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: | Monograph (Technical Report) |
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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 |
Depositing User: | Poornima Narayana |
Date Deposited: | 04 Sep 2006 |
Last Modified: | 24 May 2010 04:20 |
URI: | http://nal-ir.nal.res.in/id/eprint/2626 |
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