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A problem formulation for glideslope tracking in wind shear using advanced robust control techniquesA formulation of the longitudinal glideslope tracking of a transport-class aircraft in severe wind shear and turbulence for application to robust control system design is presented. Mathematical wind shear models are incorporated into the vehicle mathematical model, and wind turbulence is modeled as an input disturbance signal. For this problem formulation, the horizontal and vertical wind shear gradients are treated as real uncertain parameters that vary over an entire wind shear profile. The primary objective is to examine the formulation of this problem into an appropriate design format for use in m-synthesis control system design.
Document ID
19930001988
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Belcastro, Christine M.
(NASA Langley Research Center Hampton, VA, United States)
Chang, B.-C.
(Drexel Univ. Philadelphia, PA., United States)
Fischl, Robert
(Drexel Univ. Philadelphia, PA., United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1992
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-TM-104164
NAS 1.15:104164
Report Number: NASA-TM-104164
Report Number: NAS 1.15:104164
Accession Number
93N11176
Funding Number(s)
PROJECT: RTOP 505-64-52-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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