• DocumentCode
    1140558
  • Title

    Minimum Trajectory Sensitivity of a Large Launch Booster Control System

  • Author

    Luh, J.Y.S.

  • Author_Institution
    Madiassa Maguiraga Purdue University, Lafayette, Ind.
  • Issue
    2
  • fYear
    1969
  • fDate
    3/1/1969 12:00:00 AM
  • Firstpage
    213
  • Lastpage
    220
  • Abstract
    An optimal closed-loop control scheme is developed for a linear timevarying system. The system has two independent parameters which may deviate from their nominal values. The problem is motivated by the possible failure of the control system of the large launch booster after takeoff. The computational scheme involves an iterative algorithm and requires the solution to a matrix Riccati equation. An example is given as an illustration.
  • Keywords
    Control systems; Differential equations; Drag; Engines; Iterative algorithms; Optimal control; Performance analysis; Riccati equations; Taylor series; Weight control;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/TAES.1969.309907
  • Filename
    4103300
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=1140558