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西安交通大学 [4]
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Research on the Dynamic Control Method of CFETR Multi-Purpose Overload Robot
期刊论文
APPLIED SCIENCES-BASEL, 2023, 卷号: 13
作者:
Zuo, Congju
;
Qin, Guodong
;
Pan, Hongtao
;
Xia, Liang
;
Wang, Feng
收藏
  |  
浏览/下载:21/0
  |  
提交时间:2023/11/10
CFETR
multi-purpose overload robot
sliding mode controller
error compensation
rigid-flexible control
Optimal Transmission Overloads Mitigation Following Disturbances in Power Systems
期刊论文
IEEE Transactions on Industrial Informatics, 2019, 卷号: Vol.15 No.5, 页码: 2592-2604
作者:
Liang Che
;
Xuan Liu
;
Zhikang Shuai
收藏
  |  
浏览/下载:9/0
  |  
提交时间:2019/12/13
Security
Tools
Automatic generation control
Power system faults
Power system protection
Load modeling
Transient analysis
Emergency control
generation redispatch
load shedding (LS)
overload mitigation
Optimal Transmission Overloads Mitigation Following Disturbances in Power Systems
期刊论文
IEEE TRANSACTIONS ON INDUSTRIAL INFORMATICS, 2019, 卷号: Vol.15 No.5, 页码: 2592-2604
作者:
Che, L
;
Liu, X
;
Shuai, ZK
收藏
  |  
浏览/下载:10/0
  |  
提交时间:2019/12/17
Emergency control
generation redispatch
load shedding (LS)
overload mitigation
Optimal Transmission Overloads Mitigation Following Disturbances in Power Systems
期刊论文
IEEE TRANSACTIONS ON INDUSTRIAL INFORMATICS, 2019, 卷号: Vol.15 No.5, 页码: 2592-2604
作者:
Che, L
;
Liu, X
;
Shuai, ZK
收藏
  |  
浏览/下载:4/0
  |  
提交时间:2019/12/17
Emergency control
generation redispatch
load shedding (LS)
overload mitigation
Alleviation of post-contingency overloads by SOCP based corrective control considering TCSC and MTDC
期刊论文
IET GENERATION TRANSMISSION & DISTRIBUTION, 2018, 卷号: 12, 期号: 9
作者:
Bi, Ruyu
;
Lin, Tao
;
Chen, Rusi
;
Ye, Jing
;
Zhou, Xueming
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  |  
浏览/下载:5/0
  |  
提交时间:2019/12/05
DC power transmission
thyristor applications
mathematical programming
minimisation
flexible AC transmission systems
failure analysis
power generation reliability
power transmission reliability
power generation scheduling
renewable energy sources
search problems
pattern clustering
load shedding
load flow
power transmission control
power generation control
post-contingency overload alleviation
SOCP based corrective control
TCSC
MTDC
high-voltage direct current device
flexible AC transmission system
smart grid
cascading failures
DC blocking
post-contingency corrective control
large-scale renewable energy generation integration
artificial intelligence optimisation-based method
second-order cone programming CC optimisation model
SOCP-based CC optimisation model
meshed AC-DC power systems
optimisation variables
OV
heuristic search method
sensitivity index
clustering algorithm
overloaded lines
thyristor controlled series capacitor compensation levels
multiterminal direct current power
load shedding minimisation
generation rescheduling minimisation
power flow equations
computational efficiency
IEEE 30-bus test system
line outage
Coordination of DC power flow controllers and AC/DC converters on optimising the delivery of wind power
期刊论文
IET RENEWABLE POWER GENERATION, 2016, 卷号: 10, 页码: 815-823
作者:
Wang, Sheng
;
Guo, Jingli
;
Li, Chuanyue
;
Balasubramaniam, Senthooran
;
Zheng, Rui
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  |  
浏览/下载:3/0
  |  
提交时间:2019/11/26
power loss reduction
offshore wind power generation
offshore installations
wind power curtailment amount reduction
DC grids
power grids
offshore DC transmission system overload
AC-DC power convertors
DC power flow controller coordination
wind power plants
power transmission control
DC-PFC
load flow control
AC-DC converter coordination
power generation control
wind power delivery optimization
Dynamic RACH Partition for Massive Access of Differentiated M2M Services
期刊论文
SENSORS, 2016, 卷号: 16, 期号: [db:dc_citation_issue]
作者:
Du, Qinghe
;
Li, Wanyu
;
Liu, Lingjia
;
Ren, Pinyi
;
Wang, Yichen
收藏
  |  
浏览/下载:2/0
  |  
提交时间:2019/12/02
access success probability
overload control
average access delay
M2M communications
preamble partition
Dynamic Allocation of RACH Resource for Clustered M2M Communications in LTE Networks
会议论文
作者:
Li, Wanyu
;
Du, Qinghe
;
Liu, Lingjia
;
Ren, Pinyi
;
Wang, Yichen
收藏
  |  
浏览/下载:2/0
  |  
提交时间:2019/12/02
overload control
M2M communications
RACH
ACB scheme
The aircraft autopilot design of parameters changing in a wide range (EI CONFERENCE)
会议论文
2011 International Conference on Electric Information and Control Engineering, ICEICE 2011, April 15, 2011 - April 17, 2011, Wuhan, China
Zhen D.
;
Yue Z.
收藏
  |  
浏览/下载:20/0
  |  
提交时间:2013/03/25
Autopilot is an important part of aircraft
Under the action of the disturbance torque
for the flight parameters of aircraft Changing in a wide range
the range was about 16km
on the basic of analyzing the typical trajectory
the max height was about 5100m
the trajectory of feature points were selected
the deviation of lateral was about 12m
taking pitch control loop for example
the maximum angle of attack was about 3.6
a sub- PID autopilot was designed using classical control theory
the maximum elevator deflection was less than 5
using single-mode Transient suppression method
the maximum aileron deflection was less than 2
the overload due to control surface transition deflection was avoided when control parameters changing
the maximum roll was less than 5
the verification was done by non-linear simulation. The result showed that: the phase margin of autopilot was greater than 30
the response of overload can accurately track the given overload instruction. An autopilot design method of aircraft of parameter changes in a wide range was provided. 2011 IEEE.
the bandwidth was more than 14rad / s
the settling time was less than 0.7s
the maximum overshoot was 23.3%
Control method research on wide flight envelope aerocraft (EI CONFERENCE)
会议论文
2nd Annual Conference on Electrical and Control Engineering, ICECE 2011, September 16, 2011 - September 18, 2011, Yichang, China
Duan Z.
收藏
  |  
浏览/下载:19/0
  |  
提交时间:2013/03/25
The flying qualities of aerocraft was directly effected by the autopilot
for the wide flight envelope aerocraft
on the basic of analyzing the typical trajectory
the three loop autopilots of roll stability
pitch and yaw were designed
using single-mode Transient suppression method
the overload due to control surface transition deflection was avoided when control parameters changing
the verification was done by non-linear simulation. The result showed that: Under the action of the disturbance torque
the maximum roll was less than 5
the range of the aerocraft was from 13.5km to 22.4km
the max height was about 5100m
the max deviation of lateral was about 42m
the maximum elevator deflection was less than 6.5 the control law was applicable within the effective range. An autopilot design method of wide flight envelope aerocraft was provided. 2011 IEEE.
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