Limiting Performance of Nonlinear Systems with Applications to Helicopter Vibration Control Problems.

Abstract

This report summarizes the accomplishments of a study exploring new methods for the vibration control of helicopters. Reanalysis methodology permits a variety of vibration control problems to be solved efficiently. Both analytical and experimental studies have been conducted. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1982
Accession Number
ADA113239

Entities

People

  • Walter D. Pilkey

Organizations

  • University of Virginia

Tags

Communities of Interest

  • Advanced Electronics
  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Airframes
  • Algorithms
  • Circuit Boards
  • Computations
  • Computers
  • Control Systems
  • Dc Motors
  • Differential Equations
  • Equations
  • Frequency
  • Frequency Response
  • Gages
  • Helicopter Rotors
  • Helicopters
  • Power Supplies
  • Strain Gages

Readers

  • Aviation Science / Aeronautics.
  • Robotics and Automation.
  • Theoretical Analysis.