A near-optimal minimum-time guidance law to a fixed point under a terminal angular manifold is developed. The planar case and the spatial case are separately considered. The problems are solved in several stages with increased level of complexity: from the simple case of a constant speed with a fixed terminal angular direction (Dubins problem), through the case of a constant speed with a terminal conical manifold, to the more general case of atmospheric flight with a terminal conical manifold.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Near-Optimal Minimum-Time Guidance Under Spatial Angular Constraint in Atmospheric Flight


    Beteiligte:
    Indig, Nahshon (Autor:in) / Ben-Asher, Joseph Z. (Autor:in) / Sigal, Erez (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.07.2016




    Medientyp :

    Aufsatz (Konferenz) , Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Near - Optimal Minimum Time Guidance under Spatial Angular Constraint in Atmospheric Flight

    Indig, N. / Ben-Asher, J.Z. / Sigal, E. et al. | British Library Conference Proceedings | 2014



    Near-Optimal Minimum Time Guidance under a Spatial Angular Constraint in Atmospheric Flight

    Indig, Nahshon / Z. Ben-Asher, Joseph / Sigal, Erez | AIAA | 2015


    Near-Optimal Minimum Time Guidance under a Spatial Angular Constraint in Atmospheric Flight (AIAA 2015-0089)

    Indig, Nahshon / Ben-Asher, Joseph Z. / Sigal, Erez | British Library Conference Proceedings | 2015


    NEAR-OPTIMAL SPATIAL MID-COURSE GUIDANCE LAW WITH ANGULAR CONSTRAINT

    Indig, Nahshon / Ben-Asher, Joseph / Farber, Nathan | AIAA | 2012