A Practical Scheme for Adaptive Aircraft Flight Control Systems,

Abstract

The purpose of the report is to present a flight control system design, that can be implemented by analog hardware, to be used to control an aircraft with uncertain parameters. The design is based upon the use of modern control theory. The ideas are illustrated by considering control of STOL longitudinal dynamics. (Author)

Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1973
Accession Number
AD0760790

Entities

People

  • Dieter Willner
  • Michael Athans

Organizations

  • Massachusetts Institute of Technology

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Traffic Control Systems
  • Aircrafts
  • Control Systems
  • Control Theory
  • Dynamics
  • Flight Control Systems
  • Flight Testing

Fields of Study

  • Mathematics

Readers

  • Adaptive Control and Estimation with Uncertainty in Dynamic Systems.
  • Aerospace Engineering