Investigation of Feel System and Control Sensitivity Characteristics Influencing P-I-O of Unmaneuverable Aircraft

Abstract

This report results from a contract tasking TsAGI, Central Aerohydrodynamic Institute as follows: Investigate the pilot-induced-oscillation (PIO) tendency depending upon control sensitivity characteristics, damping of lever loading, lever mass and loading gradient at different flight regimes and dynamic performance using flight simulators.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1995
Accession Number
ADA339046

Entities

People

  • Alexander M. Galyuchenko
  • Larisa E. Zaichik
  • Victor V. Lyasnikov
  • Victor V. Rodchenko
  • Yury P. Yashin

Tags

DTIC Thesaurus Topics

  • Abstracts
  • Aircraft Models
  • Aircrafts
  • Airframes
  • Contracts
  • Control Systems
  • Data Processing
  • Dynamic Response
  • Experimental Data
  • Flight Simulators
  • Frequency
  • Frequency Bands
  • Ground Based
  • Mathematical Models
  • Military Aircraft
  • Simulations
  • Simulators

Readers

  • Aviation Science / Aeronautics.
  • Control Systems Engineering.
  • Political Science/ International Relations/ European Studies