首页> 外文OA文献 >Mission planning and scheduling concept for the Advanced X-ray Astrophysics Facility (AXAF)
【2h】

Mission planning and scheduling concept for the Advanced X-ray Astrophysics Facility (AXAF)

机译:先进的X射线天体物理学设施(AXAF)的任务计划和计划概念

代理获取
本网站仅为用户提供外文OA文献查询和代理获取服务,本网站没有原文。下单后我们将采用程序或人工为您竭诚获取高质量的原文,但由于OA文献来源多样且变更频繁,仍可能出现获取不到、文献不完整或与标题不符等情况,如果获取不到我们将提供退款服务。请知悉。
获取外文期刊封面目录资料

摘要

Projected for launch in the latter part of 1998, the Advanced X-ray Astrophysics Facility (AXAF), the third satellite in the Great Observatory series, promises to dramatically open the x-ray sky as the Hubble and Compton observatories have done in their respective realms. Unlike its companions, however, AXAF will be placed in a high altitude, highly elliptical orbit (10,000 x 100,000 km), and will therefore be subject to its own unique environment, spacecraft and science instrument constraints and communication network interactions. In support of this mission, ground operations personnel have embarked on the development of the AXAF Offline System (OFLS), a body of software divided into four basic functional elements: (1) Mission Planning and Scheduling, (2) Command Management, (3) Altitude Determination and Sensor Calibration and (4) Spacecraft Support and Engineering Analysis. This paper presents an overview concept for one of these major elements, the Mission Planning and Scheduling subsystem (MPS). The derivation of this concept is described in terms of requirements driven by spacecraft and science instrument characteristics, orbital environment and ground system capabilities. The flowdown of these requirements through the systems analysis process and the definition of MPS interfaces has resulted in the modular grouping of functional subelements depicted in the design implementation approach. The rationale for this design solution is explained and capabilities for the initial prototype system are proposed from the user perspective.
机译:预计于1998年下半年发射的高级X射线天体物理学设施(AXAF)是大天文台系列的第三颗卫星,有望像哈勃和康普顿天文台在各自的工作中那样,显着打开X射线天空领域。但是,与它的同伴不同,AXAF将被置于高海拔,高度椭圆形的轨道(10,000 x 100,000公里)中,因此将受到其自身独特的环境,航天器和科学仪器的约束以及通信网络的相互作用。为了支持该任务,地面作战人员着手开发AXAF离线系统(OFLS),该系统是由四个基本功能元素组成的软件:(1)任务计划和计划;(2)指挥管理;(3 )高度确定和传感器校准以及(4)航天器支持和工程分析。本文介绍了这些主要要素之一的任务计划和调度子系统(MPS)的概述概念。根据航天器和科学仪器的特性,轨道环境和地面系统能力所驱动的要求来描述此概念的派生。通过系统分析过程和MPS接口的定义,这些需求的减少导致了设计实现方法中描述的功能子元素的模块化分组。解释了此设计解决方案的基本原理,并从用户角度提出了初始原型系统的功能。

著录项

  • 作者

    Guffin, O. T.; Newhouse, M.;

  • 作者单位
  • 年度 1994
  • 总页数
  • 原文格式 PDF
  • 正文语种
  • 中图分类

相似文献

  • 外文文献
  • 中文文献
  • 专利
代理获取

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号