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Distributed Flight Control and Propulsion Control Implementation Issues and Lessons Learned FREE

[+] Author Affiliations
William R. Schley

Parker Aerospace Group, Irvine, CA

Paper No. 98-GT-003, pp. V005T15A001; 8 pages
doi:10.1115/98-GT-003
From:
  • ASME 1998 International Gas Turbine and Aeroengine Congress and Exhibition
  • Volume 5: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education
  • Stockholm, Sweden, June 2–5, 1998
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7866-8
  • Copyright © 1998 by ASME

abstract

This paper addresses the motivations for using a distributed control system architecture, technical challenges, typical functions which are off-loaded to remote terminals, sensor/effector interface issues, data bus selection, technology insertion issues, lessons learned, and objectives for future distributed control implementations. Typical design requirements, constraints, environmental conditions, and operational challenges will be described. Examples of various distributed control system implementations will be discussed, including both propulsion control and flight control examples.

Copyright © 1998 by ASME
Topics: Propulsion , Flight
This article is only available in the PDF format.

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