• DocumentCode
    1934131
  • Title

    Model based systems engineering (MBSE) applied to Radio Aurora Explorer (RAX) CubeSat mission operational scenarios

  • Author

    Spangelo, S.C. ; Cutler, J. ; Anderson, Lindsay ; Fosse, E. ; Cheng, Lin ; Yntema, R. ; Bajaj, Mohit ; Delp, C. ; Cole, B. ; Soremekum, G. ; Kaslow, D.

  • Author_Institution
    Univ. of Michigan, Ann Arbor, MI, USA
  • fYear
    2013
  • fDate
    2-9 March 2013
  • Firstpage
    1
  • Lastpage
    18
  • Abstract
    Small satellites are more highly resource-constrained by mass, power, volume, delivery timelines, and financial cost relative to their larger counterparts. Small satellites are operationally challenging because subsystem functions are coupled and constrained by the limited available commodities (e.g. data, energy, and access times to ground resources). Furthermore, additional operational complexities arise because small satellite components are physically integrated, which may yield thermal or radio frequency interference. In this paper, we extend our initial Model Based Systems Engineering (MBSE) framework developed for a small satellite mission by demonstrating the ability to model different behaviors and scenarios. We integrate several simulation tools to execute SysML-based behavior models, including subsystem functions and internal states of the spacecraft. We demonstrate utility of this approach to drive the system analysis and design process. We demonstrate applicability of the simulation environment to capture realistic satellite operational scenarios, which include energy collection, the data acquisition, and downloading to ground stations. The integrated modeling environment enables users to extract feasibility, performance, and robustness metrics. This enables visualization of both the physical states (e.g. position, attitude) and functional states (e.g. operating points of various subsystems) of the satellite for representative mission scenarios. The modeling approach presented in this paper offers satellite designers and operators the opportunity to assess the feasibility of vehicle and network parameters, as well as the feasibility of operational schedules. This will enable future missions to benefit from using these models throughout the full design, test, and fly cycle. In particular, vehicle and network parameters and schedules can be verified prior to being implemented, during mission operations, and can also be updated in near real-time with oper- tional performance feedback.
  • Keywords
    aerospace computing; artificial satellites; interference suppression; radiofrequency interference; satellite ground stations; scheduling; simulation languages; systems engineering; CubeSat mission operational scenario; Radio Aurora Explorer; SysML-based behavior models; data acquisition; energy collection; ground station; model based system engineering; network parameter; operational complexity; operational performance feedback; operational schedule; radio frequency interference; satellite component; space vehicle; spacecraft; subsystem functions; thermal interference; Analytical models; Biological system modeling; Earth; Industries; Satellites; Training; Visualization;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2013 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4673-1812-9
  • Type

    conf

  • DOI
    10.1109/AERO.2013.6496894
  • Filename
    6496894