• DocumentCode
    986561
  • Title

    Quadratically constrained attitude control via semidefinite programming

  • Author

    Kim, Yoonsoo ; Mesbahi, Mehran

  • Author_Institution
    Dept. of Aeronaut. & Astronaut., Univ. of Washington, Seattle, WA, USA
  • Volume
    49
  • Issue
    5
  • fYear
    2004
  • fDate
    5/1/2004 12:00:00 AM
  • Firstpage
    731
  • Lastpage
    735
  • Abstract
    We consider the attitude control problem augmented with an arbitrary number of nonconvex quadratic constraints. By utilizing the implicit magnitude constraint of the state vector (i.e., quaternion), we are able to reduce this problem to a convex quadratically constrained quadratic program or a semidefinite program. This result leads to an efficient solution strategy for general quadratically constrained attitude control problems. An example demonstrates the proposed methodology.
  • Keywords
    attitude control; constraint theory; convex programming; space vehicles; implicit magnitude constraints; nonconvex quadratic constraints; quadratically constrained attitude control; semidefinite programming; state vector; Constraint optimization; Linear matrix inequalities; Optical control; Optimal control; Quadratic programming; Quaternions; Space missions; Space vehicles; Symmetric matrices; Torque control; Attitude control; convex optimization; semidefinite programming; state constrained control;
  • fLanguage
    English
  • Journal_Title
    Automatic Control, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9286
  • Type

    jour

  • DOI
    10.1109/TAC.2004.825959
  • Filename
    1298998