Madhuranath, Padma and Sridhar, JK and Bhagavan, Satya B (1987) Simulation of a Light Aircraft. Technical Report. National Aeronautical Laboratory, Bangalore, India.
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Abstract
A light aircraft of the Cessna family, namely Cessna 17213; has been simulated. A sophisticated trim technique has been13; used to generate a number of desirable trim characteristics13; of the aircraft. Typical aircraft modes have been generated. Stall and recovery, spin and recovery responses have also been presented. Comparisons have been made where flight measured data is available.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Aircraft simulation;Light aircraft;Offline simulation;Six degree of freedom simulation;Digital simulation |
| Subjects: | AERONAUTICS > Aircraft Stability and Control AERONAUTICS > Aircraft Design, Testing & Performance |
| Division/Department: | Systems Engineering Division, Systems Engineering Division, Systems Engineering Division |
| Depositing User: | Deputy Head Poornima Narayana |
| Date Deposited: | 04 Sep 2006 |
| Last Modified: | 24 May 2010 09:50 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2626 |
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