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Localized Payload Management Approach to Payload Control and Data Acquisition Architecture for Space Applications

机译:用于空间应用的有效载荷控制和数据采集架构的本地化有效载荷管理方法

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This paper presents the development of a new approach for the Payload Control and Data Acquisition Subsystem (PCDAS) to be applied in micro-, up to small-satellite systems in low earth orbits with various payloads. PCDAS is the subsystem, which interfaces with the data streams to and from the payload systems, converts data from digital interfaces into data packets for transmission to the ground-station. Control packets and telemetry are converted into appropriate digital sequences to the onboard computer. The localized payload management approach tends to design PCDAS as a stand alone subsystem, i.e. to be independent from the On-Board Computer (OBC) and all on-board payload systems. For realization, the PCDAS is implemented in VHDL, and evaluated on an SRAM-Based FPGA (Field Programmable Gate Array) chip. The PCDAS simulated and functionally verified using a payload with four simultaneous channels, each with data rate of 60 Mbps.
机译:本文提出了开发新方法,用于将微量的有效载荷控制和数据采集子系统(PCDA)应用于微米,直到具有各种有效载荷的低地轨道中的小卫星系统。 PCDAS是子系统,其与往返于有效载荷系统的数据流接口,将来自数字接口的数据转换为数据分组以传输到地站。控制数据包和遥测将转换为适当的数字序列到板载计算机。本地化的有效载荷管理方法倾向于将PCDA设计为独立子系统,即独立于车载计算机(OBC)和所有车载有效载荷系统。为了实现,PCDA在VHDL中实现,并在基于SRAM的FPGA(现场可编程门阵列)芯片上进行评估。使用具有四个同时通道的有效载荷模拟和功能验证的PCDA,每个通道具有60 Mbps的数据速率。

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