Simulation of a Light Aircraft

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: 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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