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Angle of Attack and Load Factor Limiting in Fighter Aircraft using Command Governors
Linköping University, Department of Electrical Engineering, Automatic Control. Linköping University, The Institute of Technology.
Saab Aeronautics.
Linköping University, Department of Electrical Engineering, Automatic Control. Linköping University, Faculty of Science & Engineering.
2017 (English)Conference paper (Refereed)
Abstract [en]

Modern fighter aircraft require maximum control performance in order to have the upper hand in a dogfight or when they have to outmaneuver an enemy missile. Therefore pilots must be able to maneuver the aircraft very close to the limit of what it is capable of while at the same time focus on the tactical tasks of the mission. To enable this, modern flight control systems have automatic systems for angle of attack and load factor limiting.

One such design technique is reference or command governors. In this paper we investigate different ways of designing command governors for angle of attack and load factor limiting in in fighter aircraft flight control systems. We discuss different design approaches and their properties and implement one selected design in Saab's JAS 39 Gripen fighter aircraft simulation environment. 

Place, publisher, year, edition, pages
2017.
Keyword [en]
Command Governor, Reference Governor, Flight Control
National Category
Control Engineering
Identifiers
URN: urn:nbn:se:liu:diva-134246OAI: oai:DiVA.org:liu-134246DiVA: diva2:1069618
Conference
AIAA SchiTech Forum 2017, Grapevine, USA, January 9-13, 2017
Funder
VINNOVA, 2013-01226
Available from: 2017-01-30 Created: 2017-01-30 Last updated: 2017-01-30

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CiteExportLink to record
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Citation style
  • apa
  • harvard1
  • ieee
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Output format
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  • asciidoc
  • rtf