• DocumentCode
    927051
  • Title

    Avionics for the Small Remotely Piloted Vehicle

  • Author

    Vandersteen, A.D.

  • Author_Institution
    Research & Development Division, Lockheed Missiles & Space Company, Inc., Palo Alto, California
  • Volume
    2
  • Issue
    6
  • fYear
    1987
  • fDate
    6/1/1987 12:00:00 AM
  • Firstpage
    24
  • Lastpage
    30
  • Abstract
    The Lockheed developmental remotely piloted vehicle (RPV) is a highly sophisticated miniature airplane which represents the current state of the art in RPVs. The avionics, which include flight controls, inertial attitude reference, recovery guidance, payload and data link, represent more than 80 percent of the cost of the vehicle. The key cost drivers are the payload and data link which must accommodate long stand-off range and rapid AV jinking for good survivability, day and night operation, high radio jamming conditions, and high-precision laser pointing accuracy. However, there are many RPV applications which are less demanding and can therefore take advantage of substantial cost reductions. Lockheed Research & Development Division is addressing this need by defining flexible, adaptive, avionics concepts which emphasize the nondevelopmental philosophy. One such system is the Lockheed Adaptive Modular Payload (LAMP). This system promotes use of a standard universal two-axis gimbal platform into which many different forms of imaging sensors can be installed. This concept is aimed at reconnaissance and surveillance. It is now being integrated into the future RPV programs at the Lockheed Austin Division.
  • Keywords
    Aerospace control; Aerospace electronics; Airplanes; Attitude control; Navigation; Payloads;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems Magazine, IEEE
  • Publisher
    ieee
  • ISSN
    0885-8985
  • Type

    jour

  • DOI
    10.1109/MAES.1987.5005419
  • Filename
    5005419