COMPARATIVE STUDY OF TWO MODEL REFERENCE, ADAPTIVE AIRCRAFT CONTROL SYSTEMS.

V. E. Edwards, W. L. Garrard

Research output: Contribution to conferencePaperpeer-review

2 Scopus citations

Abstract

Two types of model reference adaptive control systems for aircraft were compared. One was based on the MIT design procedure and a second based on Liapunov stability theory. The basic problem considered in this study was how well each system adapted to changes in parameters affecting aircraft performance. After considering the simulated dynamic response of an adaptively controlled aircraft at a variety of flight conditions, it was concluded that the Liapunov-based technique provided more desirable response than did the MIT system.

Original languageEnglish (US)
Pages33-42
Number of pages10
StatePublished - Jan 1 1974
EventJt Autom Control Conf, 15th, Proc - Austin, TX, USA
Duration: Jun 18 1974Jun 21 1974

Other

OtherJt Autom Control Conf, 15th, Proc
CityAustin, TX, USA
Period6/18/746/21/74

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