Khare, Alok and Madhuranath, Padma (1993) Linear simulation software LINSIM. Technical Report. National Aeronautical Laboratory, Bangalore, India.
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Abstract
A Linear Simulation Software (LINSIM) has been developed to simulate the flight of an unstable airplane in the linear domain. The unstable plane is artificially controlled by suitable design of fly-by-wire control laws to ensure desired handling qualities. The software is an invaluable aid in the design and evaluation of the flight13; control law. The airplane can be trimmed for various trim states like straight and level, left turn and right turn, push-over and pull-up and the linear models generated through the linearizing link software ALLS. The software provides airplane motion through pilot command inputs from13; the stick. It facilitates interactive plotting 0f time histories 0f all the f1ight variab1es. The software plays an important role in the iterative process of fly-by-wire control law design and evaluation.13;
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Linear simulation;Simulation software Closed loop;Aircraft flight simulation |
| Subjects: | AERONAUTICS > Aircraft Design, Testing & Performance AERONAUTICS > Aerodynamics |
| Division/Department: | Flight Mechanics and Control Division, Flight Mechanics and Control Division |
| Depositing User: | Mrs Neetu Chandra |
| Date Deposited: | 11 Jul 2006 |
| Last Modified: | 24 May 2010 09:44 |
| URI: | http://nal-ir.nal.res.in/id/eprint/1824 |
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