• DocumentCode
    488146
  • Title

    Trajectory Optimization for Real-Time Guidance: Part 1, Time-Varying LQR on a Parallel Processor

  • Author

    Psiaki, Mark L. ; Park, Kihong

  • Author_Institution
    Assistant Professor, Mechanical and Aerospace Engineering, Cornell University, Ithaca, New York 14853-7501
  • fYear
    1990
  • fDate
    23-25 May 1990
  • Firstpage
    248
  • Lastpage
    253
  • Abstract
    A key algorithmic element of a real-time trajectory optimization hardware/software implementation is presented, the QP solver element. The purpose of the effort is to make nonlinear trajectory optimization fast enough to provide real-time commands during guidance of a vehicle such as an aero-maneuvering orbiter. Many methods of nonlinear programming require the solution of a quadratic program (QP) at each iteration. In the trajectory optimization case the QP has a special Dynamic Programming structure, a LQR-like structure. QP algorithm speed is increased by taking advantage of this special structure and by parallel implementation.
  • Keywords
    Aerospace engineering; Costs; Dynamic programming; Hardware; Jacobian matrices; Navigation; Quadratic programming; Software algorithms; Time varying systems; Vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1990
  • Conference_Location
    San Diego, CA, USA
  • Type

    conf

  • Filename
    4790736