Mechanization of Blended A sub N Mode for CCV YF-16.

Abstract

A root locus analysis and computer simulation are used to determine the feasibility of one proposed method of mechanizing the blending of the normal acceleration mode with the basic aircraft response for the CCV YF-16. The root locus analysis predicts the stability and speed of response of the mechanized aircraft. The computer simulation confirms these results. Comparison is made of the responses of the basic, present CCV, and proposed mechanized YF-16. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1978
Accession Number
ADA056553

Entities

People

  • Kenneth R. Race

Organizations

  • Air Force Institute of Technology

Tags

Communities of Interest

  • Air Platforms
  • Cyber

DTIC Thesaurus Topics

  • Aeronautical Engineering
  • Air Force
  • Aircraft Industry
  • Aircrafts
  • Airframes
  • Computer Programs
  • Computer Simulations
  • Computers
  • Control Systems
  • Equations
  • Equations Of Motion
  • Fighter Aircraft
  • Flight Control Systems
  • Mach Number
  • Plastic Explosives
  • Simulations
  • Transfer Functions

Readers

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