NASA NTRS · 19920000400
Automatic Flight Controller With Model Inversion
Abstract
Automatic 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.
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Meyer, George, Smith, G. Allan. 1992-07-01. Automatic Flight Controller With Model Inversion. https://ntrs.nasa.gov/citations/19920000400
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