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西安交通大学 [1]
北京航空航天大学 [1]
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Seeker-Azimuth Determination with Gyro Rotor and Optoelectronic Sensors
期刊论文
SENSORS, 2018, 卷号: 18, 期号: 4
作者:
Bai, Jian-Ming
;
Zhao, Guangshe
;
Rong, Hai-Jun
;
Wang, Xianhua
;
Rong, Hai-Jun (hjrong@mail.xjtu.edu.cn)
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浏览/下载:31/0
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提交时间:2018/05/08
Seeker Azimuth
Gyro Rotor
Optoelectronic Sensors
Duty Ratio
Seeker-Azimuth Determination with Gyro Rotor and Optoelectronic Sensors
期刊论文
SENSORS, 2018, 卷号: 18
作者:
Bai, Jian-Ming
;
Zhao, Guangshe
;
Rong, Hai-Jun
;
Wang, Xianhua
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  |  
浏览/下载:2/0
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提交时间:2019/11/26
duty ratio
gyro rotor
optoelectronic sensors
seeker azimuth
Design and Implementation of FOG Based Gyrocompass
会议论文
8tth IEEE/IACSIT/SCIEI International Conference on Optimization of the Intelligent Systems and Their Applications in Aerospace, Robotics, Mechanical Engineering, Manufacturing Systems, Biomechatornics and Neurorehabilitation (OPTIROB), ROMANIA, 2014-01-01
作者:
Abbas, Aqeel
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浏览/下载:2/0
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提交时间:2020/01/06
Gyrocompass
North finding
North seeker
FOG
Azimuth
Pre-launch alignment
Analysis of zenith pass problem in a roll-pitch optics seeker (EI CONFERENCE)
会议论文
2011 International Conference on Electronics and Optoelectronics, ICEOE 2011, July 29, 2011 - July 31, 2011, Dalian, China
Jiang H.
;
Jia H.
;
Wei Q.
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提交时间:2013/03/25
There are mainly two kind of structures for a missile two-axes seeker
which is always mentioned as elevate-azimuth and roll-pitch. The elevate-azimuth structured seeker has been studied for a long time
and it is applied in all sort of missiles. Not only structure design but also control algorithm of the elevate-azimuth seeker are deeply developed. But for elevate-azimuth seeker there are several disadvantages such as big size and large abaxial angle blind. So the elevate-azimuth seeker gimbal angle is designed up to 65 according to relative references. In modern air war
it is important for a missile to have the ability of "first recognize" and "first attack". That means the air to air missile seeker is required to be a system with large gimbal angle and large abaxial launch angle. With the mentioned requirement
roll-pitch seeker with its advantages smart size and large gimbal angle is studied widely and deeply. The pitch angle of roll-pitch is up to 90 while its roll angle up to n 360. But there are also some disadvantages for the roll-pitch seeker
the most troublesome one is the zenith pass problem. The zenith pass problem is brought about from the gimbal kinematics
it is said that when target moves in the center of image plane
roll servo command gotten from the kinematics algorithm will go to infinite. Math model of zenith pass problem is proposed in this paper and two ways to solve the problem are brought forward. 2011 IEEE.
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