Parameswaran, V and Girija, G and Raol, JR (2003) Estimation of parameters from large amplitude maneuvers13; with partitioned data for aircraft. Project Report. National Aerospace Laboratories, Bangalore, India.
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Abstract
This report describes the data partitioning method to concatenated large amplitude maneuvers (LAM) of a fighter aircraft to estimate the stability and control derivatives. Stepwise multiple linear regression is used to determine the model structure within each partitioned data set. Application of this method to LAM generated from a research simulator, yields a useful procedure for estimating the pitch up tendency by the aircraft during certain angle of attack range. Estimation results using model error method for the longitudinal derivatives from LAMs are also included in this report.
| Item Type: | Proj.Doc/Technical Report (Project Report) |
|---|---|
| Uncontrolled Keywords: | Large amplitude maneuvers, partitioning, SMLR, model error,13; Pitch up tendency, aerodynamic derivatives |
| Subjects: | AERONAUTICS > Aircraft Stability and Control |
| Division/Department: | Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division |
| Depositing User: | admin |
| Date Deposited: | 24 Jan 2005 |
| Last Modified: | 24 May 2010 09:39 |
| URI: | http://nal-ir.nal.res.in/id/eprint/583 |
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