• DocumentCode
    485470
  • Title

    Number, and Placement of Control System Actuators Considering Possible Failures

  • Author

    Vander Velde, Wall-ace E. ; Carignan, Craig R.

  • Author_Institution
    Professor, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology
  • fYear
    1982
  • fDate
    14-16 June 1982
  • Firstpage
    7
  • Lastpage
    15
  • Abstract
    One of the first questions facing the designer of the control system for a large space structure is how many components¿actuators and sensors¿to specify and where to locate them on the structure. This paper presents a methodology which is intended to assist the designer in this process with respect to actuators. A measure of controllability is defined which is a quantitative indication of how well the system can be controlled with a given set of actuators. Then the effect of component unreliability is introduced by computing the average expected Degree of Controllability over the operating lifetime of the system accounting for the likelihood of various combinations of component failures. The problem of component location is resolved by optimizing this performance measure over the admissible set of actuator locations. The variation of this optimized performance measure with number of actuators is helpful in deciding how many components to use.
  • Keywords
    Actuators; Assembly; Control systems; Controllability; Design optimization; Extraterrestrial measurements; Photovoltaic cells; Sensor systems; Solar energy; Space technology;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1982
  • Conference_Location
    Arlington, VA, USA
  • Type

    conf

  • Filename
    4787792