Methods for Aircraft State and Parameter Identification

Abstract

Twenty-nine papers and comments are contained in these Proceedings. Several discuss and compare results obtained with different parameter identification techniques applied to specific fighter aircraft at high angles of attack, subsonic and supersonic transports, VTOL and STOL aircraft, and helicopters. Special problem areas such as systems modelling with high internally-generated fluctuations, aircraft state estimation in non-steady flight and parameter identification for non-linear aerodynamic regimes are covered. The sessions at the Specialists' Meeting were titled mathematical models, instrumentation and filters, flight test techniques, analysis of flight test data, rotorcraft parameter identification and selected topics.

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1975
Accession Number
ADA013073

Entities

Organizations

  • AGARD

Tags

Communities of Interest

  • Air Platforms
  • Ground and Sea Platforms
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircraft Equipment
  • Aircraft Industry
  • Aircrafts
  • Airframes
  • Closed Loop Systems
  • Computational Fluid Dynamics
  • Computational Science
  • Computer Programs
  • Control Systems
  • Databases
  • Fighter Aircraft
  • Information Science
  • Mathematical Filters
  • Measurement
  • Short Takeoff Aircraft

Fields of Study

  • Physics

Readers

  • Academic Conference Management
  • Aerospace Engineering
  • Systems Analysis and Design

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow