遥感卫星平台与载荷一体化设计综述  

An Overview of Integrated Design of Platform and Payload for Remote Sensing Satellite

作　　者：祖家国 吴艳华 杨岩[2] 李坝清 郭崇岭[2] 蔺宇辉[2] 孙德伟[2] 田景峰[1] 王光远[1] ZU Jiaguo;WU Yanhua;YANG Yan;LI Baqing;GUO Chongling;LIN Yuhui;SUN Dewei;TIAN Jingfeng;WANG Guangyuan(Beijing Institute of Spacecraft System Engineering,Beijing 100094,China;Beijing Institute of Space Mechanics&Electricity,Beijing 100094,China)

机构地区：[1]北京空间飞行器总体设计部,北京100094 [2]北京空间机电研究所,北京100094

出　　处：《航天返回与遥感》2018年第4期87-94,共8页Spacecraft Recovery & Remote Sensing

摘　　要：随着遥感卫星使用效能的提升,整星和载荷的规模都在逐渐增大,遥感卫星现有的研制模式从构型布局、发射段抗力学以及在轨段微振动抑制等各个方面都限制了整星和载荷的研制能力,平台载荷一体化设计将成为解决大中型遥感卫星研制的重要手段。文章从一体化设计概念出发,提出了围绕载荷和基于平台的两种一体化设计理念,以一体化技术发展路线和实现目标的角度,深入探讨了平台载荷一体化设计的3个层级划分,并概要描述了遥感卫星一体化研制现状,最后明确了一体化设计的任务目标,可为后续遥感卫星平台载荷一体化研制提供借鉴。With the improvement of the use efficiency of remote sensing satellite,the dimension of the entire satellite and payload is gradually increasing.However,the current development model of remote sensing satellite,including the configuration layout,the launch phase resistance and the suppression of micro-vibration at the orbital stage and so on,limits the development ability of remote sensing satellite and the payload.Integrated Design of Platform and Payload(IDPP)will become an important way to solve the development bottleneck of large and medium-sized remote sensing satellite.Starting with the concept of IDPP,this article introduces two IDPP’s concepts,that is Payload-based and Platform-based.From the perspective of IDDP development and implementation goal,three levels of IDDP are discussed,and the development status of IDPP is briefly described.Finally,the task goal of IDDP is defined,which can provide reference for the follow-up development of remote sensing satellite IDDP.

关 键 词：一体化设计 平台 光学有效载荷 遥感卫星 

分 类 号：V423.6[航空宇航科学与技术—飞行器设计]