宇航计测技术 ›› 2023, Vol. 43 ›› Issue (2): 76-82.doi: 10.12060/j.issn.1000-7202.2023.02.14

• 计量保障技术 • 上一篇    下一篇

批产航天器自测试系统设计

杨同智,党建成,刘廷玉,安天琪,王继业   

  1. 上海卫星工程研究所,上海 201109
  • 出版日期:2023-04-21 发布日期:2023-06-21
  • 作者简介:杨同智(1987-),男,高级工程师,硕士,主要研究方向:航天器总体设计、综合测试与在轨管理。
  • 基金资助:
    国家自然科学基金(62273120)、装备预先研究(50904020101)。

Design of Self-test System for Batch-produced Spacecraft

YANG Tong-zhi,DANG Jian-cheng,LIU Ting-yu,AN Tian-qi,WANG Ji-ye   

  1. Shanghai Institute of Satellite Engineering,Shanghai 201109,China
  • Online:2023-04-21 Published:2023-06-21

摘要: 集成快检、存储快检与射前快检成为批产航天器亟待解决的问题。传统航天器综合测试模式存在测试效率低、测试改装部署繁琐、测试成本高、测试周期长和难以深入产品内部探查的问题,不能很好地适应批产研制与测发需求。针对该问题,从航天器可测试性与自测试设计出发,研究航天器自测试功能单元的设计方法、自测试通信交互模式、基于结构模型与行为模型的自测试诊断模型设计方法,设计了分层的自测试系统架构,通过总线快速调度自测试流程,提升快速检修能力,满足批产航天器快检需求。

关键词: 车载诊断系统, 内建自测试, 自测试通信接口, 自测试功能单元

Abstract: Rapid integrated test,regular rapid inspection after batch storage and rapid inspection before launch have become urgent production problems for batch-produced spacecraft.The traditional spacecraft integrated test mode has the problems of low test efficiency,cumbersome test modification and deployment,high test cost,long test cycle and difficult in-depth product internal exploration,which cannot well meet the needs of rapid development and test of batch-produced spacecraft.In view of the above problems,starting from the design of spacecraft testability and self-test,the design method of spacecraft self-test function unit,self-test communication interaction mode and self-test diagnosis model based on structural model and behavior model is studied,and the construction of layered spacecraft self-test system is designed.The self-test process is quickly scheduled through bus,which improve the rapid maintenance capability to meet the needs of rapid inspection of batch-produced spacecraft.

Key words: On-board diagnostics, Built-in self-test, Self-test communication interface, Self-test function unit

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