航天器工程2024，Vol.33Issue(1)：11-18,8.DOI:10.3969/j.issn.1673-8748.2024.01.002
面向微纳遥感星座构建的阻力差分控制方法
Differential Drag Control Method for Establishment of Micro-nano Remote Sensing Satellite Constellation
张国云 1龚轲杰 1何雨帆 1陈军 1蔡立锋 1王超 1马腾 1贺于珍1
作者信息
摘要
Abstract
Considering weight,power consumption,volume and cost of the whole satellite,some micro-nano satellites are usually not equipped with propulsion systems.In order to meet the con-stellation establishment requirements,the differential drag control(no-propulsion control)tech-nology method is proposed.By adjusting the windward area of the solar array,the differential drag is used to increase or decrease the difference of orbital semi-major axis between two satel-lites.Then,phase of the micro-nano remote sensing satellite constellation can be controlled with-out changing the satellites'body attitude or affecting the application of the payload.The differential drag control method is verified by using 20 micro-nano remote sensing satellites to construct a con-stellation.By applying the differential drag control technology to the phase control of micro-nano remote sensing satellite constellation,the satellites can be equally phased in the same orbital plane,and the constellation construction can be successfully realized.关键词
微纳遥感星座/阻力差分控制/相位控制Key words
micro-nano remote sensing satellite constellation/differential drag control/phase control分类
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张国云,龚轲杰,何雨帆,陈军,蔡立锋,王超,马腾,贺于珍..面向微纳遥感星座构建的阻力差分控制方法[J].航天器工程,2024,33(1):11-18,8.
