Rajeeva, Kumar and Shyam, Chetty (1995) Flight CoptroI Design Using Multi -objective Multi -model optimisation Technique. Technical Report. National Aerospace Laboratories, Bangalore, India.
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Abstract
The report describes the development of a flight control system synthesis software based on a multi-objective multi-model optimisation procedure using the Performance-Index13; Vector Optimisation technique based on the minimisation of the Kreisselmeier Function. The software is written in Fortran-77. Various design criteria like gain and phase margins. Gibson's drop back error. Neal-Smith criterion. Gibson's phase rate criterion, CAP', q-model following,13; flight path time delay, normal acceleration overshoot, maximum unstable root location, actuator rate. and dominant mode damping have been quantified numerically to form a part of the Performance Index Vector.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Vector Optimisation;Kreisselmeier Function;Performance Index Vector;Margins;Drop back by q;Actuator Rate;Gibson Criteria;Simplified Neal-Smith's Criteria;Flight Control System Design |
| Subjects: | AERONAUTICS > Aerodynamics |
| Division/Department: | Flight Mechanics and Control Division, Flight Mechanics and Control Division |
| Depositing User: | Mrs Neetu Chandra |
| Date Deposited: | 01 Jun 2006 |
| Last Modified: | 24 May 2010 09:41 |
| URI: | http://nal-ir.nal.res.in/id/eprint/1368 |
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