Reducing conservatism in aircraft engine response using conditionally active min-max limit regulators /

Bibliographic Details

Main Authors:	May, Ryan D. (Author), Garg, Sanjay (Author)
Corporate Authors:	United States. National Aeronautics and Space Administration (sponsoring body.), ASME Turbo Expo
Format:	Government Document Conference Proceeding eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
Series:	NASA technical memorandum ; 217814.
Subjects:	Commercial aircraft. Aircraft control. Control systems design. Engine control. Sequential control. Transient response.
Online Access:	https://purl.fdlp.gov/GPO/gpo40528