Aerodynamic parameter estimation from dynamic maneuvers by two step methodology

Gopalratnam, Girija and Raol, JR and Jategaonkar, RV (1993) Aerodynamic parameter estimation from dynamic maneuvers by two step methodology. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    Abstract

    In this document two step methodology to estimate aerodynamic derivatives of a transport aircraft from dynamic maneuvers is thoroughly described. The results of parameter with maximum likelihood method and different types of dynamic maneuvers or their combination are presented. The approach enhances confidence in the methods as well as in the results

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Two step methodology;Regression;Maximum;Likelihood method;Transport aircraft;Model selection
    Subjects: AERONAUTICS > Aircraft Design, Testing & Performance
    AERONAUTICS > Aerodynamics
    Division/Department: Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division
    Depositing User: Mrs Neetu Chandra
    Date Deposited: 03 Jul 2006
    Last Modified: 24 May 2010 09:43
    URI: http://nal-ir.nal.res.in/id/eprint/1817

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