APPLICATION OF MODEL REFERENCE PARAMETER-PERTURBATION SELF-ADAPTIVE CONTROL TO A FLIGHT CONTROL SYSTEM.
AIR FORCE INST OF TECH WRIGHT-PATTERSON AFB OH SCHOOL OF ENGINEERING
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Feedback systems along with several self-adaptive systems previously developed are introduced. A linearized mathematical solution of the adaptive loop of the controller is developed using time-varying parameter-perturbation system analysis. Simulation of the system is completed with the model reference parameter-perturbation self-adaptive controller successfully tracking and controlling sinusoidal and square wave disturbances in aerodynamic gain. A discussion of the results of the simulation is included. Several recommendations for further work in this study are stated. Author
- Research and Experimental Aircraft