• DocumentCode
    1527003
  • Title

    Manual flight control with saturating actuators

  • Author

    Pachter, M. ; Miller, R.B.

  • Author_Institution
    Air Force Inst. of Technol., Wright Patterson AFB, USA
  • Volume
    18
  • Issue
    1
  • fYear
    1998
  • fDate
    2/1/1998 12:00:00 AM
  • Firstpage
    10
  • Lastpage
    20
  • Abstract
    The objectives of this article are to concisely state the tracking control problem with actuator saturation, briefly review the current literature, and formulate the problem in a manual (flight) control context. The complexity of tracking control with saturation is demonstrated via a simple example. A new approach to the manual flight control problem with both rate and amplitude actuator constraints, referred to as linear quadratic tracking (LQT), is outlined. This approach is specifically directed toward the dynamic tracking control problem subject to both displacement and rate actuator constraints, particularly for the challenging case of open-loop unstable plants, which are of current interest in flight control. At the same time, due to the low order of the simplified plant models used in flight control it is reasonable to assume full state feedback is available, although the tracked variable is a scalar, e.g., pitch rate. The saturation avoidance aspect of the proposed LQT solution is demonstrated for the simple example
  • Keywords
    aircraft control; closed loop systems; linear quadratic control; state feedback; tracking; actuator saturation; dynamic tracking control; full state feedback; linear quadratic tracking; manual flight control; open-loop unstable plants; saturating actuators; tracking control problem; Actuators; Aerospace control; Computer crashes; Control systems; Elevators; Feedback loop; Humans; Military aircraft; Modems; Vehicles;
  • fLanguage
    English
  • Journal_Title
    Control Systems, IEEE
  • Publisher
    ieee
  • ISSN
    1066-033X
  • Type

    jour

  • DOI
    10.1109/37.648622
  • Filename
    648622