spacecraft
;
Control
allocation
刊名:Aerospace Science and Technology
出版年:2016
10.
Distributed finite-time velocity-free
attitude
coordination
control
for
spacecraft
formations
作者:
An-Min Zou
amzou2012@gmail.com" class="auth_mail" title="E-mail the corresponding author
Author Vitae
;
Anton H.J. de Ruiter
aderuiter@ryerson.ca" class="auth_mail" title="E-mail the corresponding author
Author Vitae
;
Krishna Dev Kumar
kdkumar@ryerson.ca" class="auth_mail" title="E-mail the corresponding author
Author Vitae
关键词:
Attitude
coordination
control
;
Spacecraft
formation flying
;
Finite-time
control
;
Velocity-free
;
Homogeneous method
刊名:Automatica
出版年:2016
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