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SIM-Planet Quest Interferometer Real-time Control System Architecture

机译:SIM-PLANET任务干涉仪实时控制系统架构

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This paper presents a top-level architectural overview of the instrument real-time control system currently under development at JPL for the SIM-Planet Quest interferometer. The control system must meet challenging requirements for providing milliarcsecond class pointing and nanometer class delay-line control performance while tracking science stars as dim as 20th visual magnitude. The driving functional requirements call for a three-interferometer system that also serves as an attitude sensing and tracking system. Due to the dim science requirements and complicated control initialization processes, the control system is architectured using complex estimators, multiloop feedforward signals, and distributed computational infrastructure. Control objectives and requirements are presented and the necessary control sensors and actuators are discussed. Initialization of the interferometer control system is explained, including processes for target star search, acquisition, and tracking. The nominal tracking control modes are then presented, including incorporation of pathlength and angle feedforward signals. The estimation architecture is explained next including its role in generating the necessary feedforward signals. The resulting overall algorithm structure and implementation using distributed processors on a ring-bus architecture is also briefly discussed.
机译:本文介绍了目前正在开发的仪器实时控制系统的顶级架构概述,用于JPL的SIM-Planet任务干涉仪。控制系统必须满足提供Markarcond类指向和纳米级延迟线控制性能的具有挑战性要求,同时跟踪科学恒星,如第20个视觉幅度。驱动功能要求呼叫三种干涉仪系统,该系统也用作姿态感测和跟踪系统。由于DIM科学要求和复杂的控制初始化过程,控制系统是使用复杂估计器,多环前馈信号和分布式计算基础设施的架构。提出了控制目标和要求,并讨论了必要的控制传感器和执行器。解释干涉仪控制系统的初始化,包括目标星搜索,获取和跟踪的过程。然后呈现标称跟踪控制模式,包括掺入路径长度和角度前馈信号。接下来解释估计架构,包括其在生成必要的前馈信号时的作用。还简要讨论了由Ring-总线架构上的分布式处理器的总体算法结构和实现。

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