Flying Qualities of Relaxed Static Stability Aircraft. Volume 2. Ramifications of Flight-Essential/Critical Heavily-Augmented Airplane Characteristics on Flying Qualities

Abstract

Volume 1 of the report deals with airworthiness assessment and flying qualities evaluation of highly augmented aircraft covered by Parts 23 and 25 of the Federal Aviation Regulations. Particular emphasis has been placed on aircraft with relaxed static stability and on the use of active augmentation systems to achieve the minimum requirement for a level of safety in such aircraft. Significant modifications and expansion to the FAA Engineering Flight Test Guides are detailed. Volume 2 supports the work of Volume 1 and provides the more analytically oriented research results of this report. Emphasis is placed on determining the relative similarities and differences between heavily augmented and conventional aircraft. A number of important generic distinctions have been found and are described and explained.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1982
Accession Number
ADA128720

Entities

People

  • Duane Mcruer
  • Thomas T. Myers

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aircrafts
  • Airframes
  • Airplanes
  • Closed Loop Systems
  • Control Surfaces
  • Control Systems
  • Databases
  • Diptera
  • Dynamic Response
  • Energy Efficiency
  • Engineering
  • Equations
  • Flight Paths
  • Resonant Frequency
  • Test And Evaluation
  • Transport Aircraft

Readers

  • Aviation Science / Aeronautics.
  • Business Analytics
  • Systems Analysis and Design