Volume 22 Issue 11
Nov.  2007
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WANG Xiao-feng, HUANG Hai. Multidisciplinary design optimization based on advanced model of satellite attitude control system[J]. Journal of Aerospace Power, 2007, 22(11): 1958-1962.
Citation: WANG Xiao-feng, HUANG Hai. Multidisciplinary design optimization based on advanced model of satellite attitude control system[J]. Journal of Aerospace Power, 2007, 22(11): 1958-1962.

Multidisciplinary design optimization based on advanced model of satellite attitude control system

  • Received Date: 2006-10-24
  • Rev Recd Date: 2007-10-14
  • Publish Date: 2007-11-28
  • The coupled relationship between the attitude control system and other subsystems of three-axis-stabilized satellite was analyzed in this paper,and then attitude control models and subsystem hardware were selected.More accurate analysis model was established to calculate subsystem mass and power,then optimization models of integrated system,attitude control subsystem,power subsystem and structure subsystem based on collaborative optimization(CO) methodology were built. Finally,the programs were compiled with Clanguage for the analysis models and optimization models.The results shows: subsystem model collaborates well with this system model to obtain better system performance.

     

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