The Global Positioning System (GPS) has been approved for a limited number of applications in civil aviation because it is not highly available for meeting safety-of life levels of integrity, which require timely alert if the system is unreliable for navigation under the environment of Performance Based on Navigation (PBN). This paper presents an analysis about principle of an inertial navigation system (INS) and design an new mechanical architecture of INS in terms of increased availability of GPS for civil aviation. This new mechanical architecture has a good mechanical properties in mechanical engineering of civil aviation.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    The Design of INS under PBN


    Beteiligte:

    Erschienen in:

    Applied Mechanics and Materials ; 336-338 ; 1028-1031


    Erscheinungsdatum :

    2013-07-15


    Format / Umfang :

    4 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Design Under Uncertainty

    Online Contents | 2012


    Topsides design under the microscope

    Knott, T. | Tema Archiv | 1988


    Keeping design changes under control

    Popovich, S. | Engineering Index Backfile | 1961


    Fatigue design under multiaxial solicitation

    Bignonnet,A. / Fayard,J.L. / Van,K.D. et al. | Kraftfahrwesen | 1994


    Optimal Aerodynamic Design under Uncertainty

    Schulz, Volker / Schillings, Claudia | Tema Archiv | 2013