机载光电平台自主引导精度分析

王增发; 孙丽娜; 李刚; 张建华

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机载光电平台自主引导精度分析

王增发, 孙丽娜, 李刚, 张建华

文章导航 > 红外与激光工程 > 2014 > 43(11): 3585-3591

王增发, 孙丽娜, 李刚, 张建华. 机载光电平台自主引导精度分析[J]. 红外与激光工程, 2014, 43(11): 3585-3591.

引用本文:

王增发, 孙丽娜, 李刚, 张建华. 机载光电平台自主引导精度分析[J]. 红外与激光工程, 2014, 43(11): 3585-3591.

Wang Zengfa, Sun Lina, Li Gang, Zhang Jianhua. Accuracy analysis on autonomous guiding of airborne opto-electronic platform[J]. Infrared and Laser Engineering, 2014, 43(11): 3585-3591.

Citation:

Wang Zengfa, Sun Lina, Li Gang, Zhang Jianhua. Accuracy analysis on autonomous guiding of airborne opto-electronic platform[J]. Infrared and Laser Engineering, 2014, 43(11): 3585-3591.

机载光电平台自主引导精度分析

1.
中国科学院长春光学精密机械与物理研究所航空光学成像与测量重点实验室,吉林长春 130033

基金项目:

国家高科技研究发展计划(2008AA121803)

详细信息

作者简介:
王增发(1980-),男,助理研究员,主要从事航空成像测量技术方面的研究.Email:erwin1023@163.com

中图分类号: TP273

Accuracy analysis on autonomous guiding of airborne opto-electronic platform

1.
Key Laboratory of Airborne Optical Imaging and Measurement,Changchun Institute of Optics,Fine Mechanics and Physics,Chinese Academy of Sciences,Changchun 130033,China

摘要: 航空侦察是为获取敌情、地形和有关作战情报而采取的重要手段,各种电磁信号侦察、光电信号侦察在同一飞机平台的应用越来越广泛,电磁信号侦察以及地面其他系统发现目标后,通过目标的位置信息引导光电侦察系统对目标进行搜索、跟踪、查证的应用也越来越多.当机载光电平台接收到目标的坐标值后,自行接收GPS和惯导信息,并实时解算出被测目标在光电平台坐标系下的方位角和俯仰角,引导目标进入光学载荷视场内,并用图像视频跟踪的方法捕获和跟踪目标.针对飞机平台对地面固定目标或者运动目标的引导进行研究,将目标点坐标从大地坐标系转换到光电平台载机坐标系,并建立自主引导测量方程,利用蒙特卡罗统计的方法分析自主引导测量方程中各个误差因素对最终引导精度的影响,针对如何提高引导精度提出了一些建议.并在某光电平台上进行飞行试验验证,目标均能很好地进入跟踪视场内,完成捕获、跟踪功能.
- 光电平台 /
- 自主引导 /
- 蒙特卡罗 /
- 坐标转换
Abstract: Aerial reconnaissance is an important means to obtain information, terrain and other relevant intelligence of the enemy. Various of electromagnetic and photoelectric signals used in the same aircraft platform are more widely. When the target is found by other reconnaissance means, it needs the position information of the target of the photoelectric reconnaissance system to search, track and verificate. When the photoelectric platform receives the coordinates of the target value, and the GPS and inertial navigation information of the airplane, the azimuth and elevation of the measured target are calculated real-timely. The platform guides target into the optical payload field, and tracks the target using the image tracking video. This paper studied the methods to guide the opto-electronic platform to trace the fixed targets or moving targets on the ground, which established the automatic guiding measurement equation, to translate the target coordinates from geodetic coordinate to the opto-electronic platform coordinate system. To analyze the each factors in automatic guiding measurement equation, using Monte Carlo statistical method, and find how each factors error in measurement equation to affect the precision of the final guidance, in order to improve the guiding precision puts forward some suggestions, the target can be well guided into the track field in a flight test.
- photoelectric platform /
- automatic guiding /
- Monte Carlo /
- coordinate transformation

[1]	Ma Jiaguang, Tang Tao. Review of compound axis servo mechanism tracking control technology[J]. Infrared and Laser Engineering, 2013, 42(1): 218-226. (in Chinese) 马佳光, 唐涛. 复合轴精密跟踪技术的应用与发展[J]. 红外与激光工程, 2013, 42(1): 218-226.
[2]
[3]	Zhang Bao, Yao Junfeng, Gao Limin. Measuring orientation technology based on airborne GPS[J]. Optics and Precision Engineering, 2009, 17(1): 172-178. (in Chinese) 张葆, 姚俊峰, 高利民. 机载GPS测量定位技术研究[J]. 光学精密工程, 2009, 17(1): 172-178.
[4]
[5]
[6]	Miller Michael D, Drummond Oliver E. Comparison of methodologies for mitigating coordinate transformation bias in target tracking[C]//SPIE, 2000, 4048: 414-427.
[7]
[8]	James Underwood, Andrew Hill, Steve Scheding. Calibration of range sensor pose on mobile platforms[C]//Proceedings of the 2007 IEEE/RSJ International Conference on Intelligent Robots and Systems, 2007: 3866-3871.
[9]
[10]	Yavin G. Airborne reconnaissance system: US, 7136726[P]. 2006-11-14.
[11]
[12]	Wang Jing, Gao Limin, Yao Junfeng. Analysis on coordinate conversion error of airborne measuring device[J]. Optics and Precision Engineering, 2009, 17(2): 388-394. (in Chinese) 王晶, 高利民, 姚俊峰. 机载测量平台中的坐标转换误差分析[J]. 光学精密工程, 2009, 17(2): 388-394.
[13]
[14]	Wang Jiaqi, Jin Guang, Yan Changxiang. Orientation error analysis of airborne opto-electric tracking and measuring device[J]. Optics and Precision Engineering, 2009, 17(2): 388-394. (in Chinese) 王家骐, 金光, 颜昌翔. 机载光电跟踪测量设备的目标定位误差分析[J]. 光学精密工程, 2009, 17(2): 388-394.
[15]
[16]	Chen Wenjian, Ji Ming, Zhang Jianfeng, et al. Electro-optical pod inertial orientation during geographic tracking[J]. Journal of Applied Optic, 2009, 28(6): 675-679. (in Chinese) 陈文建, 纪明, 张建峰, 等. 地理跟踪过程中光电吊仓惯性定位技术研究[J]. 应用光学, 2009, 28(6): 675-679.
[17]	Wang Dezhou, Li Yaomin. Design of radar guidance system based on GPS[J]. Computer Measurement Control, 2013, 21(1): 139-141. (in Chinese) 王德周, 李耀民. 基于GPS技术辅助雷达引导系统设计[J]. 计算机测量与控制, 2013, 21(1): 139-141.

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机载光电平台自主引导精度分析

1. 中国科学院长春光学精密机械与物理研究所航空光学成像与测量重点实验室,吉林长春 130033

作者简介:
王增发(1980-),男,助理研究员,主要从事航空成像测量技术方面的研究.Email:erwin1023@163.com

收稿日期: 2014-03-11
修回日期: 2014-04-20
刊出日期: 2014-11-25

基金项目:

国家高科技研究发展计划(2008AA121803)

中图分类号: TP273

关键词:

摘要: 航空侦察是为获取敌情、地形和有关作战情报而采取的重要手段,各种电磁信号侦察、光电信号侦察在同一飞机平台的应用越来越广泛,电磁信号侦察以及地面其他系统发现目标后,通过目标的位置信息引导光电侦察系统对目标进行搜索、跟踪、查证的应用也越来越多.当机载光电平台接收到目标的坐标值后,自行接收GPS和惯导信息,并实时解算出被测目标在光电平台坐标系下的方位角和俯仰角,引导目标进入光学载荷视场内,并用图像视频跟踪的方法捕获和跟踪目标.针对飞机平台对地面固定目标或者运动目标的引导进行研究,将目标点坐标从大地坐标系转换到光电平台载机坐标系,并建立自主引导测量方程,利用蒙特卡罗统计的方法分析自主引导测量方程中各个误差因素对最终引导精度的影响,针对如何提高引导精度提出了一些建议.并在某光电平台上进行飞行试验验证,目标均能很好地进入跟踪视场内,完成捕获、跟踪功能.

English Abstract

Accuracy analysis on autonomous guiding of airborne opto-electronic platform

1. Key Laboratory of Airborne Optical Imaging and Measurement,Changchun Institute of Optics,Fine Mechanics and Physics,Chinese Academy of Sciences,Changchun 130033,China

Received Date: 2014-03-11
Rev Recd Date: 2014-04-20
Publish Date: 2014-11-25

Keywords:

Abstract: Aerial reconnaissance is an important means to obtain information, terrain and other relevant intelligence of the enemy. Various of electromagnetic and photoelectric signals used in the same aircraft platform are more widely. When the target is found by other reconnaissance means, it needs the position information of the target of the photoelectric reconnaissance system to search, track and verificate. When the photoelectric platform receives the coordinates of the target value, and the GPS and inertial navigation information of the airplane, the azimuth and elevation of the measured target are calculated real-timely. The platform guides target into the optical payload field, and tracks the target using the image tracking video. This paper studied the methods to guide the opto-electronic platform to trace the fixed targets or moving targets on the ground, which established the automatic guiding measurement equation, to translate the target coordinates from geodetic coordinate to the opto-electronic platform coordinate system. To analyze the each factors in automatic guiding measurement equation, using Monte Carlo statistical method, and find how each factors error in measurement equation to affect the precision of the final guidance, in order to improve the guiding precision puts forward some suggestions, the target can be well guided into the track field in a flight test.