APPLICATION OF MODEL REFERENCE PARAMETER-PERTURBATION SELF-ADAPTIVE CONTROL TO A FLIGHT CONTROL SYSTEM.

Abstract

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)

Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1968
Accession Number
AD0836735

Entities

People

  • Charles L. Nefzger

Organizations

  • Air Force Institute of Technology

Tags

DTIC Thesaurus Topics

  • Adaptive Systems
  • Closed Loop Systems
  • Control Systems
  • Feedback
  • Flight Control Systems
  • Perturbations
  • Simulations
  • Square Waves
  • Waves

Readers

  • Control Systems Engineering.