• DocumentCode
    2387884
  • Title

    Adaptive control and the NASA X-15 program: A concise history, lessons learned, and a provably correct design

  • Author

    Dydek, Zachary T. ; Annaswamy, Anuradha M. ; Lavretsky, Eugene

  • Author_Institution
    Dept. of Mech. Eng., Massachusetts Inst. of Technol., Cambridge, MA
  • fYear
    2008
  • fDate
    11-13 June 2008
  • Firstpage
    2957
  • Lastpage
    2962
  • Abstract
    The NASA X-15 research airplane was one of the earliest aircraft to feature an adaptive control scheme, making its first flight in 1959. The program is largely considered a success, the one exception being the fatal accident that occurred on November 15, 1967. The circumstances which led to the anomalous behavior of the X-15 during that flight are reproduced using a fully nonlinear six-degree-of-freedom aircraft model and a detailed model of the original MH-96 adaptive controller. Using the lessons learned from the X-15 program as well as decades of work in the field of stable adaptive control, a provably correct (PC) adaptive controller is designed for the X-15. When subjected to the same conditions that caused the original MH-96 adaptive controller to fail, the PC adaptive controller is able to recover and complete the maneuver successfully.
  • Keywords
    adaptive control; aircraft control; control system synthesis; history; nonlinear control systems; MH-96 adaptive controller; NASA X-15 research airplane; nonlinear six-degree-of-freedom aircraft model; provably correct adaptive controller; stable adaptive control; Accidents; Adaptive control; Aerodynamics; Aerospace control; Aircraft; History; Low earth orbit satellites; NASA; Programmable control; Vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 2008
  • Conference_Location
    Seattle, WA
  • ISSN
    0743-1619
  • Print_ISBN
    978-1-4244-2078-0
  • Electronic_ISBN
    0743-1619
  • Type

    conf

  • DOI
    10.1109/ACC.2008.4586945
  • Filename
    4586945