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内部出版物
Elsevier电子期刊(853)
在“
Elsevier电子期刊
”中,
命中:
853
条,耗时:小于0.01 秒
在所有数据库中总计命中:
853
条
1.
Robust autopilot design for bank-to-turn
missile
s using adaptive dual-layer sliding mode control
作者:
Zongyi Guo
;
Eason.work@qq.com
;
Jun Zhou
;
Jianguo Guo
关键词:
Dual-layer sliding mode control
;
Adaptive
;
Bank-to-turn
missile
s
;
Autopilot design
;
External disturbances
刊名:Optik - International Journal for Light and Electron Optics
出版年:2017
2.
Dynamic stability of rolling
missile
s employing a two-loop autopilot with consideration for the radome aberration parasitic feedback loop
作者:
Duo Zheng
a
;
zhengduohello@126.com
;
Defu Lin
a
;
Jiang Wang
a
;
Xinghua Xu
b
关键词:
Dynamic stability
;
Two-loop autopilot
;
Cross coupling
;
Radome aberration
;
Parasitic feedback
刊名:Aerospace Science and Technology
出版年:2017
3.
An integrated guidance and control approach in three-dimensional space for hypersonic
missile
constrained by impact angles
作者:
Xiaodong Liu
;
k.start@163.com
;
Wanwei Huang
wwhuang@163.com
;
Lifu Du
dulifu0328@163.com
关键词:
Dynamic surface control
;
Dynamic inversion control
;
Integrated guidance and control
;
Nonlinear control
;
Robust control
刊名:ISA Transactions
出版年:2017
4.
A preliminary study on the local impact behavior of Steel-plate Concrete walls
作者:
Kap-sun Kim
a
;
kapskim11@khnp.co.kr
;
Il-hwan Moon
b
;
Hyung-jin Choi
c
;
Deok-woo Nam
a
关键词:
Missile
impact
;
Impact test
;
Numerical simulation
;
Local impact behavior
;
Steel-plate Concrete walls(SC walls)
刊名:Annals of Nuclear Energy
出版年:2017
5.
Explicit hidden coupling terms handling in gain-scheduling control design via eigenstructure assignment
作者:
H. Lhachemi
;
hugo.lhachemi@polymtl.ca
;
D. Saussié
;
d.saussie@polymtl.ca
;
G. Zhu
guchuan.zhu@polymtl.ca
关键词:
Hidden coupling terms
;
Gain-scheduling
;
Eigenstructure assignment
;
Missile
autopilot
刊名:Control Engineering Practice
出版年:2017
6.
Adaptive Backstepping Autopilot Design for
Missile
s of Fast Time-varying Velocity
作者:
Seokwon Lee
*
;
blueswl@snu.ac.kr" class="auth_mail" title="E-mail the corresponding author
;
Youdan Kim
**
;
ydkim@snu.ac.kr" class="auth_mail" title="E-mail the corresponding author
;
Guanyoung Moon
***
;
rootlocy@daum.net" class="auth_mail" title="E-mail the corresponding author
;
Byung-Eul Jun
****
;
mountrees@gmail.com" class="auth_mail" title="E-mail the corresponding author
关键词:
Missile
Autopilot
;
Adaptive Control
;
Fin-controlled
Missile
;
Backstepping
刊名:IFAC-PapersOnLine
出版年:2016
7.
Obstacle avoidance for multi-
missile
network via distributed coordination algorithm
作者:
Jiang Zhao
;
jzhao@buaa.edu.cn" class="auth_mail" title="E-mail the corresponding author
Author Vitae
;
Rui Zhou
zhr@buaa.edu.cn" class="auth_mail" title="E-mail the corresponding author
Author Vitae
关键词:
Cooperative guidance
;
Distributed algorithms
;
Impact time
;
Missile
guidance
;
Multiple
missile
s
;
Obstacle avoidance
;
Proportional navigation
刊名:Chinese Journal of Aeronautics
出版年:2016
8.
Rapid Structure Design and Automated Adjustment of
Missile
Body
作者:
Jixing Li
;
Tao Ning
;
li_jixing@buaa.edu.cn" class="auth_mail" title="E-mail the corresponding author
;
Ping Xi
;
Tian Wang
关键词:
preliminary design
;
missile
body structure
;
parametric design
;
automated adjustment
刊名:Procedia CIRP
出版年:2016
9.
A new cruise
missile
path tracking method based on second-order smoothing
作者:
Yang-Wang Fang
a
;
ywfang2008@sohu.com" class="auth_mail" title="E-mail the corresponding author
;
Dong-Dong Qiao
a
;
suifeng103@126.com" class="auth_mail" title="E-mail the corresponding author
;
Lei Zhang
a
;
szl1985@163.com" class="auth_mail" title="E-mail the corresponding author
;
Peng-Fei Yang
a
;
pfyang1988@126.com" class="auth_mail" title="E-mail the corresponding author
;
Wei-Shi Peng
a
;
b
;
peng_weishi@163.com" class="auth_mail" title="E-mail the corresponding author
关键词:
Path tracking
;
Path smoothing
;
Cruise
missile
;
Symmetrical polar polynomial curve
刊名:Optik - International Journal for Light and Electron Optics
出版年:2016
10.
Roll-pitch-yaw autopilot design for nonlinear time-varying
missile
using partial state observer based global fast terminal sliding mode control
作者:
Ahmed AwadAuthor Vitae
;
Haoping Wang
;
hp.wang@njust.edu.cn" class="auth_mail" title="E-mail the corresponding author
Author Vitae
关键词:
Flight control system
;
Global fast terminal sliding mode control
;
Integrated autopilot
;
Nonlinear state observer
;
Skid-to-turn
missile
刊名:Chinese Journal of Aeronautics
出版年:2016
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