Abstract The principle of active system control (ASC) can and should be applied at the elemental and modular levels of design of a system, as well as at the whole system level of design. This chapter presents an application of ASC for flight mode determination using currently available flight data and the state of an aircraft (based on previous states of flight). Using a dependency matrix structure with analysis of flight data, we present a rigorous model of flight mode detection. We also illustrate how the flight mode system works by providing examples of the program modules required.


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    Title :

    Flight Mode Concept and Realisation


    Contributors:

    Published in:

    Publication date :

    2017-09-10


    Size :

    32 pages




    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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