Computation model and error budget for image motion of aerial imaging system

SUN Hui; ZHANG Shu-mei

doi:10.3788/OPE.20122011.2492

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Computation model and error budget for image motion of aerial imaging system

Article | 更新时间：2020-08-12

- Computation model and error budget for image motion of aerial imaging system
- Optics and Precision Engineering Vol. 20, Issue 11, Pages: 2492-2499(2012)
- 作者机构：
  
  中国科学院长春光学精密机械与物理研究所中科院航空光学成像与测量重点实验室,吉林长春 130033
- 作者简介：
- 基金信息：
- DOI：10.3788/OPE.20122011.2492
  CLC： TP274;V245.6
- Received：19 October 2011，
  
  Revised：10 February 2012，
  
  Published：10 November 2012
- 稿件说明：
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孙辉, 张淑梅. 机载成像系统像移计算模型与误差分析[J]. 光学精密工程, 2012,20(11): 2492-2499

SUN Hui, ZHANG Shu-mei. Computation model and error budget for image motion of aerial imaging system[J]. Editorial Office of Optics and Precision Engineering, 2012,20(11): 2492-2499
孙辉, 张淑梅. 机载成像系统像移计算模型与误差分析[J]. 光学精密工程, 2012,20(11): 2492-2499 DOI： 10.3788/OPE.20122011.2492.

SUN Hui, ZHANG Shu-mei. Computation model and error budget for image motion of aerial imaging system[J]. Editorial Office of Optics and Precision Engineering, 2012,20(11): 2492-2499 DOI： 10.3788/OPE.20122011.2492.

摘要

研究了机载成像系统的像移及其对成像质量与相机分辨率的影响。为准确获取像移矢量

实现成像系统像移补偿

提出了一种基于坐标变换的机载成像系统像移计算模型。通过线性坐标变换

建立了从地面目标景物到成像系统像面的坐标变换模型

推导了地面目标景物在成像系统像面的解析表达式

根据坐标在相机积分时间内的变化来确定像移矢量。分析了成像系统像移误差的主要来源

讨论了载机轨道坐标、飞行姿态角和相机视轴角误差对像移计算结果的影响

采用蒙特卡罗方法分析和统计了像移计算误差。样本实验结果表明

在载机姿态角和相机摆角不变条件下

像移量与载机速度成正比

与目标距离成反比

像移误差随着参数误差的增加而增加

其中载机经度和纬度误差是影响像移计算误差的重要因素。结果显示本文方法对机载成像系统的像移补偿具有实用价值。

Abstract

The image motion of an aerial imaging system was researched and its effects on imaging quality and the resolution of the camera were analyzed. In order to obtain and compensate the image motion of the aerial imaging system

a computation model of image motion based on coordinate trans-formation was proposed. The coordinate transformation model from a ground object to a sensor plane was established by using linear coordinate transformation

and the computation formula of image motion was derived based on the different coordinates of the same ground object during camera exposure. The sources of image shift error of the imaging system were analyzed and the influences of various error factors including the aircraft motion

attitude angle and the camera swing angle on image shift calculation were discussed. Then

the calculation error budget and synthesis with Mont Carlo method was presented. The experimental result shows that the image motion is directly proportional to the velocity of aircraft

and inversely proportional to the distance between aircraft and ground object when the attitude angle and camera swing angle are constant. Furthermore

the calculation error becomes greater with the increase of the parameter disturbance

especially the measuring errors of aircraft motion in longitude and latitude. It concludes that this method is efficient and will be useful to the image motion compensation of aerial imaging systems.

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references

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中国科学院长春光学精密机械与物理研究所

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