一种星载软件通信调度方法及系统

本发明提供一种星载软件通信调度方法及系统,针对不基于嵌入式操作系统、作为通信总线网络主站的星载软件,在该通信调度架构下,可以并行开展周期性载荷信息采集与任务驱动式载荷状态配置通信,既保障了地面测控系统可实时监测航天器全运行阶段的各载荷状态,也确保了航天器各项地面测试、在轨测试任务的高效顺利开展,在航天器研制领域具有较好的工程应用价值,能胜任未来通信任务与通信场景日趋复杂多样的新要求,提高了航天器综合电子系统的可靠性与可维护性。 The invention provides a satellite-borne software communication scheduling method an...

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LanguageChinese
Published 20.09.2024
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Summary:本发明提供一种星载软件通信调度方法及系统,针对不基于嵌入式操作系统、作为通信总线网络主站的星载软件,在该通信调度架构下,可以并行开展周期性载荷信息采集与任务驱动式载荷状态配置通信,既保障了地面测控系统可实时监测航天器全运行阶段的各载荷状态,也确保了航天器各项地面测试、在轨测试任务的高效顺利开展,在航天器研制领域具有较好的工程应用价值,能胜任未来通信任务与通信场景日趋复杂多样的新要求,提高了航天器综合电子系统的可靠性与可维护性。 The invention provides a satellite-borne software communication scheduling method and a satellite-borne software communication scheduling system, aiming at satellite-borne software which is not based on an embedded operating system and is used as a communication bus network master station, periodic load information acquisition and task-driven load state configuration communication can be carried out in parallel under a communication scheduling architecture, and the communication efficiency is improved. The ground measurement and control system is guaranteed to monitor each load state of the spacecraft in a full operation stage in real time, efficient and smooth development of each ground test and on-orbit test task of the spacecraft is also guaranteed, the method has a good engineering application
Bibliography:Application Number: CN202210003391