A BLENDED FEEDBACK VARIABLE FOR CONTROL AUGMENTATION SYSTEMS.

Abstract

A man-airframe disturbance sensitivity model has been postulated. The existence of optimum pilot chosen compensation in the multiloop compensatory mode is shown to result in minimum closed loop sensitivity to pilot induced stick input errors. Based on existing fixed base simulator data it is shown that an optimum ratio exists for blended feedback control of pitch rate and normal acceleration. (Author)

Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1967
Accession Number
AD0659753

Entities

People

  • D. T. Makers

Organizations

  • General Electric

Tags

DTIC Thesaurus Topics

  • Airframes
  • Compensation
  • Feedback
  • Mechanical Structure
  • Sensitivity
  • Simulators

Fields of Study

  • Physics

Readers

  • Control Systems Engineering.