Specifications for a MDS for flight control software development

Karunakar, K and Prasad, Shylaja and Chandrasekhar, Ahalya (1986) Specifications for a MDS for flight control software development. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    In the development of modern aircraft, the translation of control laws into reliable software which has to be executed in the target flight computer in realtime is complex engineering effort. The task of developing and validating high integrity FCS systems can only be achieved in practical time scales if adequate tools are availabe. This document highlights the need for a microcomputer development system with a link to host computer. A detailed specification of the system required for the above task is also given.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Microcomputer development system (MDS;Fly-by-wire(FBW);Control system;Avionics compilers;Target computer; Emulation;Simulation;Software development;Host computer link
    Subjects: MATHEMATICAL AND COMPUTER SCIENCES > Computer Programming and Software
    AERONAUTICS > Avionics & Aircraft Instrumentation
    Division/Department: Systems Engineering Division, Systems Engineering Division, Systems Engineering Division
    Depositing User: Mr. Ravikumar R
    Date Deposited: 18 Aug 2006
    Last Modified: 24 May 2010 09:46
    URI: http://nal-ir.nal.res.in/id/eprint/2248

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