Padma, Madhuranatha and Rekha, R and Srinathkumar, S (1991) Linear Models For The - LCA 645-33. Technical Report. NAL, Bangalore.
Full text available as:![[img]](http://nal-ir.nal.res.in/style/images/fileicons/application_pdf.png) | PDF Download (76Kb) |
Abstract
The Stability Analysis And Control Law Design Of The Contemplated Light Combat Aircraft Needs Derivation Of Linear Aircraft Models From Non-Linear Flight Simulation Models . This Document Presents The Linear Longitudinal And Lateral State And Observation Models-Of The LCA Version 645-33 Obtained From NAL Developed Software For A Dozen Representative Conditions In The Flight Envelope . Poles And Zeros Of The Corresponding - Transfer Functions Have Been Generated And Compared With Those. Obtained By The Aircraft Prime.The Comparisons Give Confidence In The Use Of The Models Obtained From The NAL . Software For Control Law Design.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Linear Models; Combat Aircraft; -Flight Simulation; Control Law Design Aid |
| Subjects: | ASTRONAUTICS > Astronautics (General) |
| Division/Department: | Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division |
| Depositing User: | M/S ICAST NAL |
| Date Deposited: | 24 Aug 2012 10:05 |
| Last Modified: | 24 Aug 2012 10:05 |
| URI: | http://nal-ir.nal.res.in/id/eprint/10777 |
Actions (login required)
| View Item |
