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Multivariable control of a twin lift helicopter system using the LQG/LTR design methodologyGuidelines for developing a multivariable centralized automatic flight control system (AFCS) for a twin lift helicopter system (TLHS) are presented. Singular value ideas are used to formulate performance and stability robustness specifications. A linear Quadratic Gaussian with Loop Transfer Recovery (LQG/LTR) design is obtained and evaluated.
Document ID
19870026145
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rodriguez, A. A. (Massachusetts Inst. of Tech. Cambridge, MA, United States)
Athans, M. (MIT Cambridge, MA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1986
Subject Category
Aircraft Stability And Control
Accession Number
87A13419
Funding Number(s)
CONTRACT_GRANT: NAG2-297
Distribution Limits
Public
Copyright
Other

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