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automatic flight controller with model inversionAutomatic digital electronic control system based on inverse-model-follower concept being developed for proposed vertical-attitude-takeoff-and-landing airplane. Inverse-model-follower control places inverse mathematical model of dynamics of controlled plant in series with control actuators of controlled plant so response of combination of model and plant to command is unity. System includes feedback to compensate for uncertainties in mathematical model and disturbances imposed from without.
Document ID
19920000400
Document Type
Other - NASA Tech Brief
Authors
Meyer, George
(NASA Ames Research Center, Moffett Field, CA.)
Smith, G. Allan
(Yale Univ.)
Date Acquired
August 15, 2013
Publication Date
July 1, 1992
Publication Information
Publication: NASA Tech Briefs
Volume: 16
Issue: 7
ISSN: 0145-319X
Subject Category
ELECTRONIC SYSTEMS
Report/Patent Number
ARC-12849
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.