Parameswaran, V and Jatinder, Singh and Basappa, - and Raol, JR (2004) Estimation of Aerodynamic Derivatives and Drag Polars from LCA-TDI(SG) Flight Test Data. Technical Report. NAL, Bangalore.
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Abstract
Stabilized Output Error Method (SOEM) Is Applied To LCA-TD1 (SG) Flight Test Data And Aircraft Aerodynamic Derivatives Are Estimated For Zero Slat,U/C Up And Clean Configurations. The Results Presented In Chapter 1 Of The Report Show That The Pitch Damping In Flight Is Lower Than That Predicted By NDLM Values And There Is A Noticeable Reduction In The Flight Determined Derivative C„Fla (And Hence, Weathercock Stability) And C15 (Aileron Control Effectiveness).In Chapter 2, The Performance Maneuver Data Generated During The LCA-TD1 (SG) Flight Tests At Subsonic Speeds Have Been Analyzed . The Flight Determined Drag Of LCA Is Found To Be Lower Than The Drag Obtained From Reference Aerodata.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Flight Data; Stability and Control Derivatives; Estimation; SOEM Drag Polar; Linear Model Vlaues; Model Validation. |
| Subjects: | ASTRONAUTICS > Astronautics (General) |
| Division/Department: | Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division |
| Depositing User: | M/S ICAST NAL |
| Date Deposited: | 06 Aug 2012 10:33 |
| Last Modified: | 06 Aug 2012 10:33 |
| URI: | http://nal-ir.nal.res.in/id/eprint/10710 |
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