Henschel, Frohmut and Chetty, Shyam (1987) An improved design technique for model following control13; systems in quot;In-flight simulationquot;. Technical Report. National Aeronautical Laboratory, Bangalore, India.
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Abstract
The report outlines the various improvements that were made in the design technique to obtain better performance.13; The feedforward branches include additional filters to make the forward loop gains independent of the model aircraft parameters. This permits the use of both linear/13; nonlinear models for the model aircraft during inflight13; simulation. For determining the feedback gains new robustness measures derived from singular value decomposition were used to supplement the time domain criteria during optimisation. The present technique yields designs with lower feedback gains and improved performance.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | In-flight simulation;Model following control;Singular values;Robustness |
| Subjects: | AERONAUTICS > Aircraft Design, Testing & Performance |
| Division/Department: | Other, Systems Engineering Division |
| Depositing User: | Mr. Ravikumar R |
| Date Deposited: | 07 Jul 2006 |
| Last Modified: | 24 May 2010 09:46 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2161 |
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