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.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Flight Mode Concept and Realisation


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    10.09.2017


    Format / Umfang :

    32 pages




    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Flight Mode: Concept and Realisation

    Schagaev, Igor / Kirk, Brian / Friedrich, Felix et al. | Springer Verlag | 2025




    Concept and Realisation of Sequential Port Time Injection of CNG

    Jaasma, S. / International Association for Natural Gas Vehicles / European Natural Gas Vehicle Association | British Library Conference Proceedings | 1998


    The chassis concept of the AUDI A5. From ideas to realisation

    Schindlmaister, Roman / Dietz, Jürgen / Kainz, Peter et al. | Tema Archiv | 2007