Highly integrated modular avionics from platform to payload for micro-satellites

Peipei Xu, Lianxiang Jiang, Bingui Xu, Mingxiang Li, Fei Wang
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Abstract

Low-cost, intelligence and short development cycle has become its trend of small satellites. A hybrid on-board avionics topology based on CAN bus and router was proposed. The telemetry was collected by On-Board Computer (OBC) via CAN bus, while the router integrated RS422, LVDS, Ethernet, Camera Link and TLK2711 interfaces, which support data rate varying from 1Mbps to 10Gbps and usually used by payloads, so it makes regular payloads integrated into the avionics much easier. The OBC used the PowerPC MPC8548 processor, which run at 1GHz. Plug and play mechanism was adopted to make the OBC recognize the devices dynamically when they powered on, which accelerated the system integration; furthermore, the software modules were also allowed to install or uninstall dynamically on-line for flexibility. For the modular and various interfaces supported, payload modules such as GNSS-R receiver, ADS-B receiver and camera electronics was easily integrated into the avionics box, so the signaling were transferred via the backplane instead of cables.
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微型卫星从平台到有效载荷的高度集成模块化航空电子设备
低成本、智能化、研制周期短已成为其发展的趋势。提出了一种基于CAN总线和路由器的混合机载航空电子拓扑结构。遥测数据由机载计算机(OBC)通过CAN总线收集,而路由器集成了RS422、LVDS、以太网、Camera Link和TLK2711接口,支持1Mbps到10Gbps的数据速率,通常用于有效载荷,因此使常规有效载荷集成到航空电子设备中变得更加容易。OBC使用PowerPC MPC8548处理器,运行频率为1GHz。采用即插即用机制,使OBC在设备上电时动态识别,加快了系统集成;此外,软件模块还允许在线动态安装或卸载,以提高灵活性。由于支持模块化和各种接口,GNSS-R接收机、ADS-B接收机和相机电子设备等有效载荷模块很容易集成到航空电子设备盒中,因此信号通过背板而不是电缆传输。
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