The invention provides a satellite layout method and system for satellite-borne full-airspace loads. The method comprises the steps of 1, analyzing satellite configuration characteristics according tothe configuration of a satellite platform and an effective load; 2, constraining the full-airspace loads according to the satellite configuration characteristics; 3, constructing a load configurationconforming to a preset condition according to the constrained full airspace loads; and 4, based on the configuration of the existing satellite platform and the effective load, performing the satellite layout of the full-airspace loads according to the preset load configuration. According to the invention, the layout problem of full-airspace loads of different frequency bands, systems and purposeson various satellite platforms of different types is solved, the universality and the practicability are high, and support can be provided for the design of the overall satellite and related load configurations.

    本发明提供了一种星载全空域载荷的卫星布局方法及系统,包括:步骤1:根据卫星平台和有效载荷的配置,分析卫星构型特点;步骤2:根据卫星构型特点,对全空域载荷进行约束;步骤3:根据约束后的全空域载荷构建符合预设的载荷构型;步骤4:基于现有的卫星平台和有效载荷的配置,根据预设的载荷构型,进行全空域载荷的卫星布局。本发明解决了各种不同类型卫星平台上的不同频段、体制和用途的全空域载荷的布局问题,通用性和实用性较强,可为卫星总体和相关载荷构型的设计提供支撑。


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    Title :

    Satellite layout method and system for satellite-borne full-airspace loads


    Additional title:

    星载全空域载荷的卫星布局方法及系统


    Contributors:
    FENG YANJUN (author) / GU YONGKUN (author) / HUANG YEPING (author) / ZHANG GUOQIANG (author) / LI JINLIANG (author)

    Publication date :

    2020-11-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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