• DocumentCode
    2593465
  • Title

    Avionics systems for advanced launch vehicles

  • Author

    Nelson, Kurt D.

  • Author_Institution
    Gen. Dynamics, San Diego, CA, USA
  • fYear
    1990
  • fDate
    15-18 Oct 1990
  • Firstpage
    430
  • Lastpage
    435
  • Abstract
    A brief description of the successful pre-planned product improvement program used for the integration of modern avionics into the Centaur upper stage system is used to illustrate the implementation of evolutionary changes to an existing launch system. This concept can be used to leverage industry technology to existing vehicles as well as new programs. A common module approach to standard avionics processing capabilities is developed to provide a technology evolution plan to benefit existing and future systems and reduce the total development risk. Topics discussed include multipath redundant avionics, adaptive guidance, navigation & control, electromechanical actuators, integrated GPS (Global Positioning System) with the inertial navigation system, and laser ordnance initiation systems
  • Keywords
    adaptive systems; aerospace control; aerospace instrumentation; electric actuators; inertial navigation; radionavigation; satellite relay systems; Centaur upper stage; Global Positioning System; adaptive guidance; advanced launch vehicles; avionics; control; data acquisition; development risk; electromechanical actuators; inertial navigation; integrated GPS; laser ordnance initiation; multipath redundant avionics; navigation; redundancy; Adaptive control; Aerospace electronics; Control systems; Electrical equipment industry; Global Positioning System; Intelligent vehicles; Navigation; Optical control; Programmable control; Standards development;
  • 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.1990.111327
  • Filename
    111327