An improved design technique for model following control; systems in;In-flight simulation

Henschel, F and Chetty, Shyam (1987) An improved design technique for model following control; systems in;In-flight simulation. 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: Monograph (Technical Report)
Uncontrolled Keywords: In-flight simulation;Model following control;Singular values;Robustness
Subjects: AERONAUTICS > Aircraft Design, Testing & Performance
Depositing User: Users 64 not found.
Date Deposited: 07 Jul 2006
Last Modified: 12 Aug 2015 07:20
URI: http://nal-ir.nal.res.in/id/eprint/2161

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