• DocumentCode
    1863185
  • Title

    Development of a modular on-orbit serviceable satellite architecture

  • Author

    Moynahan, Stephen A. ; Touhy, Seamus

  • Author_Institution
    Draper (C.S.) Lab., Cambridge, MA, USA
  • Volume
    2
  • fYear
    2001
  • fDate
    37165
  • Abstract
    This paper describes an to develop an avionics architecture that enables replacement of deficient satellite hardware on-orbit as well as upgrade/adapt on-orbit systems. It is anticipated that routine, safe, and reliable spacecraft servicing will have significant payoff for many future types of science and military missions. The technologies that enable modern satellite servicing will therefore be critical for implementing new space architectures. Satellites that are placed on-orbit and are functionally lost due to simple failures beg for the development of an on-orbit replacement capability. Human intervention in space, however, carries risk and cost associated with it that would not be necessary if an autonomous satellite repair capability was developed. The associated capability to perform preplanned upgrades and adaptations to on-orbit space assets also has the potential for architecting high performance future spacecraft. Such a capability would allow system designers to accommodate differing rates of technology advancement and would minimize the need fore pre-launch risk reduction measures. The first step in developing a serviceable satellite is to evolve the tightly integrated satellite architectures of today toward an architecture that supports functional and/or physical replacement of anomalous or failed hardware. Draper Laboratory has performed a trade study to develop a single-point architecture that provides a growth path from the functionally efficient satellite designs of today to a functionally reliable modular architecture that will support the autonomous on-orbit upgrade and functional enhancement of tomorrow´s satellites. This paper presents an overview of an architecture that can enable autonomous satellite servicing
  • Keywords
    aerospace computing; avionics; fault location; fault tolerance; maintenance engineering; space vehicle electronics; system buses; IEEE-1394 data bus; autonomous on-orbit upgrade; autonomous satellite repair capability; avionics architecture; deficient satellite hardware replacement; fault-detection; functional enhancement; functionally reliable modular architecture; modular on-orbit serviceable architecture; plug and stay architecture; reliable spacecraft servicing; satellite fault tolerance; single-point architecture; top-level design strategies; Aerospace electronics; Design methodology; Hardware; Humans; Laboratories; Military satellites; Power generation economics; Space shuttles; Space technology; Space vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Digital Avionics Systems, 2001. DASC. 20th Conference
  • Conference_Location
    Daytona Beach, FL
  • Print_ISBN
    0-7803-7034-1
  • Type

    conf

  • DOI
    10.1109/DASC.2001.964236
  • Filename
    964236