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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