A reusable architectural pattern for auto-generated payload management flight software

A. Murray, M. Schoppers, Steve F. Scandore
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引用次数: 3

Abstract

Mars Science Laboratory (MSL), NASA's next mission to Mars, will deploy a large Rover carrying a battery of eleven science instruments, representing a wide variety of payload types. The Rover's flight software (FSW) has the task of monitoring, commanding, collecting, managing and in some cases calibrating data from these instruments. Though the instruments represent a large variety of requirements, complexity, data volumes, fault protection, and commanding logic, the FSW is designed to exploit the commonality among the instruments' requirements in order to maximize reuse of software and to minimize design, implementation and testing effort. To achieve this, we developed an architectural pattern in which all of the common features and patterns of behavior required to manage an instrument are supported, and clear adaptation points are identified and provided to allow expression of the unique behaviors needed for each instrument. For each instrument there is a FSW module called an Instrument Manager (IM), and each of these is an instance of the common pattern. The common IM architecture is expressed in the design as a FSW module called the Instrument Manager Framework (IMF), along with a supporting library for handling instrument communications, the Instrument Manager Library (IML). The IMF module includes a code generator that reads specifications of the ground command set for an instrument, their associated behaviors, and other internal behaviors (e.g. fault response behaviors), expressed in spreadsheets, and produces a set of source code files containing implementations of these commands and behaviors, and their supporting types and variables. The IML module also includes a code generator which transforms a spreadsheet specifying the set of commands that the instrument accepts into C code that parameterizes communications with the instruments. We first describe the instrument management requirements on the Rover FSW, and then continue with an exposition of the IM architectural pattern. We conclude with some statistics on the efficiencies gained in the application of this pattern.
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自动生成有效载荷管理飞行软件的可重用架构模式
火星科学实验室(MSL)是美国宇航局的下一个火星任务,它将部署一个大型火星车,携带11个科学仪器,代表各种有效载荷类型。火星车的飞行软件(FSW)的任务是监控、指挥、收集、管理和在某些情况下校准来自这些仪器的数据。虽然这些仪器代表了各种各样的需求、复杂性、数据量、故障保护和命令逻辑,但FSW的设计目的是利用仪器需求之间的共性,以最大限度地重用软件,并最大限度地减少设计、实现和测试工作。为了实现这一点,我们开发了一个体系结构模式,其中支持管理工具所需的所有公共特征和行为模式,并确定和提供了明确的适应点,以允许表达每个工具所需的独特行为。对于每种乐器,都有一个称为乐器管理器(instrument Manager, IM)的FSW模块,每个模块都是通用模式的实例。通用IM架构在设计中表示为FSW模块,称为仪器管理器框架(IMF),以及用于处理仪器通信的支持库,即仪器管理器库(IML)。IMF模块包括一个代码生成器,它读取仪器的地面命令集规范、相关行为和其他内部行为(如故障响应行为),并生成一组源代码文件,其中包含这些命令和行为的实现及其支持类型和变量。IML模块还包括一个代码生成器,它将指定仪器接受的命令集的电子表格转换为参数化与仪器通信的C代码。我们首先描述了Rover FSW上的仪器管理需求,然后继续阐述了IM架构模式。最后,我们提供了一些关于此模式的应用程序所获得的效率的统计数据。
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