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安徽大学 [2]
厦门大学 [1]
长春光学精密机械与物... [1]
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期刊论文 [3]
会议论文 [1]
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2014 [3]
2010 [1]
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On Some Classes of Sequential Spiking Neural P Systems
期刊论文
http://dx.doi.org/10.1162/NECO_a_00580, 2014
Zhang, Xingyi
;
Zeng, Xiangxiang
;
Luo, Bin
;
Pan, Linqiang
;
曾湘祥
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浏览/下载:4/0
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提交时间:2015/07/22
EXHAUSTIVE USE
RULES
LANGUAGES
On Some Classes of Sequential Spiking Neural P Systems
期刊论文
Neural Computation, 2014, 卷号: Vol.26 No.5, 页码: 974-997
作者:
Zhang,Xingyi
;
Pan,Linqiang
;
Zeng,Xiangxiang
;
Luo,Bin
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浏览/下载:3/0
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提交时间:2019/04/22
EXHAUSTIVE USE
RULES
LANGUAGES
Spiking Neural P Systems with a Generalized Use of Rules
期刊论文
Neural Computation, 2014, 卷号: Vol.26 No.12, 页码: 2925-2943
作者:
Zhang,Xingyi
;
Pan,Linqiang
;
Wang,Bangju
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浏览/下载:2/0
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提交时间:2019/04/22
EXHAUSTIVE USE
LANGUAGES
The method on the measurement of the aircraft attitude by the spatial cosines relationship of the single station and planes to the intersection the multi-station of electro-optical theodolite (EI CONFERENCE)
会议论文
2010 International Conference on Computer, Mechatronics, Control and Electronic Engineering, CMCE 2010, August 24, 2010 - August 26, 2010, Changchun, China
Zhao L.-R.
;
Cao Y.-G.
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浏览/下载:16/0
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提交时间:2013/03/25
In order to realize the aircraft attitude measurement
The paper advances electro-optical theodolite methods of measuring the aircraft attitude by using the spatial cosines relationship the single station theodolite and how to use intersection of the multi-station theodolite. The single station theodolite was introduced in a measured distance from the aircraft posture information. An exhaustive approach was used to access to the aircraft axis of the feature points and the location in the space was used to obtain space posture parameters. The multi-station theodolite was introduced to get the information of the aircraft flight attitude by method of using planes to the intersection. Two-dimensional image to obtain objective axis by fitting algorithm using Hough transform. And then
Calculate the vertical distance of the origin to the target of the central axis and the origin to the target of the central axis of the angle between the normal and the X-axis obtaining the linear equation in the two-dimensional plane. Two-dimensional axis of the target image and the camera system's optical center only identified a space plane. The aircraft yaw axis angle and pitch angle can be obtained by getting the space axis using plains to the intersection method. Experimental results show that attitude angle error of the single station theodolite is less than 1 when its distance is less than 6000m and attitude angle error of the multi-station theodolite is less than 0.6 when its intersection angle is between 30 and 150. In this paper
according to test result of precision comparing the mathematical model is correct and the algorithm is reasonable in extracting effective parameters of the aircraft's attitude. 2010 IEEE.
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