Fixed Gain Controller Design for Aircraft.

Abstract

A Method for designing fixed gain controllers and filters for systems with large parameter variation is presented. The approach, based of minmax information criteria, is used to design a non-adaptive back-up control system for a given aircraft and is shown to provide good performance qualities. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Jun 30, 1981
Accession Number
ADA104877

Entities

People

  • Doron Eidelman
  • Yoram Baram

Organizations

  • Tel Aviv University

Tags

Communities of Interest

  • Air Platforms
  • Materials and Manufacturing Processes
  • Space

DTIC Thesaurus Topics

  • Adaptive Control Systems
  • Adaptive Filters
  • Adaptive Systems
  • Aircrafts
  • Control Systems
  • Design Criteria
  • Dynamic Pressure
  • Eigenvalues
  • Equations
  • Estimators
  • Fighter Aircraft
  • Filters
  • Kalman Filters
  • Mach Number
  • Measurement
  • Military Aircraft
  • Optimal Estimators

Readers

  • Aviation Science / Aeronautics.
  • Neural Network Machine Learning.
  • Operations Research