Helicopter System Dynamics Identification.

Abstract

Methods are discussed which can be used to identify helicopter system dynamics. Stochastic and deterministic techniques are presented and the latter method is applied to flight test data. The stochastic technique is based on the Maximum Likelihood (ML) criterion and can be reduced to the deterministic case. A computer program listing of the deterministic method is given.

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1973
Accession Number
ADA005216

Entities

People

  • A. Fermelia

Tags

DTIC Thesaurus Topics

  • Aircrafts
  • Computer Programs
  • Computers
  • Computing Devices
  • Digital Information
  • Dynamics
  • Helicopters
  • Identification

Readers

  • Aviation Science / Aeronautics.
  • Computer Science.
  • Statistical inference.