Rajamurthy, MS (1988) Stability and control derivatives of Light Canard Research Aircraft (LCRA). Technical Report. National Aeronautical Laboratory, Bangalore, India.
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Abstract
From the geometric data of NAL's Light Canard Research Aircraft (Rutan Long-Ez), its stability and control derivatives were estimated for various flight conditions using analytical/ empirical procedures . These estimated values would serve as basic data and would be used for designing optimal control inputs for generating flight test data for parameter estimation . This basic data would be compared with the flight test results to ascertain the accuracy of the analytical estimation procedures for this type of configurations .
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Stability and control derivatives;Canard configuration |
| Subjects: | AERONAUTICS > Aircraft Stability and Control |
| Division/Department: | Systems Engineering Division |
| Depositing User: | Deputy Head Poornima Narayana |
| Date Deposited: | 18 Aug 2006 |
| Last Modified: | 24 May 2010 09:46 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2148 |
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