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Robust and modular on-board architecture for future robotic spacecraft

机译:坚固耐用的模块化机载架构,适合未来的机器人航天器

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This paper presents a novel approach for future robotic spacecraft by utilizing a modular and robust software architecture based on the time and space partitioning (TSP) concept. Classic satellites are characterized by a strict separation between platform and payload subsystems, both in hardware resources as well as in control software. Novel space-robotic applications such as on-orbit servicing (OOS) feature dexterous robotic devices attached onto the satellite that impose a direct physical feedback on their floating base. Through the high degree of interdependencies, the whole satellite turns into a space robot. Hence, the robot becomes an integral part of the spacecraft itself and needs to be integrated into the existing control and operations approach. The developed embedded on-board framework represents a modular and robust control and communication environment that allows both classic satellite as well as real-time and autonomous robotic operations. The framework features an integral fault detection, isolation and recovery (FDIR) concept in order to prevent overall system shutdown upon single-point failure. Single software components reside in separate logical modules, i.e. partitions, in order to avoid resource violations. Upon critical failure, partitions can be restarted without detracting the rest of the system. By applying explicit time scheduling of partitions, system resources can be optimally distributed and deterministic behavior be achieved. Core system functionality has been implemented by ECSS-tested components that are configurable and thus re-usable over multiple missions. As demonstrator, a realistic on-orbit servicing simulation was set up that comprises autonomous target satellite capture and fault management. The presented architecture follows an integrated approach that is required for safely operating future robotic spacecraft. Through re-usability of software components, fewer resources for the implementation and verification process are - equired as only additional, mission-specific components need to be taken care of. Application developers can use the core functionality and communication API and concentrate on their own task at hand.
机译:本文通过利用基于时空划分(TSP)概念的模块化且强大的软件体系结构,为未来的机器人航天器提出了一种新颖的方法。经典卫星的特点是,在硬件资源和控制软件中,平台子系统和有效载荷子系统之间必须严格分开。诸如在轨维修(OOS)之类的新型太空机器人应用具有连接到卫星的灵巧机器人设备,这些机器人设备在其浮动基座上施加了直接的物理反馈。通过高度的相互依赖,整个卫星变成了太空机器人。因此,机器人成为航天器本身不可或缺的一部分,需要集成到现有的控制和操作方法中。开发的嵌入式机载框架代表了模块化且强大的控制和通信环境,该环境允许经典卫星以及实时和自主机器人操作。该框架具有集成的故障检测,隔离和恢复(FDIR)概念,以防止单点故障时整个系统关闭。单个软件组件位于单独的逻辑模块(即分区)中,以避免资源冲突。发生严重故障时,可以重新启动分区,而不会影响系统的其余部分。通过应用分区的显式时间调度,可以最佳地分配系统资源并实现确定性行为。核心系统功能已由经过ECSS测试的组件实现,这些组件可配置,因此可在多个任务中重复使用。作为演示者,建立了一个现实的在轨维修仿真,其中包括自主目标卫星的捕获和故障管理。提出的架构遵循安全操作未来机器人航天器所需的集成方法。通过软件组件的可重用性,实现和验证过程所需的资源更少-等同于只需要维护额外的,特定于任务的组件。应用程序开发人员可以使用核心功能和通信API,并专注于手头的任务。

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