航天返回与遥感
航天返迴與遙感
항천반회여요감
SPACECRAFT RECOVERY & REMOTE SENSING
2015年
2期
24-31
,共8页
常学立%龙小祥%应荷香%王密%张致齐
常學立%龍小祥%應荷香%王密%張緻齊
상학립%룡소상%응하향%왕밀%장치제
几何定标模型%模式与流程%定标软件%星载线阵相机
幾何定標模型%模式與流程%定標軟件%星載線陣相機
궤하정표모형%모식여류정%정표연건%성재선진상궤
geometric calibration model%mode and workflow%calibration software%space-borne linear array camera
文章采用一种基于探元指向角和相机安装角的星载线阵相机在轨几何定标模型,设计了适合于不同几何成像特点的在轨几何定标模式和流程,并对定标过程中的关键技术环节进行了分析说明。在此基础上设计并实现了星载线阵相机在轨几何定标软件,最后选择资源系列卫星数据,利用软件进行了实验验证。实验结果表明,设计和实现的多个模式定标软件能高效、高精度地完成多星、多相机的在轨几何定标任务,具有兼容多模式定标要求、可扩展至其他卫星型号的特点,能够作为统一的在轨几何定标软件平台。
文章採用一種基于探元指嚮角和相機安裝角的星載線陣相機在軌幾何定標模型,設計瞭適閤于不同幾何成像特點的在軌幾何定標模式和流程,併對定標過程中的關鍵技術環節進行瞭分析說明。在此基礎上設計併實現瞭星載線陣相機在軌幾何定標軟件,最後選擇資源繫列衛星數據,利用軟件進行瞭實驗驗證。實驗結果錶明,設計和實現的多箇模式定標軟件能高效、高精度地完成多星、多相機的在軌幾何定標任務,具有兼容多模式定標要求、可擴展至其他衛星型號的特點,能夠作為統一的在軌幾何定標軟件平檯。
문장채용일충기우탐원지향각화상궤안장각적성재선진상궤재궤궤하정표모형,설계료괄합우불동궤하성상특점적재궤궤하정표모식화류정,병대정표과정중적관건기술배절진행료분석설명。재차기출상설계병실현료성재선진상궤재궤궤하정표연건,최후선택자원계렬위성수거,이용연건진행료실험험증。실험결과표명,설계화실현적다개모식정표연건능고효、고정도지완성다성、다상궤적재궤궤하정표임무,구유겸용다모식정표요구、가확전지기타위성형호적특점,능구작위통일적재궤궤하정표연건평태。
AbstractIn this paper, we adopt an on-orbit geometric calibration model for space-borne optical linear array camera based on the detector’s directional angle and the camera’s installation angle; we design different on-orbit geometric calibration mode and workflow which are applicable to the characteristics of different geometric imaging patterns; we also analyze the key technology in the process of the calibration. On the basis of the above, we have designed and implemented an on-orbit geometric calibration software for space-borne optical linear array camera. Finally, we chose the satellites’ data of ZY series to validate the software. The validation result proves that the multiple modes of calibration software we design and implement can not only complete on-orbit geometric calibration task of multiple satellites and multiple sensors with high efficiency and high precision, but also has the characteristic of compatibility of multiple calibration mode requirements and good extendability to other satellites. This shows that the software proposed in the paper can be used as a unified on-orbit geometric calibration software platform.