• DocumentCode
    2592718
  • Title

    Automatic throttle control for business and commuter aircraft

  • Author

    Bader, Douglas L.

  • fYear
    1990
  • fDate
    15-18 Oct 1990
  • Firstpage
    205
  • Lastpage
    211
  • Abstract
    Honeywell has developed a digital autothrottle system for application on the Gulfstream IV business jet. This is the first true full-authority digital autothrottle designed specifically for the business and commuter market. A system description of the Gulfstream IV autothrottle is presented, and attention is given to modes and functions, design tradeoffs, and resulting performance. The autothrottle´s modes are: takeoff, go around, flight level change, and speed hold. The primary design tradeoff during development was throttle activity versus control accuracy and dynamic response. The Honeywell design includes several techniques to yield the required accuracy with smooth response and minimal throttle activity. The result is an autothrottle system appropriate for business jets (where passenger comfort is very important). Some of the special considerations involved in designing a digital autothrottle system for use with FADEC (full authority digital engine controls)-controlled engines are discussed
  • Keywords
    aerospace engines; aircraft control; digital control; Gulfstream IV business jet; Honeywell; aircraft control; automatic throttle control; commuter aircraft; digital autothrottle; dynamic response; flight level change; full authority digital engine controls; passenger comfort; smooth response; speed hold; takeoff; Aerospace control; Aircraft navigation; Aircraft propulsion; Automatic control; Business; Control systems; Digital control; Engines; Flexible manufacturing systems; Testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Digital Avionics Systems Conference, 1990. Proceedings., IEEE/AIAA/NASA 9th
  • Conference_Location
    Virginia Beach, VA
  • Type

    conf

  • DOI
    10.1109/DASC.1990.111287
  • Filename
    111287