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.
![[img]](https://nal-ir.nal.res.in/style/images/fileicons/application_pdf.png) |
PDF
tr_pdfc_9311_RR77835_txt.pdf Restricted to Repository staff only Download (11MB) |
![[img]](https://nal-ir.nal.res.in/style/images/fileicons/other.png) |
Indexer Terms (Generate index codes conversion from application/pdf to indexcodes)
indexcodes.txt Restricted to Repository staff only Download (9kB) |
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: | Monograph (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Two step methodology;Regression;Maximum;Likelihood method;Transport aircraft;Model selection |
| Subjects: | AERONAUTICS > Aircraft Design, Testing & Performance AERONAUTICS > Aerodynamics |
| Depositing User: | Mrs Neetu Chandra |
| Date Deposited: | 03 Jul 2006 |
| Last Modified: | 24 May 2010 04:13 |
| URI: | http://nal-ir.nal.res.in/id/eprint/1817 |
Actions (login required)
 |
View Item |
