Six degree of freedom simulation software

Govindaraj, KS and Sridhar, JK and Madhuranath, Padma and Bhagawan, BS (1986) Six degree of freedom simulation software. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    The methodology for realizing a general six degree of freedom aircraft simulation on UNIVAC has been documented by taking CESSNA 172 as an example. The software package has been designed, developed and validated by making the program trim the aircraft for a flight condition and then exciting the longitudinal and lateral modes. The results compare well with those reported in literature. The 13; soft-ware structure is designed to simulate any known aircraft and enables modular addition of complex flight control systems, turbulence and landing gear dynamics.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Aircraft simulation;Six degree freedom;Nonlinear simulation software
    Subjects: AERONAUTICS > Aircraft Stability and Control
    Division/Department: Other, Systems Engineering Division, Systems Engineering Division, Systems Engineering Division
    Depositing User: Mr. Ravikumar R
    Date Deposited: 24 Jul 2006
    Last Modified: 24 May 2010 09:47

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