In examples, systems and methods for a radiating system of an aircraft are described. The aircraft system includes a conformal antenna array having a flexible substrate configured to conform to a curvature of a portion of an aircraft. Additionally, the conformal array has a plurality of antenna elements coupled to a first surface of the flexible substrate, where the plurality of antennas are formed in an array. The aircraft system further includes radio front-end hardware configured to communicate signals to and from the plurality of antenna elements. Moreover, the aircraft system includes a radar processing system coupled to the radio front-end hardware. Yet further, the aircraft system includes a renewable energy source configured to power the radar processing system and the radio front-end hardware.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Flexible Hybrid Electronic Sensing System for UAV Applications


    Beteiligte:

    Erscheinungsdatum :

    2022-06-30


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G01S RADIO DIRECTION-FINDING , Funkpeilung / B64C AEROPLANES , Flugzeuge / H01Q Antennen , ANTENNAS, i.e. RADIO AERIALS / H02S GENERATION OF ELECTRIC POWER BY CONVERSION OF INFRA-RED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, E.G. USING PHOTOVOLTAIC [PV] MODULES , Erzeugung elektrischer Energie durch Umwandlung von Infrarot-Strahlung, sichtbarem Licht oder ultraviolettem Licht, z.B. unter Verwendung von Photovoltaik [PV]-Modulen




    Flexible electronic assemblies for space applications

    Del Castillo, Linda / Moussessian, Alina / McPherson, Ryan et al. | IEEE | 2010


    Flexible Electronic Assemblies for Space Applications

    Del Castillo, L | Online Contents | 2010


    Multilayered flexible uni-polymer and hybrid composites for ballistic applications

    Butola, B. S. / Majumdar, A. / Jain, A. et al. | British Library Online Contents | 2017