Ride Quality Design Criteria for Aircraft with Active Mode Control Systems

Abstract

Ride quality is becoming an important area of concern in the acceptability of an aircraft. This has led to considering the use of active structural mode control systems on present and future aircraft to obtain acceptable ride quality. Although ride quality criteria are available, these criteria have not included considerations of mode control system effects and performance. This report extends the suggested criteria of a previous report to include the effects of an active structural mode control system. It is shown how the criteria as applied to separate vertical and lateral systems may be used in the design of a single system which controls both the vertical and lateral axes simultaneously.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1972
Accession Number
ADA004456

Entities

People

  • John W. Rustenburg

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Acceptability
  • Air Force
  • Air Force Facilities
  • Aircrafts
  • Airplanes
  • Control Systems
  • Design Criteria
  • Dynamic Response
  • Engineering
  • Probability
  • Probability Density Functions
  • Probability Distributions
  • Ride Quality
  • Saturation
  • Specifications
  • Structural Response
  • Task Performance And Analysis

Readers

  • Aviation Science / Aeronautics.
  • Robotics and Automation.
  • Systems Analysis and Design