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长春光学精密机械与物... [9]
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期刊论文 [6]
会议论文 [2]
学位论文 [1]
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2022 [1]
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专题:长春光学精密机械与物理研究所
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Numerical and Experimental Study on Vertical Takeoff and Separation of the Compound Aircraft
期刊论文
Ieee Access, 2022, 卷号: 10, 页码: 47597-47617
作者:
D. Wang
;
Q. Z. Hong
;
X. Huang
;
X. B. Pei and J. Wang
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浏览/下载:0/0
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提交时间:2023/06/14
Research on the Multiagent Joint Proximal Policy Optimization Algorithm Controlling Cooperative Fixed-Wing UAV Obstacle Avoidance
期刊论文
Sensors, 2020, 卷号: 20, 期号: 16, 页码: 16
作者:
W. W. Zhao,H. R. Chu,X. K. Miao,L. H. Guo,H. H. Shen,C. H. Zhu,F. Zhang and D. X. Liang
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浏览/下载:4/0
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提交时间:2021/07/06
Flocking Control of Fixed-Wing UAVs With Cooperative Obstacle Avoidance Capability
期刊论文
Ieee Access, 2019, 卷号: 7, 页码: 17798-17808
作者:
W.W.Zhao
;
H.R.Chu
;
M.Y.Zhang
;
T.T.Sun
;
L.H.Guo
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浏览/下载:2/0
  |  
提交时间:2020/08/24
Fixed-wing UAV swarm,multi-agent system,flocking control,cooperative,obstacle avoidance,consensus,local information communication,multiagent systems,behaviors,algorithm,consensus,Computer Science,Engineering,Telecommunications
Adaptive internal model control research in autonomous landing phase for a fixed-wing UAV
期刊论文
CEAS Aeronautical Journal, 2017, 卷号: 8, 期号: 1
作者:
Gao, J.-z. and H.-g. Jia
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浏览/下载:17/0
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提交时间:2018/06/13
Design of longitudinal control law for small fixed-wing UAV during auto landing
期刊论文
Guangxue Jingmi Gongcheng/Optics and Precision Engineering, 2016, 卷号: 24, 期号: 7
作者:
Gao, J.-Z. and H.-G. Jia
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浏览/下载:10/0
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提交时间:2017/09/11
无人机飞行控制系统若干关键技术研究
学位论文
博士: 中国科学院大学, 2014
段镇
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浏览/下载:275/0
  |  
提交时间:2014/08/21
Review and analysis of avionic helmet-mounted displays
期刊论文
Optical Engineering, 2013, 卷号: 52, 期号: 11
作者:
Zhang X.
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浏览/下载:21/0
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提交时间:2014/05/14
Longitudinal control law design and simulation of fixed-wing UAV (EI CONFERENCE)
会议论文
2012 International Conference on Measurement, Instrumentation and Automation, ICMIA 2012, September 15, 2012 - September 16, 2012, Guangzhou, China
Duan Z.
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浏览/下载:19/0
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提交时间:2013/03/25
Taken some fixed-wing UAV as the study object
the aircraft movement was broken down into the longitudinal movement and lateral movement according to the linearized small perturbation principle
the longitudinal control law design method was discussed using root locus which belonged to classical control theory. The six degrees of freedom nonlinear model simulation result shows that: the control parameters designed are reasonable
the simulation profile is fully consistent with the setting profile
the control effect of pitch angle loop and altitude loop meets with the indices requirements
the method is mature and reliable
easy to realize in engineering. (2013) Trans Tech Publications
Switzerland.
Longitudinal control law design and simulation of fixed-wing UAV
会议论文
2012 International Conference on Measurement, Instrumentation and Automation, ICMIA 2012, September 15, 2012 - September 16, 2012, Guangzhou, China, September 15, 2012 - September 16, 2012
Duan Z.
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浏览/下载:15/0
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提交时间:2014/05/15
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