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浏览/检索结果:
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Missile guidance with assisted deep reinforcement learning for head-on interception of maneuvering target
期刊论文
COMPLEX & INTELLIGENT SYSTEMS, 2021, 页码: 12
作者:
Li, Weifan
;
Zhu, Yuanheng
;
Zhao, Dongbin
收藏
  |  
浏览/下载:41/0
  |  
提交时间:2021/12/28
Reinforcement learning
Missile guidance
Auxiliary learning
Self-imitation learning
Optimal interception strategy of air defence missile system considering multiple targets and phases
期刊论文
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART O-JOURNAL OF RISK AND RELIABILITY, 2021, 页码: 10
作者:
Gao, Kaiye
;
Xiao, Hui
;
Qu, Li
;
Wang, Shouyang
收藏
  |  
浏览/下载:21/0
  |  
提交时间:2021/10/26
Interception strategy
reliability
combinatorial optimization
missile-target defence
Weighting by Cross-Validation: A Calibration Method for Force Measurements via Transient Response Analysis
期刊论文
EXPERIMENTAL TECHNIQUES, 2019, 卷号: 43, 期号: 4, 页码: 469-478
作者:
Luo ZT(罗长童)
;
Wang YP(汪运鹏)
;
Hu ZM(胡宗民)
;
Li JP(李进平)
;
Jiang ZL(姜宗林)
收藏
  |  
浏览/下载:75/0
  |  
提交时间:2019/10/21
Aerodynamic force measurement
Dynamic system
Impact response
Cross-validation
System identification
Terminal Guidance Based on Bezier Curve for Climb-and-Dive Maneuvering Trajectory With Impact Angle Constraint
期刊论文
IEEE ACCESS, 2019, 卷号: 7, 页码: 2969-2977
作者:
Qin, Zhen
;
Qi, Xiaoye
;
Fu, Yongling
收藏
  |  
浏览/下载:11/0
  |  
提交时间:2019/12/30
Cruise missile
terminal guidance
maneuvering trajectory
impact angle
Bezier curve
Three-Dimensional Impact Time and Angle Control Guidance Based on MPSP
期刊论文
INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING, 2019, 卷号: 2019
作者:
Li, Yang
;
Zhou, Hao
;
Chen, Wanchun
收藏
  |  
浏览/下载:11/0
  |  
提交时间:2019/12/30
Air navigation
Air to surface missiles
Electronic guidance systems
Air to ground missile
Control saturation constraints
Flight path angle
Initial conditions
Model predictive
Nonlinear guidance laws
Static programming
Terminal impact angles
Guided missiles
Learning to Guide: Guidance Law Based on Deep Meta-Learning and Model Predictive Path Integral Control
期刊论文
IEEE ACCESS, 2019, 卷号: 7, 页码: 47353-47365
作者:
Liang, Chen
;
Wang, Weihong
;
Liu, Zhenghua
;
Lai, Chao
;
Zhou, Benchun
收藏
  |  
浏览/下载:4/0
  |  
提交时间:2019/12/30
Missile guidance
model predictive control
meta-learning
deep reinforcement learning
impact angle constraint
Autopilot and guidance law design considering impact angle and time
期刊论文
IET CONTROL THEORY AND APPLICATIONS, 2018, 卷号: 12, 期号: 2, 页码: 221-232
作者:
Wang, Xianghua
;
Tan, Chee Pin
;
Zhou, Donghua
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  |  
浏览/下载:5/0
  |  
提交时间:2019/12/11
missile control
impact (mechanical)
autopilot
guidance law design
impact angle
impact time
missile flight
missile LOS angle
missile
line-of-sight angle
Three-dimensional guidance method for air to ground missile with impact time constraint
会议论文
2018 37TH CHINESE CONTROL CONFERENCE (CCC), 2018-01-01
作者:
Guo, Dong
;
Jiang, Peng
;
Liang, Zixuan
;
Ren, Zhang
收藏
  |  
浏览/下载:5/0
  |  
提交时间:2019/12/30
air-to-ground missile
guidance law
time constraint
sliding mode control
salvo attack
Sliding Mode Guidance Law Considering Missile Dynamic Characteristics and Impact Angle Constraints
期刊论文
International Journal of Automation and Computing, 2018, 卷号: 15, 期号: 2, 页码: 218-227
作者:
Hui-Bo Zhou
;
Jun-Hong Song
;
Shen-Min Song
收藏
  |  
浏览/下载:10/0
  |  
提交时间:2021/02/23
Autopilot
impact angle
nonsingular terminal sliding mode
finite-time convergent
guidance.
Simultaneous attack of a stationary target using multiple missiles: a consensus-based approach
期刊论文
SCIENCE CHINA-INFORMATION SCIENCES, 2017
Zhou, Jialing
;
Yang, Jianying
;
Li, Zhongkui
收藏
  |  
浏览/下载:4/0
  |  
提交时间:2017/12/03
simultaneous attack
consensus problem
cooperative control
distributed control
guidance low design
MULTIAGENT SYSTEMS
IMPACT-TIME
GUIDANCE LAW
SLIDING MODE
TRACKING
ANGLE
DYNAMICS
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