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在“
Elsevier电子期刊
”中,
命中:
119
条,耗时:0.0649385 秒
在所有数据库中总计命中:
2,051
条
1.
Robust
autopilot
design
for bank-to-turn missiles 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 missiles
;
Autopilot
design
;
External disturbances
刊名:Optik - International Journal for Light and Electron Optics
出版年:2017
2.
Sigmoid function based integral-derivative observer and application to
autopilot
design
作者:
Xingling Shao
a
;
b
;
huanying3557913@sina.com" class="auth_mail" title="E-mail the corresponding author
;
Honglun Wang
c
;
d
;
Jun Liu
a
;
b
;
Jun Tang
a
;
b
;
Jie Li
a
;
b
;
Xiaoming Zhang
a
;
b
;
Chong Shen
a
;
b
关键词:
Sigmoid function
;
Integral-derivative observer
;
Drift phenomena
;
Chattering effect
;
Singular perturbation
;
Describing function
;
Autopilot
design
刊名:Mechanical Systems and Signal Processing
出版年:2017
3.
Augmented nonlinear differentiator
design
作者:
Xingling Shao
;
shaoxl@nuc.edu.cn
;
Jun Liu
;
Wei Yang
;
Jun Tang
;
Jie Li
关键词:
Augmented nonlinear differentiator (AND)
;
Noisy measurement
;
Noise-tolerance capability
;
Describing function
;
Autopilot
design
;
Displacement following
刊名:Mechanical Systems and Signal Processing
出版年:2017
4.
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
5.
Dynamic stability of rolling missiles 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
6.
Model reference adaptive
autopilot
with anti-windup compensator for an autonomous underwater vehicle:
Design
and hardware in the loop implementation results
作者:
Pouria Sarhadi
;
Abolfazl Ranjbar Noei
;
Alireza Khosravi
;
akhosravi@nit.ac.ir
关键词:
Model reference adaptive control
;
Six degrees of freedom simulation
;
Input saturation
;
Anti-windup compensator
;
Hardware in the loop simulation
;
AUV
刊名:Applied Ocean Research
出版年:2017
7.
Lévy flight based pigeon-inspired optimization for control parameters optimization in automatic carrier landing system
作者:
Rui Dou
;
Haibin Duan
;
hbduan@buaa.edu.cn
关键词:
Carrier landing
;
Automatic carrier landing system (ACLS)
;
Pigeon inspired optimization (PIO)
;
Lé
;
vy flight
刊名:Aerospace Science and Technology
出版年:2017
8.
Control Loss Recovery
Autopilot
Design
for Fixed-Wing Aircraft
作者:
Şeyma Akyü
;
rek
*
;
seymaakyurek@gmail.com" class="auth_mail" title="E-mail the corresponding author
;
Burak Kü
;
rkç
;
ü
;
*
;
kurkcub@gmail.com" class="auth_mail" title="E-mail the corresponding author
;
Ü
;
nver Kaynak
*
;
unkaynak@gmail.com" class="auth_mail" title="E-mail the corresponding author
;
Coşku Kasnakoğlu
*
;
kasnakoglu@gmail.com" class="auth_mail" title="E-mail the corresponding author
关键词:
Loop-shaping
;
loss of control
;
surface jam
;
power loss
;
autopilot
design
;
numerical simulation
刊名:IFAC-PapersOnLine
出版年:2016
9.
Novel two phase algorithm to
design
three loop
autopilot
using parameter plane technique and particle swarm optimization
作者:
Siddhardha Kedarisetty
siddhardhak2010@gmail.com" class="auth_mail" title="E-mail the corresponding author
关键词:
Lateral acceleration
autopilot
;
Parameter plane technique
;
Particle swarm optimization
刊名:IFAC-PapersOnLine
出版年:2016
10.
Optimization of three-loop missile
autopilot
gain under crossover frequency constraint
作者:
M.A. Abd-elatif
;
Mdyosf2010@yahoo.com" class="auth_mail" title="E-mail the corresponding author
;
Long-jun Qian
;
Yu-ming Bo
关键词:
Three-loop missile
autopilot
;
Optimal gain
design
;
Crossover frequency constraint
;
Performance optimization
刊名:Defence Technology
出版年:2016
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