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.
Automatic Flight Controller With Model Inversion
NASA Tech Briefs ; 16 , 7
1992-07-01
Miscellaneous
No indication
English
Structured Adaptive Model Inversion Controller for Mars Atmospheric Flight
Online Contents | 2008
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